175 Commits
v1.0.5 ... v2.0

Author SHA1 Message Date
Junzi Sun
72fe72c16c pypi release v2.0 2019-02-21 14:52:15 +01:00
Junzi Sun
31df5c2042 fix dump path 2019-02-21 14:39:57 +01:00
Junzi Sun
10e9b234ad sort dump output by time 2019-02-21 14:33:15 +01:00
Junzi Sun
546d69c129 bug fix 2019-02-16 01:10:12 +01:00
Junzi Sun
c4c285266c update readme for new dump option 2019-02-08 16:43:02 +01:00
Junzi Sun
ebc11e5e84 enable saving decode data to csv files 2019-02-08 16:41:24 +01:00
Junzi Sun
f5c2b36209 Merge pull request #35 from Ka-zam/skysense
Enable skysense raw type in the streamer.
2019-01-23 11:49:04 +01:00
Magnus Lundmark
759380b5a9 Updated README 2019-01-22 09:52:01 +01:00
Magnus Lundmark
3f6389a67d Clarifications of Skysense format 2019-01-22 09:44:58 +01:00
Magnus Lundmark
c252647e77 Bugfixes 2019-01-21 16:16:41 +01:00
Magnus Lundmark
1795d2f3c0 updates to handler 2019-01-18 17:44:19 +01:00
Magnus Lundmark
fb4cef7085 Initial Skysense support 2019-01-18 16:09:04 +01:00
Junzi Sun
b24c1101b6 add DF 0 and 16 to altcode 2018-12-14 17:22:55 +01:00
Junzi Sun
8a43d711aa add track rate from bds50 to streamer 2018-12-04 18:17:05 +01:00
Junzi Sun
495f320988 fix exceptions 2018-11-30 23:36:58 +01:00
Junzi Sun
44a9c8d2aa fix test for commb 2018-11-30 22:50:05 +01:00
Junzi Sun
ecfc4037a1 catch exceptions in uncertainty handeling 2018-11-30 22:47:00 +01:00
Junzi Sun
61f2191feb add BDS50 roll to streamer 2018-11-30 16:51:27 +01:00
Junzi Sun
9e1cc2c5a2 Merge pull request #32 from Akasch/fix_screen_offset
streamer.screen: fix missing flights in view
2018-11-27 17:40:56 +01:00
Junzi Sun
500c3ca9bd Merge pull request #33 from Akasch/fix_cpu_usage
modeslive: fix hight CPU usage
2018-11-27 17:16:57 +01:00
Nils Rokita
78f1ca77c7 modeslive: fix hight CPU usage
The core loop in modeslive is currently busy waiting for updates
I think an update rate at 50Hz is more reasonable and reduces cpu usage.
2018-11-27 15:59:37 +01:00
Nils Rokita
576713f13b streamer.screen: fix missing flights in view
the row is countin from 3 to the window hight, but the idx ist used
as index into the icaos list beginning at 0. the offset is 0 for the
first page. This results in the first 3 flights not shown.
2018-11-27 15:46:56 +01:00
Junzi Sun
3502fedf02 Merge pull request #31 from Akasch/fix_screen_clear
streamer.screen: fix undefined variable icao on emty flight list
2018-11-26 21:33:47 +01:00
Nils Rokita
de9ec43912 streamer.screen: fix undefined variable icao on emty flight list
The icao variable is tested for None on line 136 but is not defined if
no flight is known
2018-11-26 16:00:46 +01:00
Junzi Sun
16c83d1505 fix bug in NACv 2018-10-02 23:32:07 +02:00
Junzi Sun
e5d5633535 relax bds17 identification 2018-08-24 16:45:12 +02:00
Junzi Sun
8adacd8e91 Merge pull request #27 from hv92/master
Update readme
2018-07-25 22:38:12 +02:00
Huy Vu
fd15b13c17 Update readme 2018-07-25 20:09:28 +02:00
Junzi Sun
405d8ed108 update screenshot 2018-07-04 21:35:48 +02:00
Junzi Sun
0085d03d4a add callsign to modeslive 2018-07-04 21:31:09 +02:00
Junzi Sun
6f139d4ae9 make modeslive uncertanty values optional 2018-07-04 21:20:23 +02:00
Junzi Sun
e5ca76ac0d rename live script to modeslive 2018-07-04 20:56:11 +02:00
Junzi Sun
ef9d2cfd16 fix NICv2 bug 2018-07-04 18:14:13 +02:00
Junzi Sun
ea1ccc0c70 add instructions for getting a raw stream from RTL-SDR 2018-06-29 14:13:20 +02:00
Junzi Sun
648f4660b7 Merge branch 'JoseAndresMR-master' 2018-06-27 22:09:05 +02:00
Junzi Sun
0df6a664a3 resturctue the uncertainty module, and some additional fixings. 2018-06-27 22:08:13 +02:00
JoseAndresMR
44b277f0ad various fixing 2018-06-26 23:15:57 +02:00
JoseAndresMR
715d0a3c66 implementation of uncertainty values from csv files 2018-06-26 16:22:42 +02:00
JoseAndresMR
6db5ea8023 "fetch from upstream" 2018-06-25 16:25:17 +02:00
JoseAndresMR
7685f1590f for first merge with upstream 2018-06-25 16:19:07 +02:00
Junzi Sun
5fa090b95f update screenshot 2018-06-23 16:05:06 +02:00
Junzi Sun
6c5ae2141b add example screenshot of pmslive 2018-06-23 15:59:26 +02:00
Junzi Sun
24f3658673 skeleton code for DF 0/4/5/11/16 2018-06-23 15:54:17 +02:00
Junzi Sun
205725872a update pmslive and tcpclient, add support for AVR. 2018-06-23 15:19:29 +02:00
Junzi Sun
01a573a1af update live screen 2018-06-23 14:40:27 +02:00
Junzi Sun
c0476f5e16 readme code format 2018-06-23 01:29:58 +02:00
Junzi Sun
140b68afbc add pmslive command reference 2018-06-23 01:28:41 +02:00
Junzi Sun
70b3af2c8b add script: pmslive 2018-06-23 01:24:15 +02:00
Junzi Sun
0ef64be934 update pmstream, add nic/nac/sil. 2018-06-23 00:20:38 +02:00
Junzi Sun
bbe6e50fb2 Merge branch 'JoseAndresMR-master', add ADS-B uncertainties 2018-06-22 22:52:36 +02:00
Junzi Sun
a3e44b5626 fixing code 2018-06-22 22:52:11 +02:00
JoseAndresMR
457a948879 Uncertainty and Accuracy parameters 2018-06-22 12:31:19 +02:00
Junzi Sun
54b2038a41 update readme, add id / alt code instruction 2018-06-21 17:38:59 +02:00
Junzi Sun
82b912bc05 update readme 2018-06-20 22:25:47 +02:00
Junzi Sun
6d5869a9e0 update readme 2018-06-20 22:22:42 +02:00
Junzi Sun
36840e0225 Merge branch 'master' into dev-2.0 2018-06-20 17:03:40 +02:00
Junzi Sun
972ffe264e Update README.rst 2018-06-20 16:29:36 +02:00
Junzi Sun
d4ca81e0ca Update README.rst 2018-06-20 16:18:39 +02:00
Junzi Sun
9fa475ab9a add more DF to icao function 2018-05-30 10:25:00 +02:00
Junzi Sun
c91bd4bb03 fix bug 2018-05-24 12:49:46 +02:00
Junzi Sun
4f0946c4da update readme 2018-05-17 10:49:40 +02:00
Junzi Sun
46a99852d6 update readme 2018-05-17 10:40:22 +02:00
Junzi Sun
2389c12b98 add [commb], depricate [ehs] and [els] 2018-05-17 10:34:14 +02:00
Junzi Sun
6128c5a18d update sample run script for comm-b 2018-05-17 09:52:50 +02:00
Junzi Sun
72c1a9f645 Merge pull request #21 from federicoorta/dev-2.0
Run samples updated in dev-2.0
2018-05-17 09:32:12 +02:00
Junzi Sun
f221c67295 keep only bds 40 50 60
Other bds code does not belong to Enhanced Mode-S definition.
2018-05-17 09:24:31 +02:00
forta
14a537030d Sample run of EHS decoding has been fixed. 2018-05-16 19:09:02 +02:00
forta
b7afd841ff Import of 'util' module substituted with 'common'. 2018-05-16 17:41:19 +02:00
Junzi Sun
11b85b6959 fix temp44 and bds imports 2018-05-02 14:33:27 +02:00
Junzi Sun
8a54f927f6 fix deprecation warning 2018-04-19 09:45:56 +02:00
Junzi Sun
9bfc116516 Merge branch 'dev-2.0' of github.com:junzis/pyModeS into dev-2.0 2018-04-17 15:08:35 +02:00
Junzi Sun
be38acabfd fix type error 2018-04-17 14:48:55 +02:00
Junzi Sun
0b6d5576d3 Merge pull request #18 from hv92/patch-1
Add additional BDS 4,0 check
2018-04-13 16:39:35 +02:00
Huy Vû
dfdddb77f2 Update bds40.py 2018-04-13 16:17:31 +02:00
Huy Vû
a872cd253e Update bds40.py 2018-04-13 16:14:31 +02:00
Junzi Sun
edbfdc68de fix bug 2018-04-05 15:32:17 +02:00
Junzi Sun
f246c88dd6 add try except 2018-04-04 16:41:34 +02:00
Junzi Sun
e821b8fa77 update roll check 2018-04-04 10:41:55 +02:00
Junzi Sun
1b3dcef659 add oe_flag() back 2018-04-04 09:46:21 +02:00
Junzi Sun
7653b2459d minor update 2018-04-04 09:46:05 +02:00
Junzi Sun
7c52db318d release version 1.2.2 2018-03-28 13:49:46 +02:00
Junzi Sun
362b92de7a major update; adsb restructure; rename combining util/modes to common. 2018-03-28 13:31:24 +02:00
Junzi Sun
ef8f4b3b7f Merge branch 'dev-2.0' of github.com:junzis/pyModeS into dev-2.0 2018-03-27 18:24:33 +02:00
Junzi Sun
773efff9bc added deprecation waring 2018-03-27 18:24:22 +02:00
Junzi Sun
05e34e7516 Merge pull request #17 from hv92/dev-2.0
Minor change BDS 5,0 roll angle detection
2018-03-27 13:55:19 +02:00
Huy Vu
161ea31ee1 Minor change BDS 5,0 roll, if status and sign bit are both 1, roll angle was -90 degrees. 2018-03-27 13:04:52 +02:00
Junzi Sun
12506e7c7f restructure, add BDS30 2018-03-26 21:05:54 +02:00
Junzi Sun
fcd98d6bcc Merge pull request #15 from hv92/patch-2
too hight rounding track/heading angles, change to 3 decimal points.
2018-03-16 11:57:46 +01:00
Junzi Sun
ef40acdbfd Update ehs.py
let's make them to  3 decimals even
2018-03-16 11:56:49 +01:00
Junzi Sun
8b48fabf5a add ehs BDS10 decoder, cut redundancies 2018-03-16 11:53:09 +01:00
Huy Vû
d91ad261cd Too rough rounding track/heading angles
Due to resolution of 0.175 degrees, rounding difference up to 0.05 degrees can occur.
2018-03-16 11:22:10 +01:00
Junzi Sun
4911e69171 update EHS BDS identification, add isBDS50or60() function 2018-03-13 16:55:50 +01:00
Junzi Sun
5697e5b88e Merge pull request #14 from hv92/patch-1
Probabilistic method for BDS detection
2018-03-13 12:08:32 +01:00
Junzi Sun
3073187d24 Update ehs.py 2018-03-13 12:08:10 +01:00
Huy Vû
441cd27761 Probabilistic method for BDS detection
Including probabilistic method to determine BDS 5,0 and BDS 6,0 (by using a multivariate normal distribution with reference data)
2018-03-13 11:31:34 +01:00
Junzi Sun
c4406ba276 update pip install 2018-03-12 13:45:48 +01:00
Junzi Sun
de6238f5e9 improve isBDS60 identification 2018-03-09 13:58:10 +01:00
Junzi Sun
711fd889e6 Merge branch 'master' into dev-2.0 2018-03-09 13:19:33 +01:00
Junzi Sun
e692d30d66 fix vertical rate 2018-03-09 13:19:12 +01:00
Junzi Sun
d6a04865dc merge from master with BDS60 vertical rate bug fix 2018-03-08 16:41:20 +01:00
Junzi Sun
fd8bb8386f fix vertical rate bug in BDS60 2018-03-08 16:36:09 +01:00
Junzi Sun
6baa218596 update crc 2018-01-16 15:37:04 +01:00
Junzi Sun
8a9045e730 arguments for pmstream 2017-12-20 17:16:31 +01:00
Junzi Sun
d13e1bd12e initial commit for v2.0 2017-12-20 17:00:02 +01:00
Junzi Sun
2b1f2a5878 rename spd to trk 2017-12-12 23:06:03 +01:00
Junzi Sun
3538645e22 Update README.rst 2017-12-12 21:48:25 +01:00
Junzi Sun
a9887d6238 minor fix in bit sequence 2017-11-18 22:14:09 +01:00
Junzi Sun
7c8fd74db7 fix velocity message with no data; and update some comments 2017-11-15 22:33:06 +01:00
Junzi Sun
35b0d63fa9 update readme 2017-11-01 11:53:10 +01:00
Junzi Sun
2ae7bf4c19 Merge pull request #13 from hv92/patch-6
update identification function for BDS44
2017-10-24 17:59:17 +02:00
Huy Vû
e8449154ca Update ehs.py
Additional checks BDS4,4
2017-10-24 13:02:08 +02:00
Junzi Sun
fbe5b63286 Merge pull request #12 from hv92/patch-2
Temperature requirement
2017-10-11 20:34:39 +02:00
Huy Vû
45c32cd7aa Temperature requirement
Temperature range [-80,60] is a requirement in Annex 3
2017-10-11 11:38:26 +02:00
Junzi Sun
c708d57fcc Update README.rst 2017-09-19 11:19:54 +02:00
junzis
53a258bd35 version 1.2.0 2017-09-18 16:00:58 +02:00
junzis
d9e277dc54 set zero altitude when decoding surface message 2017-08-03 17:18:07 +02:00
junzis
854386fbd4 update EHS sample data 2017-07-31 14:28:26 +02:00
junzis
3117febac0 update EHS sample data 2017-07-31 14:23:59 +02:00
junzis
8693c51998 update sample run data and scripts 2017-07-27 13:41:21 +02:00
junzis
8c90371111 update BDS60 check 2017-07-26 12:02:49 +02:00
Junzi Sun
c6952e4e63 major bug fix, signed values in ehs (two's complement) 2017-07-25 23:29:03 +02:00
junzis
98e5d81ae1 update test altcode test function 2017-07-25 13:05:48 +02:00
junzis
fd557d1c40 fix DF4,20 altitude decoding 2017-07-25 12:28:06 +02:00
junzis
cdbcf47bc2 fix DF4,20 altitude decoding 2017-07-25 12:27:07 +02:00
junzis
5f7e28950c work on altitude code 2017-07-24 17:06:20 +02:00
junzis
c1d0a925d5 work on altitude code 2017-07-24 17:01:10 +02:00
junzis
b0a71717f0 work on altitude code 2017-07-24 16:59:46 +02:00
Junzi Sun
25e5a4e412 increase roll angle limit 2017-07-22 11:58:29 +02:00
junzis
d3022c6fe5 update readme 2017-07-21 17:45:08 +02:00
junzis
aa9f49b470 add DF4/20 altitude and DF5/21 squawk decoding 2017-07-21 17:40:10 +02:00
junzis
27daf52850 minor update 2017-07-21 16:02:40 +02:00
junzis
0e29a4d18a minor update 2017-07-21 15:57:32 +02:00
junzis
1e842e4789 add altitude difference function in adsb, fix bug. 2017-07-21 15:53:50 +02:00
junzis
1220368ada Merge branch 'master' of github.com:junzis/pyModeS 2017-07-21 15:17:13 +02:00
junzis
fb32ace095 update BDS 1,7 decoding 2017-07-21 15:17:02 +02:00
Junzi Sun
abafd97b3f Merge pull request #10 from hv92/patch-1
Fix altitude
2017-07-21 05:58:49 -07:00
hv92
0a38231713 Fix altitude 2017-07-21 13:58:14 +02:00
junzis
2fd822d275 update BDS 6,0 checks 2017-03-31 17:24:55 +02:00
Junzi Sun
8de58bb01f Fixed what seems to be an ICAO documentation error: sign reversed in vertical speed in BDS60 messages. 2017-03-29 21:32:40 +02:00
junzis
140f312c11 new release v1.1.1 2017-03-23 16:15:15 +01:00
junzis
fefd26a787 fix import error in Python3 2017-03-23 16:10:22 +01:00
junzis
1e82b5c59c update EHS module 2017-03-23 13:12:33 +01:00
junzis
a1615767b6 Merge branch 'master' of github.com:junzis/pyModeS 2017-03-23 12:08:36 +01:00
junzis
03a62dc68c update EHS module 2017-03-23 12:08:15 +01:00
junzis
46fee6b7dc update EHS module 2017-03-23 11:48:51 +01:00
Junzi Sun
8aa821c8dd Update requirements.txt 2017-03-22 21:25:07 +01:00
Junzi Sun
621d3e7580 new release version 2017-03-22 21:14:41 +01:00
Junzi Sun
3b3609bf2b Update README.rst 2017-03-22 21:07:59 +01:00
Junzi Sun
ef2268127c Major funciton renaming in EHS for suppporting more BDS types. Bug fixes. 2017-03-22 21:06:51 +01:00
junzis
cc66e2f4e4 version 1.0.9 2017-03-21 18:14:30 +01:00
junzis
128163b41d update BDS 4,4 decoder, default to revised version 2017-03-17 18:03:54 +01:00
Junzi Sun
8933afb1c1 Update ehs.py 2017-03-17 15:24:18 +01:00
junzis
15f2833aee add surface velocity decoding from msg TC:5-8 2017-03-07 13:41:07 +01:00
junzis
2b3e2c62d0 update package version 2017-03-07 10:35:45 +01:00
junzis
cadcbb1756 major bug fix for function adsb.position_with_ref() 2017-03-07 10:22:53 +01:00
Junzi Sun
b9c6db6f65 fix error in surface position with reference 2016-11-10 13:45:36 +01:00
Junzi Sun
220b8e9716 update setup and test code 2016-10-26 21:03:14 +02:00
Junzi Sun
3691d6f73d fix vertical rate, scale 64 times 2016-10-26 20:52:33 +02:00
Junzi Sun
dad1cd89a9 Merge pull request #8 from rwnobrega/patch-1
Fix typos and remove redundant info in README.rst
2016-10-26 14:49:40 +02:00
Roberto Nobrega
3b3fc27a42 Fix typos and remove redundant info in README.rst 2016-10-25 17:26:09 -02:00
junzis
4bafa1de19 complete surface position decoding 2016-10-19 16:22:28 +02:00
junzis
b648f4e7a5 add EHS BDS44 decoding (not reliable though...) 2016-10-05 17:37:50 +02:00
junzis
a08c91a3a1 fix imports again and rename files 2016-10-05 15:40:56 +02:00
junzis
567fcda931 make tox to /tmp 2016-10-03 22:34:42 +02:00
Junzi Sun
56dbb618c6 use relative imports within pyModeS package 2016-10-03 21:31:22 +02:00
Junzi Sun
58447346aa Merge pull request #7 from watterso/watterso_refactor_automated_testing_merge
merge in watterso_setup_automated_testing
2016-10-03 21:29:50 +02:00
Junzi Sun
bccc319856 Merge branch 'master' of github.com:junzis/pyModeS 2016-10-03 21:18:41 +02:00
Junzi Sun
375041717b ehs new function 2016-10-03 21:18:17 +02:00
James Watterson
23192a97fd merge in watterso_setup_automated_testing
added .idea to .gitignore for pycharm
pulled tests out of run.py, created adsb_test, ehs_test, and util test
moved the rest of runp.py into decode_test_data
changed imports and __init__ file so it doesn't contain magic
2016-09-11 20:48:43 -07:00
Junzi Sun
240f706e81 update BDS(msg) docstring 2016-08-23 23:02:56 +02:00
junzis
168acfb88d update README and docs 2016-08-16 17:07:02 +02:00
junzis
70e9aa7c8d update docstrings 2016-08-16 16:59:11 +02:00
junzis
fc286299ec fix docstrings 2016-08-16 16:48:13 +02:00
junzis
700b290047 remove doc theme 2016-08-16 16:40:27 +02:00
junzis
55fbdcd029 rename doc files 2016-08-16 16:36:55 +02:00
55 changed files with 14465 additions and 3236 deletions

4
.gitignore vendored
View File

@@ -3,6 +3,7 @@
# Byte-compiled / optimized / DLL files
__pycache__/
*.py[cod]
.pytest_cache/
# C extensions
*.so
@@ -54,3 +55,6 @@ docs/_build/
# PyBuilder
target/
# PyCharm
.idea/

View File

@@ -1,109 +1,255 @@
A Python Mode-S Decoder
=======================
The Python ADS-B/Mode-S Decoder
==========================================
Python library for Mode-S message decoding. Two seprate methods are
develop to decode the following messages:
Python library for ADS-B/Mode-S message decoding. Supported Downlink Formats (DF) are:
- Automatic Dependent Surveillance - Broadcast (ADS-B) (DF17)
**DF17 / DF18: Automatic Dependent Surveillance - Broadcast (ADS-B)**
- aircraft infomation that cotains: icao address, position,
altitude, velocity (ground speed), and callsign, etc.
- TC=1-4 / BDS 0,8: Aircraft identification and category
- TC=5-8 / BDS 0,6: Surface position
- TC=9-18 / BDS 0,5: Airborne position
- TC=19 / BDS 0,9: Airborne velocity
- TC=28 / BDS 6,1: Airborne status [to be implemented]
- TC=29 / BDS 6,2: Target state and status information [to be implemented]
- TC=31 / BDS 6,5: Aircraft operational status [to be implemented]
- Mode-S Enhanced Surveillance (EHS) (DF20 and DF21)
- additional information in response to SSR interogation, such as:
true airspeed, indicated airspeed, mach number, track angle,
heading, and roll angle, etc.
**DF20 / DF21: Mode-S Comm-B replies**
A detailed manuel on Mode-S decoding is published by the author, at:
http://adsb-decode-guide.readthedocs.org
- BDS 1,0: Data link capability report
- BDS 1,7: Common usage GICB capability report
- BDS 2,0: Aircraft identification
- BDS 2,1: Aircraft and airline registration markings
- BDS 3,0: ACAS active resolution advisory
- BDS 4,0: Selected vertical intention
- BDS 4,4: Meteorological routine air report
- BDS 5,0: Track and turn report
- BDS 5,3: Air-referenced state vector
- BDS 6,0: Heading and speed report
**DF4 / DF20: Altitude code**
**DF5 / DF21: Identity code (squawk code)**
Detailed manual on Mode-S decoding is published by the author, at:
https://mode-s.org/decode
New features in v2.0
---------------------
- New structure of the libraries
- ADS-B and Comm-B data streaming
- Active aircraft viewing (terminal curses)
- Improved BDS identification
- Optimizing decoding speed
Source code
-----------
Checkourt and contribute to this open source project at:
Checkout and contribute to this open-source project at:
https://github.com/junzis/pyModeS
API documentation at:
http://pymodes.readthedocs.io
[To be updated]
Install
-------
Checkout source code, or install using pip:
To install latest version from the GitHub:
::
pip install pyModeS
pip install git+https://github.com/junzis/pyModeS
Usage
-----
To install the stable version (2.0) from pip:
::
pip install pyModeS
Live view traffic (modeslive)
----------------------------------------------------
Supports **Mode-S Beast** and **AVR** raw stream
::
modeslive --server [server_address] --port [tcp_port] --rawtype [beast,avr,skysense] --latlon [lat] [lon] --dumpto [folder]
Arguments:
-h, --help show this help message and exit
--server SERVER server address or IP
--port PORT raw data port
--rawtype RAWTYPE beast, avr or skysense
--latlon LAT LON receiver position
--show-uncertainty display uncertaint values, default off
--dumpto folder to dump decoded output
If you have a RTL-SDR receiver or Mode-S Beast, use modesmixer2 (http://xdeco.org/?page_id=48) to create raw beast TCP stream:
::
$ modesmixer2 --inSeriel port[:speed[:flow_control]] --outServer beast:[tcp_port]
Example screenshot:
.. image:: https://github.com/junzis/pyModeS/raw/master/doc/modeslive-screenshot.png
:width: 700px
Use the library
---------------
.. code:: python
import pyModeS as pms
import pyModeS as pms
Common function for Mode-S message:
Common functions
*****************
.. code:: python
pms.df(msg) # Downlink Format
pms.crc(msg, encode=False) # Perform CRC or generate parity bit
pms.df(msg) # Downlink Format
pms.icao(msg) # Infer the ICAO address from the message
pms.crc(msg, encode=False) # Perform CRC or generate parity bit
pms.hex2bin(str) # Convert hexadecimal string to binary string
pms.bin2int(str) # Convert binary string to integer
pms.hex2int(str) # Convert hexadecimal string to integer
pms.hex2bin(str) # Convert hexadecimal string to binary string
pms.bin2int(str) # Convert binary string to integer
pms.hex2int(str) # Convert hexadecimal string to integer
pms.gray2int(str) # Convert grey code to interger
Core functions for ADS-B decoding:
Core functions for ADS-B decoding
*********************************
.. code:: python
pms.adsb.icao(msg)
pms.adsb.callsign(msg)
pms.adsb.position(msg_even, msg_odd, t_even, t_odd)
pms.adsb.position_with_ref(msg, lat_ref, lon_ref)
pms.adsb.altitude(msg)
pms.adsb.velocity(msg)
pms.adsb.speed_heading(msg)
pms.adsb.icao(msg)
pms.adsb.typecode(msg)
**Hint: When you have a fix position of the aircraft or you know the
location of your receiver, it is convinent to use `position_with_ref()` method
to decode with only one position message (either odd or even)**
# Typecode 1-4
pms.adsb.callsign(msg)
Core functions for EHS decoding:
# Typecode 5-8 (surface), 9-18 (airborne, barometric height), and 9-18 (airborne, GNSS height)
pms.adsb.position(msg_even, msg_odd, t_even, t_odd, lat_ref=None, lon_ref=None)
pms.adsb.airborne_position(msg_even, msg_odd, t_even, t_odd)
pms.adsb.surface_position(msg_even, msg_odd, t_even, t_odd, lat_ref, lon_ref)
pms.adsb.position_with_ref(msg, lat_ref, lon_ref)
pms.adsb.airborne_position_with_ref(msg, lat_ref, lon_ref)
pms.adsb.surface_position_with_ref(msg, lat_ref, lon_ref)
pms.adsb.altitude(msg)
# Typecode: 19
pms.adsb.velocity(msg) # Handles both surface & airborne messages
pms.adsb.speed_heading(msg) # Handles both surface & airborne messages
pms.adsb.surface_velocity(msg)
pms.adsb.airborne_velocity(msg)
Note: When you have a fix position of the aircraft, it is convenient to
use `position_with_ref()` method to decode with only one position message
(either odd or even). This works with both airborne and surface position
messages. But the reference position shall be with in 180NM (airborne)
or 45NM (surface) of the true position.
Decode altitude replies in DF4 / DF20
**************************************
.. code:: python
pms.common.altcode(msg) # Downlink format must be 4 or 20
Decode identity replies in DF5 / DF21
**************************************
.. code:: python
pms.common.idcode(msg) # Downlink format must be 5 or 21
Common Mode-S functions
************************
.. code:: python
pms.ehs.icao(msg) # icao address
pms.ehs.BDS(msg) # Comm-B Data Selector Version
pms.icao(msg) # Infer the ICAO address from the message
pms.bds.infer(msg) # Infer the Modes-S BDS register
# for BDS version 2,0
pms.ehs.callsign(msg) # Aircraft callsign
# Check if BDS is 5,0 or 6,0, give reference speed, track, altitude (from ADS-B)
pms.bds.is50or60(msg, spd_ref, trk_ref, alt_ref)
# for BDS version 4,0
pms.ehs.alt_mcp(msg) # MCP/FCU selected altitude (ft)
pms.ehs.alt_fms(msg) # FMS selected altitude (ft)
pms.ehs.alt_pbaro(msg) # Barometric pressure (mb)
# Check each BDS explicitly
pms.bds.bds10.is10(msg)
pms.bds.bds17.is17(msg)
pms.bds.bds20.is20(msg)
pms.bds.bds30.is30(msg)
pms.bds.bds40.is40(msg)
pms.bds.bds44.is44(msg)
pms.bds.bds50.is50(msg)
pms.bds.bds60.is60(msg)
# for BDS version 5,0
pms.ehs.roll(msg) # roll angle (deg)
pms.ehs.track(msg) # track angle (deg)
pms.ehs.gs(msg) # ground speed (kt)
pms.ehs.rtrack(msg) # track angle rate (deg/sec)
pms.ehs.tas(msg) # true airspeed (kt)
# for BDS version 6,0
pms.ehs.heading(msg) # heading (deg)
pms.ehs.ias(msg) # indicated airspeed (kt)
pms.ehs.mach(msg) # MACH number
pms.ehs.baro_vr(msg) # barometric altitude rate (ft/min)
pms.ehs.ins_vr(msg) # inertial vertical speed (ft/min)
Some helper functions:
Mode-S Elementary Surveillance (ELS)
*************************************
.. code:: python
pms.df(msg) # downlink format of a Mode-S message
pms.hex2bin(msg) # convert hexadecimal string to binary string
pms.hex2int(msg) # convert hexadecimal string to integer
pms.bin2int(msg) # convert binary string to integer
pms.commb.ovc10(msg) # Overlay capability, BDS 1,0
pms.commb.cap17(msg) # GICB capability, BDS 1,7
pms.commb.cs20(msg) # Callsign, BDS 2,0
Mode-S Enhanced Surveillance (EHS)
***********************************
.. code:: python
# For BDS register 4,0
pms.commb.alt40mcp(msg) # MCP/FCU selected altitude (ft)
pms.commb.alt40fms(msg) # FMS selected altitude (ft)
pms.commb.p40baro(msg) # Barometric pressure (mb)
# For BDS register 5,0
pms.commb.roll50(msg) # Roll angle (deg)
pms.commb.trk50(msg) # True track angle (deg)
pms.commb.gs50(msg) # Ground speed (kt)
pms.commb.rtrk50(msg) # Track angle rate (deg/sec)
pms.commb.tas50(msg) # True airspeed (kt)
# For BDS register 6,0
pms.commb.hdg60(msg) # Magnetic heading (deg)
pms.commb.ias60(msg) # Indicated airspeed (kt)
pms.commb.mach60(msg) # Mach number (-)
pms.commb.vr60baro(msg) # Barometric altitude rate (ft/min)
pms.commb.vr60ins(msg) # Inertial vertical speed (ft/min)
Meteorological routine air report (MRAR) [Experimental]
*******************************************************
.. code:: python
# For BDS register 4,4
pms.commb.wind44(msg, rev=False) # Wind speed (kt) and direction (true) (deg)
pms.commb.temp44(msg, rev=False) # Static air temperature (C)
pms.commb.p44(msg, rev=False) # Average static pressure (hPa)
pms.commb.hum44(msg, rev=False) # Humidity (%)
Developement
------------
To perform unit tests. First install ``tox`` through pip, Then, run the following commands:
.. code:: bash
$ tox

View File

@@ -50,7 +50,7 @@ source_suffix = '.rst'
# source_encoding = 'utf-8-sig'
# The master toctree document.
master_doc = 'pyModeS'
master_doc = 'index'
# General information about the project.
project = u'pyModeS'
@@ -124,7 +124,7 @@ todo_include_todos = True
# The theme to use for HTML and HTML Help pages. See the documentation for
# a list of builtin themes.
#
html_theme = 'alabaster'
# html_theme = 'alabaster'
# Theme options are theme-specific and customize the look and feel of a theme
# further. For a list of options available for each theme, see the

View File

@@ -4,9 +4,13 @@
contain the root `toctree` directive.
pyModeS API documents
pyModeS APIs
=====================
This document contains all the functions within pyModeS package.
Source code and user guide: https://github.com/junzis/pyModeS
pyModeS.adsb module
-------------------

Binary file not shown.

After

Width:  |  Height:  |  Size: 98 KiB

View File

@@ -1 +1 @@
pyModeS==1.0.5
pyModeS==1.1.0

View File

@@ -1,5 +1,15 @@
from __future__ import absolute_import, print_function, division
from .util import *
from . import adsb
from . import ehs
from .decoder.common import *
from .decoder import adsb
from .decoder import commb
from .decoder import common
from .decoder import bds
from .extra import aero
from .extra import tcpclient
# from .decoder import els # depricated
# from .decoder import ehs # depricated
import os
dirpath = os.path.dirname(os.path.realpath(__file__))

View File

@@ -1,461 +0,0 @@
"""
A python package for decoding ABS-D messages.
Copyright (C) 2015 Junzi Sun (TU Delft)
This program is free software: you can redistribute it and/or modify
it under the terms of the GNU General Public License as published by
the Free Software Foundation, either version 3 of the License, or
(at your option) any later version.
This program is distributed in the hope that it will be useful,
but WITHOUT ANY WARRANTY; without even the implied warranty of
MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
GNU General Public License for more details.
You should have received a copy of the GNU General Public License
along with this program. If not, see <http://www.gnu.org/licenses/>.
"""
import math
from . import util
from .util import crc
def df(msg):
"""Get the downlink format (DF) number
Args:
msg (string): 28 bytes hexadecimal message string
Returns:
int: DF number
"""
return util.df(msg)
def icao(msg):
"""Get the ICAO 24 bits address, bytes 3 to 8.
Args:
msg (string): 28 bytes hexadecimal message string
Returns:
String: ICAO address in 6 bytes hexadecimal string
"""
return msg[2:8]
def data(msg):
"""Return the data frame in the message, bytes 9 to 22"""
return msg[8:22]
def typecode(msg):
"""Type code of ADS-B message
Args:
msg (string): 28 bytes hexadecimal message string
Returns:
int: type code number
"""
msgbin = util.hex2bin(msg)
return util.bin2int(msgbin[32:37])
# ---------------------------------------------
# Aircraft Identification
# ---------------------------------------------
def category(msg):
"""Aircraft category number
Args:
msg (string): 28 bytes hexadecimal message string
Returns:
int: category number
"""
if typecode(msg) < 1 or typecode(msg) > 4:
raise RuntimeError("%s: Not a identification message" % msg)
msgbin = util.hex2bin(msg)
return util.bin2int(msgbin[5:8])
def callsign(msg):
"""Aircraft callsign
Args:
msg (string): 28 bytes hexadecimal message string
Returns:
string: callsign
"""
if typecode(msg) < 1 or typecode(msg) > 4:
raise RuntimeError("%s: Not a identification message" % msg)
chars = '#ABCDEFGHIJKLMNOPQRSTUVWXYZ#####_###############0123456789######'
msgbin = util.hex2bin(msg)
csbin = msgbin[40:96]
cs = ''
cs += chars[util.bin2int(csbin[0:6])]
cs += chars[util.bin2int(csbin[6:12])]
cs += chars[util.bin2int(csbin[12:18])]
cs += chars[util.bin2int(csbin[18:24])]
cs += chars[util.bin2int(csbin[24:30])]
cs += chars[util.bin2int(csbin[30:36])]
cs += chars[util.bin2int(csbin[36:42])]
cs += chars[util.bin2int(csbin[42:48])]
# clean string, remove spaces and marks, if any.
# cs = cs.replace('_', '')
cs = cs.replace('#', '')
return cs
# ---------------------------------------------
# Positions
# ---------------------------------------------
def oe_flag(msg):
"""Check the odd/even flag. Bit 54, 0 for even, 1 for odd.
Args:
msg (string): 28 bytes hexadecimal message string
Returns:
int: 0 or 1, for even or odd frame
"""
if typecode(msg) < 5 or typecode(msg) > 18:
raise RuntimeError("%s: Not a position message" % msg)
msgbin = util.hex2bin(msg)
return int(msgbin[53])
def cprlat(msg):
"""CPR encoded latitude
Args:
msg (string): 28 bytes hexadecimal message string
Returns:
int: encoded latitude
"""
if typecode(msg) < 5 or typecode(msg) > 18:
raise RuntimeError("%s: Not a position message" % msg)
msgbin = util.hex2bin(msg)
return util.bin2int(msgbin[54:71])
def cprlon(msg):
"""CPR encoded longitude
Args:
msg (string): 28 bytes hexadecimal message string
Returns:
int: encoded longitude
"""
if typecode(msg) < 5 or typecode(msg) > 18:
raise RuntimeError("%s: Not a position message" % msg)
msgbin = util.hex2bin(msg)
return util.bin2int(msgbin[71:88])
def position(msg0, msg1, t0, t1):
if (5 <= typecode(msg0) <= 8 and 5 <= typecode(msg1) <= 8):
return surface_position(msg0, msg1, t0, t1)
elif (9 <= typecode(msg0) <= 18 and 9 <= typecode(msg1) <= 18):
return airborne_position(msg0, msg1, t0, t1)
else:
raise RuntimeError("incorrect or inconsistant message types")
def airborne_position(msg0, msg1, t0, t1):
"""Decode airborn position from a pair of even and odd position message
131072 is 2^17, since CPR lat and lon are 17 bits each.
Args:
msg0 (string): even message (28 bytes hexadecimal string)
msg1 (string): odd message (28 bytes hexadecimal string)
t0 (int): timestamps for the even message
t1 (int): timestamps for the odd message
Returns:
(float, float): (latitude, longitude) of the aircraft
"""
msgbin0 = util.hex2bin(msg0)
msgbin1 = util.hex2bin(msg1)
cprlat_even = util.bin2int(msgbin0[54:71]) / 131072.0
cprlon_even = util.bin2int(msgbin0[71:88]) / 131072.0
cprlat_odd = util.bin2int(msgbin1[54:71]) / 131072.0
cprlon_odd = util.bin2int(msgbin1[71:88]) / 131072.0
air_d_lat_even = 360.0 / 60
air_d_lat_odd = 360.0 / 59
# compute latitude index 'j'
j = util.floor(59 * cprlat_even - 60 * cprlat_odd + 0.5)
lat_even = float(air_d_lat_even * (j % 60 + cprlat_even))
lat_odd = float(air_d_lat_odd * (j % 59 + cprlat_odd))
if lat_even >= 270:
lat_even = lat_even - 360
if lat_odd >= 270:
lat_odd = lat_odd - 360
# check if both are in the same latidude zone, exit if not
if _cprNL(lat_even) != _cprNL(lat_odd):
return None
# compute ni, longitude index m, and longitude
if (t0 > t1):
ni = max(_cprNL(lat_even), 1)
m = util.floor(cprlon_even * (_cprNL(lat_even)-1) -
cprlon_odd * _cprNL(lat_even) + 0.5)
lon = (360.0 / ni) * (m % ni + cprlon_even)
lat = lat_even
else:
ni = max(_cprNL(lat_odd) - 1, 1)
m = util.floor(cprlon_even * (_cprNL(lat_odd)-1) -
cprlon_odd * _cprNL(lat_odd) + 0.5)
lon = (360.0 / ni) * (m % ni + cprlon_odd)
lat = lat_odd
if lon > 180:
lon = lon - 360
return round(lat, 5), round(lon, 5)
def position_with_ref(msg, lat_ref, lon_ref):
if 5 <= typecode(msg) <= 8:
return airborne_position_with_ref(msg, lat_ref, lon_ref)
elif 9 <= typecode(msg) <= 18:
return surface_position_with_ref(msg, lat_ref, lon_ref)
else:
raise RuntimeError("incorrect or inconsistant message types")
def airborne_position_with_ref(msg, lat_ref, lon_ref):
"""Decode airborn position with one message,
knowing previous reference location
Args:
msg (string): even message (28 bytes hexadecimal string)
lat_ref: previous known latitude
lon_ref: previous known longitude
Returns:
(float, float): (latitude, longitude) of the aircraft
"""
i = oe_flag(msg)
d_lat = 360.0/59 if i else 360.0/60
msgbin = util.hex2bin(msg)
cprlat = util.bin2int(msgbin[54:71]) / 131072.0
cprlon = util.bin2int(msgbin[71:88]) / 131072.0
j = util.floor(lat_ref / d_lat) \
+ util.floor(0.5 + ((lat_ref % d_lat) / d_lat) - cprlat)
lat = d_lat * (j + cprlat)
ni = _cprNL(lat) - i
if ni > 0:
d_lon = 360.0 / ni
else:
d_lon = 360.0
m = util.floor(lon_ref / d_lon) \
+ util.floor(0.5 + ((lon_ref % d_lon) / d_lon) - cprlon)
lon = d_lon * (m + cprlon)
return round(lat, 5), round(lon, 5)
def surface_position(msg0, msg1, t0, t1):
# TODO: implement surface positon
raise RuntimeError('suface position decoding to be implemented soon...')
def surface_position_with_ref(msg, lat_ref, lon_ref):
"""Decode surface position with one message,
knowing reference nearby location, such as previously calculated location,
ground station, or airport location, etc.
Args:
msg (string): even message (28 bytes hexadecimal string)
lat_ref: previous known latitude
lon_ref: previous known longitude
Returns:
(float, float): (latitude, longitude) of the aircraft
"""
i = oe_flag(msg)
d_lat = 90.0/59 if i else 90.0/60
msgbin = util.hex2bin(msg)
cprlat = util.bin2int(msgbin[54:71]) / 131072.0
cprlon = util.bin2int(msgbin[71:88]) / 131072.0
j = util.floor(lat_ref / d_lat) \
+ util.floor(0.5 + ((lat_ref % d_lat) / d_lat) - cprlat)
lat = d_lat * (j + cprlat)
ni = _cprNL(lat) - i
if ni > 0:
d_lon = 360.0 / ni
else:
d_lon = 360.0
m = util.floor(lon_ref / d_lon) \
+ util.floor(0.5 + ((lon_ref % d_lon) / d_lon) - cprlon)
lon = d_lon * (m + cprlon)
return round(lat, 5), round(lon, 5)
def _cprNL(lat):
if lat == 0:
return 59
if lat == 87 or lat == -87:
return 2
if lat > 87 or lat < -87:
return 1
nz = 15
a = 1 - math.cos(math.pi / (2 * nz))
b = math.cos(math.pi / 180.0 * abs(lat)) ** 2
nl = 2 * math.pi / (math.acos(1 - a/b))
NL = util.floor(nl)
return NL
def altitude(msg):
"""Decode aircraft altitude
Args:
msg (string): 28 bytes hexadecimal message string
Returns:
int: altitude in feet
"""
if typecode(msg) < 9 or typecode(msg) > 18:
raise RuntimeError("%s: Not a position message" % msg)
msgbin = util.hex2bin(msg)
q = msgbin[47]
if q:
n = util.bin2int(msgbin[40:47]+msgbin[48:52])
alt = n * 25 - 1000
return alt
else:
return None
def nic(msg):
"""Calculate NIC, navigation integrity category
Args:
msg (string): 28 bytes hexadecimal message string
Returns:
int: NIC number (from 0 to 11), -1 if not applicable
"""
if typecode(msg) < 9 or typecode(msg) > 18:
raise RuntimeError("%s: Not a airborne position message" % msg)
msgbin = util.hex2bin(msg)
tc = typecode(msg)
nic_sup_b = util.bin2int(msgbin[39])
if tc in [0, 18, 22]:
nic = 0
elif tc == 17:
nic = 1
elif tc == 16:
if nic_sup_b:
nic = 3
else:
nic = 2
elif tc == 15:
nic = 4
elif tc == 14:
nic = 5
elif tc == 13:
nic = 6
elif tc == 12:
nic = 7
elif tc == 11:
if nic_sup_b:
nic = 9
else:
nic = 8
elif tc in [10, 21]:
nic = 10
elif tc in [9, 20]:
nic = 11
else:
nic = -1
return nic
# ---------------------------------------------
# Velocity
# ---------------------------------------------
def velocity(msg):
"""Calculate the speed, heading, and vertical rate
Args:
msg (string): 28 bytes hexadecimal message string
Returns:
(int, float, int, string): speed (kt), heading (degree),
rate of climb/descend (ft/min), and speed type
('GS' for ground speed, 'AS' for airspeed)
"""
if typecode(msg) != 19:
raise RuntimeError("%s: Not a airborne velocity message" % msg)
msgbin = util.hex2bin(msg)
subtype = util.bin2int(msgbin[37:40])
if subtype in (1, 2):
v_ew_sign = util.bin2int(msgbin[45])
v_ew = util.bin2int(msgbin[46:56]) - 1 # east-west velocity
v_ns_sign = util.bin2int(msgbin[56])
v_ns = util.bin2int(msgbin[57:67]) - 1 # north-south velocity
v_we = -1*v_ew if v_ew_sign else v_ew
v_sn = -1*v_ns if v_ns_sign else v_ns
spd = math.sqrt(v_sn*v_sn + v_we*v_we) # unit in kts
hdg = math.atan2(v_we, v_sn)
hdg = math.degrees(hdg) # convert to degrees
hdg = hdg if hdg >= 0 else hdg + 360 # no negative val
tag = 'GS'
else:
hdg = util.bin2int(msgbin[46:56]) / 1024.0 * 360.0
spd = util.bin2int(msgbin[57:67])
tag = 'AS'
vr_sign = util.bin2int(msgbin[68])
vr = util.bin2int(msgbin[69:78]) # vertical rate
rocd = -1*vr if vr_sign else vr # rate of climb/descend
return int(spd), round(hdg, 1), int(rocd), tag
def speed_heading(msg):
"""Get speed and heading only from the velocity message
Args:
msg (string): 28 bytes hexadecimal message string
Returns:
(int, float): speed (kt), heading (degree)
"""
spd, hdg, rocd, tag = velocity(msg)
return spd, hdg

View File

@@ -0,0 +1,3 @@
from __future__ import absolute_import, print_function, division
from pyModeS.decoder import *

21
pyModeS/decoder/acas.py Normal file
View File

@@ -0,0 +1,21 @@
# Copyright (C) 2018 Junzi Sun (TU Delft)
# This program is free software: you can redistribute it and/or modify
# it under the terms of the GNU General Public License as published by
# the Free Software Foundation, either version 3 of the License, or
# (at your option) any later version.
# This program is distributed in the hope that it will be useful,
# but WITHOUT ANY WARRANTY; without even the implied warranty of
# MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
# GNU General Public License for more details.
# You should have received a copy of the GNU General Public License
# along with this program. If not, see <http://www.gnu.org/licenses/>.
"""
Decoding Air-Air Surveillance (ACAS) DF=0/16
"""
from __future__ import absolute_import, print_function, division
from pyModeS.decoder import common

500
pyModeS/decoder/adsb.py Normal file
View File

@@ -0,0 +1,500 @@
# Copyright (C) 2015 Junzi Sun (TU Delft)
# This program is free software: you can redistribute it and/or modify
# it under the terms of the GNU General Public License as published by
# the Free Software Foundation, either version 3 of the License, or
# (at your option) any later version.
# This program is distributed in the hope that it will be useful,
# but WITHOUT ANY WARRANTY; without even the implied warranty of
# MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
# GNU General Public License for more details.
# You should have received a copy of the GNU General Public License
# along with this program. If not, see <http://www.gnu.org/licenses/>.
"""
The wrapper for decoding ADS-B messages
"""
from __future__ import absolute_import, print_function, division
import pyModeS as pms
from pyModeS.decoder import common
from pyModeS.decoder import uncertainty
# from pyModeS.decoder.bds import bds05, bds06, bds09
from pyModeS.decoder.bds.bds05 import airborne_position, airborne_position_with_ref, altitude
from pyModeS.decoder.bds.bds06 import surface_position, surface_position_with_ref, surface_velocity
from pyModeS.decoder.bds.bds08 import category, callsign
from pyModeS.decoder.bds.bds09 import airborne_velocity, altitude_diff
def df(msg):
return common.df(msg)
def icao(msg):
return common.icao(msg)
def typecode(msg):
return common.typecode(msg)
def position(msg0, msg1, t0, t1, lat_ref=None, lon_ref=None):
"""Decode position from a pair of even and odd position message
(works with both airborne and surface position messages)
Args:
msg0 (string): even message (28 bytes hexadecimal string)
msg1 (string): odd message (28 bytes hexadecimal string)
t0 (int): timestamps for the even message
t1 (int): timestamps for the odd message
Returns:
(float, float): (latitude, longitude) of the aircraft
"""
tc0 = typecode(msg0)
tc1 = typecode(msg1)
if (5<=tc0<=8 and 5<=tc1<=8):
if (not lat_ref) or (not lon_ref):
raise RuntimeError("Surface position encountered, a reference \
position lat/lon required. Location of \
receiver can be used.")
else:
return surface_position(msg0, msg1, t0, t1, lat_ref, lon_ref)
elif (9<=tc0<=18 and 9<=tc1<=18):
# Airborne position with barometric height
return airborne_position(msg0, msg1, t0, t1)
elif (20<=tc0<=22 and 20<=tc1<=22):
# Airborne position with GNSS height
return airborne_position(msg0, msg1, t0, t1)
else:
raise RuntimeError("incorrect or inconsistant message types")
def position_with_ref(msg, lat_ref, lon_ref):
"""Decode position with only one message,
knowing reference nearby location, such as previously
calculated location, ground station, or airport location, etc.
Works with both airborne and surface position messages.
The reference position shall be with in 180NM (airborne) or 45NM (surface)
of the true position.
Args:
msg (string): even message (28 bytes hexadecimal string)
lat_ref: previous known latitude
lon_ref: previous known longitude
Returns:
(float, float): (latitude, longitude) of the aircraft
"""
tc = typecode(msg)
if 5<=tc<=8:
return surface_position_with_ref(msg, lat_ref, lon_ref)
elif 9<=tc<=18 or 20<=tc<=22:
return airborne_position_with_ref(msg, lat_ref, lon_ref)
else:
raise RuntimeError("incorrect or inconsistant message types")
def altitude(msg):
"""Decode aircraft altitude
Args:
msg (string): 28 bytes hexadecimal message string
Returns:
int: altitude in feet
"""
tc = typecode(msg)
if tc<5 or tc==19 or tc>22:
raise RuntimeError("%s: Not a position message" % msg)
if tc>=5 and tc<=8:
# surface position, altitude 0
return 0
msgbin = common.hex2bin(msg)
q = msgbin[47]
if q:
n = common.bin2int(msgbin[40:47]+msgbin[48:52])
alt = n * 25 - 1000
return alt
else:
return None
def velocity(msg):
"""Calculate the speed, heading, and vertical rate
(handles both airborne or surface message)
Args:
msg (string): 28 bytes hexadecimal message string
Returns:
(int, float, int, string): speed (kt), ground track or heading (degree),
rate of climb/descend (ft/min), and speed type
('GS' for ground speed, 'AS' for airspeed)
"""
if 5 <= typecode(msg) <= 8:
return surface_velocity(msg)
elif typecode(msg) == 19:
return airborne_velocity(msg)
else:
raise RuntimeError("incorrect or inconsistant message types, expecting 4<TC<9 or TC=19")
def speed_heading(msg):
"""Get speed and ground track (or heading) from the velocity message
(handles both airborne or surface message)
Args:
msg (string): 28 bytes hexadecimal message string
Returns:
(int, float): speed (kt), ground track or heading (degree)
"""
spd, trk_or_hdg, rocd, tag = velocity(msg)
return spd, trk_or_hdg
def oe_flag(msg):
"""Check the odd/even flag. Bit 54, 0 for even, 1 for odd.
Args:
msg (string): 28 bytes hexadecimal message string
Returns:
int: 0 or 1, for even or odd frame
"""
msgbin = common.hex2bin(msg)
return int(msgbin[53])
def version(msg):
"""ADS-B Version
Args:
msg (string): 28 bytes hexadecimal message string, TC = 31
Returns:
int: version number
"""
tc = typecode(msg)
if tc != 31:
raise RuntimeError("%s: Not a status operation message, expecting TC = 31" % msg)
msgbin = common.hex2bin(msg)
version = common.bin2int(msgbin[72:75])
return version
def nuc_p(msg):
"""Calculate NUCp, Navigation Uncertainty Category - Position (ADS-B version 1)
Args:
msg (string): 28 bytes hexadecimal message string,
Returns:
int: Horizontal Protection Limit
int: 95% Containment Radius - Horizontal (meters)
int: 95% Containment Radius - Vertical (meters)
"""
tc = typecode(msg)
if typecode(msg) < 5 or typecode(msg) > 22:
raise RuntimeError(
"%s: Not a surface position message (5<TC<8), \
airborne position message (8<TC<19), \
or airborne position with GNSS height (20<TC<22)" % msg
)
try:
NUCp = uncertainty.TC_NUCp_lookup[tc]
HPL = uncertainty.NUCp[NUCp]['HPL']
RCu = uncertainty.NUCp[NUCp]['RCu']
RCv = uncertainty.NUCp[NUCp]['RCv']
except KeyError:
HPL, RCu, RCv = uncertainty.NA, uncertainty.NA, uncertainty.NA
if tc in [20, 21]:
RCv = uncertainty.NA
return HPL, RCu, RCv
def nuc_v(msg):
"""Calculate NUCv, Navigation Uncertainty Category - Velocity (ADS-B version 1)
Args:
msg (string): 28 bytes hexadecimal message string,
Returns:
int or string: 95% Horizontal Velocity Error
int or string: 95% Vertical Velocity Error
"""
tc = typecode(msg)
if tc != 19:
raise RuntimeError("%s: Not an airborne velocity message, expecting TC = 19" % msg)
msgbin = common.hex2bin(msg)
NUCv = common.bin2int(msgbin[42:45])
try:
HVE = uncertainty.NUCv[NUCv]['HVE']
VVE = uncertainty.NUCv[NUCv]['VVE']
except KeyError:
HVE, VVE = uncertainty.NA, uncertainty.NA
return HVE, VVE
def nic_v1(msg, NICs):
"""Calculate NIC, navigation integrity category, for ADS-B version 1
Args:
msg (string): 28 bytes hexadecimal message string
NICs (int or string): NIC supplement
Returns:
int or string: Horizontal Radius of Containment
int or string: Vertical Protection Limit
"""
if typecode(msg) < 5 or typecode(msg) > 22:
raise RuntimeError(
"%s: Not a surface position message (5<TC<8), \
airborne position message (8<TC<19), \
or airborne position with GNSS height (20<TC<22)" % msg
)
tc = typecode(msg)
NIC = uncertainty.TC_NICv1_lookup[tc]
if isinstance(NIC, dict):
NIC = NIC[NICs]
try:
Rc = uncertainty.NICv1[NIC][NICs]['Rc']
VPL = uncertainty.NICv1[NIC][NICs]['VPL']
except KeyError:
Rc, VPL = uncertainty.NA, uncertainty.NA
return Rc, VPL
def nic_v2(msg, NICa, NICbc):
"""Calculate NIC, navigation integrity category, for ADS-B version 2
Args:
msg (string): 28 bytes hexadecimal message string
NICa (int or string): NIC supplement - A
NICbc (int or srting): NIC supplement - B or C
Returns:
int or string: Horizontal Radius of Containment
"""
if typecode(msg) < 5 or typecode(msg) > 22:
raise RuntimeError(
"%s: Not a surface position message (5<TC<8), \
airborne position message (8<TC<19), \
or airborne position with GNSS height (20<TC<22)" % msg
)
tc = typecode(msg)
NIC = uncertainty.TC_NICv2_lookup[tc]
if 20<=tc<=22:
NICs = 0
else:
NICs = NICa*2 + NICbc
try:
if isinstance(NIC, dict):
NIC = NIC[NICs]
Rc = uncertainty.NICv2[NIC][NICs]['Rc']
except KeyError:
Rc = uncertainty.NA
return Rc
def nic_s(msg):
"""Obtain NIC supplement bit, TC=31 message
Args:
msg (string): 28 bytes hexadecimal message string
Returns:
int: NICs number (0 or 1)
"""
tc = typecode(msg)
if tc != 31:
raise RuntimeError("%s: Not a status operation message, expecting TC = 31" % msg)
msgbin = common.hex2bin(msg)
nic_s = int(msgbin[75])
return nic_s
def nic_a_c(msg):
"""Obtain NICa/c, navigation integrity category supplements a and c
Args:
msg (string): 28 bytes hexadecimal message string
Returns:
(int, int): NICa and NICc number (0 or 1)
"""
tc = typecode(msg)
if tc != 31:
raise RuntimeError("%s: Not a status operation message, expecting TC = 31" % msg)
msgbin = common.hex2bin(msg)
nic_a = int(msgbin[75])
nic_c = int(msgbin[51])
return nic_a, nic_c
def nic_b(msg):
"""Obtain NICb, navigation integrity category supplement-b
Args:
msg (string): 28 bytes hexadecimal message string
Returns:
int: NICb number (0 or 1)
"""
tc = typecode(msg)
if tc < 9 or tc > 18:
raise RuntimeError("%s: Not a airborne position message, expecting 8<TC<19" % msg)
msgbin = common.hex2bin(msg)
nic_b = int(msgbin[39])
return nic_b
def nac_p(msg):
"""Calculate NACp, Navigation Accuracy Category - Position
Args:
msg (string): 28 bytes hexadecimal message string, TC = 29 or 31
Returns:
int or string: 95% horizontal accuracy bounds, Estimated Position Uncertainty
int or string: 95% vertical accuracy bounds, Vertical Estimated Position Uncertainty
"""
tc = typecode(msg)
if tc not in [29, 31]:
raise RuntimeError("%s: Not a target state and status message, \
or operation status message, expecting TC = 29 or 31" % msg)
msgbin = common.hex2bin(msg)
if tc == 29:
NACp = common.bin2int(msgbin[71:75])
elif tc == 31:
NACp = common.bin2int(msgbin[76:80])
try:
EPU = uncertainty.NACp[NACp]['EPU']
VEPU = uncertainty.NACp[NACp]['VEPU']
except KeyError:
EPU, VEPU = uncertainty.NA, uncertainty.NA
return EPU, VEPU
def nac_v(msg):
"""Calculate NACv, Navigation Accuracy Category - Velocity
Args:
msg (string): 28 bytes hexadecimal message string, TC = 19
Returns:
int or string: 95% horizontal accuracy bounds for velocity, Horizontal Figure of Merit
int or string: 95% vertical accuracy bounds for velocity, Vertical Figure of Merit
"""
tc = typecode(msg)
if tc != 19:
raise RuntimeError("%s: Not an airborne velocity message, expecting TC = 19" % msg)
msgbin = common.hex2bin(msg)
NACv = common.bin2int(msgbin[42:45])
try:
HFOMr = uncertainty.NACv[NACv]['HFOMr']
VFOMr = uncertainty.NACv[NACv]['VFOMr']
except KeyError:
HFOMr, VFOMr = uncertainty.NA, uncertainty.NA
return HFOMr, VFOMr
def sil(msg, version):
"""Calculate SIL, Surveillance Integrity Level
Args:
msg (string): 28 bytes hexadecimal message string with TC = 29, 31
Returns:
int or string: Probability of exceeding Horizontal Radius of Containment RCu
int or string: Probability of exceeding Vertical Integrity Containment Region VPL
string: SIL supplement based on per "hour" or "sample", or 'unknown'
"""
tc = typecode(msg)
if tc not in [29, 31]:
raise RuntimeError("%s: Not a target state and status messag, \
or operation status message, expecting TC = 29 or 31" % msg)
msgbin = common.hex2bin(msg)
if tc == 29:
SIL = common.bin2int(msgbin[76:78])
elif tc == 31:
SIL = common.bin2int(msgbin[82:84])
try:
PE_RCu = uncertainty.SIL[SIL]['PE_RCu']
PE_VPL = uncertainty.SIL[SIL]['PE_VPL']
except KeyError:
PE_RCu, PE_VPL = uncertainty.NA, uncertainty.NA
base = 'unknown'
if version == 2:
if tc == 29:
SIL_SUP = common.bin2int(msgbin[39])
elif tc == 31:
SIL_SUP = common.bin2int(msgbin[86])
if SIL_SUP == 0:
base = "hour"
elif SIL_SUP == 1:
base = "sample"
return PE_RCu, PE_VPL, base

View File

@@ -0,0 +1,21 @@
# Copyright (C) 2018 Junzi Sun (TU Delft)
# This program is free software: you can redistribute it and/or modify
# it under the terms of the GNU General Public License as published by
# the Free Software Foundation, either version 3 of the License, or
# (at your option) any later version.
# This program is distributed in the hope that it will be useful,
# but WITHOUT ANY WARRANTY; without even the implied warranty of
# MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
# GNU General Public License for more details.
# You should have received a copy of the GNU General Public License
# along with this program. If not, see <http://www.gnu.org/licenses/>.
"""
Decoding all call replies DF=11
"""
from __future__ import absolute_import, print_function, division
from pyModeS.decoder import common

View File

@@ -0,0 +1,147 @@
# Copyright (C) 2015 Junzi Sun (TU Delft)
# This program is free software: you can redistribute it and/or modify
# it under the terms of the GNU General Public License as published by
# the Free Software Foundation, either version 3 of the License, or
# (at your option) any later version.
# This program is distributed in the hope that it will be useful,
# but WITHOUT ANY WARRANTY; without even the implied warranty of
# MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
# GNU General Public License for more details.
# You should have received a copy of the GNU General Public License
# along with this program. If not, see <http://www.gnu.org/licenses/>.
"""
Common functions for Mode-S decoding
"""
from __future__ import absolute_import, print_function, division
import numpy as np
from pyModeS.extra import aero
from pyModeS.decoder import common
from pyModeS.decoder.bds import bds05, bds06, bds08, bds09, \
bds10, bds17, bds20, bds30, bds40, bds44, bds50, bds53, bds60
def is50or60(msg, spd_ref, trk_ref, alt_ref):
"""Use reference ground speed and trk to determine BDS50 and DBS60
Args:
msg (String): 28 bytes hexadecimal message string
spd_ref (float): reference speed (ADS-B ground speed), kts
trk_ref (float): reference track (ADS-B track angle), deg
alt_ref (float): reference altitude (ADS-B altitude), ft
Returns:
String or None: BDS version, or possible versions, or None if nothing matches.
"""
def vxy(v, angle):
vx = v * np.sin(np.radians(angle))
vy = v * np.cos(np.radians(angle))
return vx, vy
if not (bds50.is50(msg) and bds60.is60(msg)):
return None
h50 = bds50.trk50(msg)
v50 = bds50.gs50(msg)
if h50 is None or v50 is None:
return 'BDS50,BDS60'
h60 = bds60.hdg60(msg)
m60 = bds60.mach60(msg)
i60 = bds60.ias60(msg)
if h60 is None or (m60 is None and i60 is None):
return 'BDS50,BDS60'
m60 = np.nan if m60 is None else m60
i60 = np.nan if i60 is None else i60
XY5 = vxy(v50*aero.kts, h50)
XY6m = vxy(aero.mach2tas(m60, alt_ref*aero.ft), h60)
XY6i = vxy(aero.cas2tas(i60*aero.kts, alt_ref*aero.ft), h60)
allbds = ['BDS50', 'BDS60', 'BDS60']
X = np.array([XY5, XY6m, XY6i])
Mu = np.array(vxy(spd_ref*aero.kts, trk_ref))
# compute Mahalanobis distance matrix
# Cov = [[20**2, 0], [0, 20**2]]
# mmatrix = np.sqrt(np.dot(np.dot(X-Mu, np.linalg.inv(Cov)), (X-Mu).T))
# dist = np.diag(mmatrix)
# since the covariance matrix is identity matrix,
# M-dist is same as eculidian distance
try:
dist = np.linalg.norm(X-Mu, axis=1)
BDS = allbds[np.nanargmin(dist)]
except ValueError:
return 'BDS50,BDS60'
return BDS
def infer(msg):
"""Estimate the most likely BDS code of an message
Args:
msg (String): 28 bytes hexadecimal message string
Returns:
String or None: BDS version, or possible versions, or None if nothing matches.
"""
df = common.df(msg)
if common.allzeros(msg):
return 'EMPTY'
# For ADS-B / Mode-S extended squitter
if df == 17:
tc = common.typecode(msg)
if 1 <= tc <= 4:
return 'BDS08' # indentification and category
if 5 <= tc <= 8:
return 'BDS06' # surface movement
if 9 <= tc <= 18:
return 'BDS05' # airborne position, baro-alt
if tc == 19:
return 'BDS09' # airborne velocity
if 20 <= tc <= 22:
return 'BDS05' # airborne position, gnss-alt
if tc == 28:
return 'BDS61' # aircraft status
if tc == 29:
return 'BDS62' # target state and status
if tc == 31:
return 'BDS65' # operational status
# For Comm-B replies, ELS + EHS only
IS10 = bds10.is10(msg)
IS17 = bds17.is17(msg)
IS20 = bds20.is20(msg)
IS30 = bds30.is30(msg)
IS40 = bds40.is40(msg)
IS50 = bds50.is50(msg)
IS60 = bds60.is60(msg)
allbds = np.array([
"BDS10", "BDS17", "BDS20", "BDS30", "BDS40", "BDS50", "BDS60"
])
mask = [IS10, IS17, IS20, IS30, IS40, IS50, IS60]
bds = ','.join(sorted(allbds[mask]))
if len(bds) == 0:
return None
else:
return bds

View File

@@ -0,0 +1,162 @@
# Copyright (C) 2018 Junzi Sun (TU Delft)
# This program is free software: you can redistribute it and/or modify
# it under the terms of the GNU General Public License as published by
# the Free Software Foundation, either version 3 of the License, or
# (at your option) any later version.
# This program is distributed in the hope that it will be useful,
# but WITHOUT ANY WARRANTY; without even the implied warranty of
# MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
# GNU General Public License for more details.
# You should have received a copy of the GNU General Public License
# along with this program. If not, see <http://www.gnu.org/licenses/>.
"""
------------------------------------------
BDS 0,5
ADS-B TC=9-18
Airborn position
------------------------------------------
"""
from __future__ import absolute_import, print_function, division
from pyModeS.decoder import common
def airborne_position(msg0, msg1, t0, t1):
"""Decode airborn position from a pair of even and odd position message
Args:
msg0 (string): even message (28 bytes hexadecimal string)
msg1 (string): odd message (28 bytes hexadecimal string)
t0 (int): timestamps for the even message
t1 (int): timestamps for the odd message
Returns:
(float, float): (latitude, longitude) of the aircraft
"""
mb0 = common.hex2bin(msg0)[32:]
mb1 = common.hex2bin(msg1)[32:]
# 131072 is 2^17, since CPR lat and lon are 17 bits each.
cprlat_even = common.bin2int(mb0[22:39]) / 131072.0
cprlon_even = common.bin2int(mb0[39:56]) / 131072.0
cprlat_odd = common.bin2int(mb1[22:39]) / 131072.0
cprlon_odd = common.bin2int(mb1[39:56]) / 131072.0
air_d_lat_even = 360.0 / 60
air_d_lat_odd = 360.0 / 59
# compute latitude index 'j'
j = common.floor(59 * cprlat_even - 60 * cprlat_odd + 0.5)
lat_even = float(air_d_lat_even * (j % 60 + cprlat_even))
lat_odd = float(air_d_lat_odd * (j % 59 + cprlat_odd))
if lat_even >= 270:
lat_even = lat_even - 360
if lat_odd >= 270:
lat_odd = lat_odd - 360
# check if both are in the same latidude zone, exit if not
if common.cprNL(lat_even) != common.cprNL(lat_odd):
return None
# compute ni, longitude index m, and longitude
if (t0 > t1):
lat = lat_even
nl = common.cprNL(lat)
ni = max(common.cprNL(lat)- 0, 1)
m = common.floor(cprlon_even * (nl-1) - cprlon_odd * nl + 0.5)
lon = (360.0 / ni) * (m % ni + cprlon_even)
else:
lat = lat_odd
nl = common.cprNL(lat)
ni = max(common.cprNL(lat) - 1, 1)
m = common.floor(cprlon_even * (nl-1) - cprlon_odd * nl + 0.5)
lon = (360.0 / ni) * (m % ni + cprlon_odd)
if lon > 180:
lon = lon - 360
return round(lat, 5), round(lon, 5)
def airborne_position_with_ref(msg, lat_ref, lon_ref):
"""Decode airborne position with only one message,
knowing reference nearby location, such as previously calculated location,
ground station, or airport location, etc. The reference position shall
be with in 180NM of the true position.
Args:
msg (string): even message (28 bytes hexadecimal string)
lat_ref: previous known latitude
lon_ref: previous known longitude
Returns:
(float, float): (latitude, longitude) of the aircraft
"""
mb = common.hex2bin(msg)[32:]
cprlat = common.bin2int(mb[22:39]) / 131072.0
cprlon = common.bin2int(mb[39:56]) / 131072.0
i = int(mb[21])
d_lat = 360.0/59 if i else 360.0/60
j = common.floor(lat_ref / d_lat) \
+ common.floor(0.5 + ((lat_ref % d_lat) / d_lat) - cprlat)
lat = d_lat * (j + cprlat)
ni = common.cprNL(lat) - i
if ni > 0:
d_lon = 360.0 / ni
else:
d_lon = 360.0
m = common.floor(lon_ref / d_lon) \
+ common.floor(0.5 + ((lon_ref % d_lon) / d_lon) - cprlon)
lon = d_lon * (m + cprlon)
return round(lat, 5), round(lon, 5)
def altitude(msg):
"""Decode aircraft altitude
Args:
msg (string): 28 bytes hexadecimal message string
Returns:
int: altitude in feet
"""
tc = common.typecode(msg)
if tc<9 or tc==19 or tc>22:
raise RuntimeError("%s: Not a airborn position message" % msg)
mb = common.hex2bin(msg)[32:]
if tc < 19:
# barometric altitude
q = mb[15]
if q:
n = common.bin2int(mb[8:15]+mb[16:20])
alt = n * 25 - 1000
else:
alt = None
else:
# GNSS altitude, meters -> feet
alt = common.bin2int(mb[8:20]) * 3.28084
return alt

View File

@@ -0,0 +1,187 @@
# Copyright (C) 2018 Junzi Sun (TU Delft)
# This program is free software: you can redistribute it and/or modify
# it under the terms of the GNU General Public License as published by
# the Free Software Foundation, either version 3 of the License, or
# (at your option) any later version.
# This program is distributed in the hope that it will be useful,
# but WITHOUT ANY WARRANTY; without even the implied warranty of
# MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
# GNU General Public License for more details.
# You should have received a copy of the GNU General Public License
# along with this program. If not, see <http://www.gnu.org/licenses/>.
"""
------------------------------------------
BDS 0,6
ADS-B TC=5-8
Surface position
------------------------------------------
"""
from __future__ import absolute_import, print_function, division
from pyModeS.decoder import common
import math
def surface_position(msg0, msg1, t0, t1, lat_ref, lon_ref):
"""Decode surface position from a pair of even and odd position message,
the lat/lon of receiver must be provided to yield the correct solution.
Args:
msg0 (string): even message (28 bytes hexadecimal string)
msg1 (string): odd message (28 bytes hexadecimal string)
t0 (int): timestamps for the even message
t1 (int): timestamps for the odd message
lat_ref (float): latitude of the receiver
lon_ref (float): longitude of the receiver
Returns:
(float, float): (latitude, longitude) of the aircraft
"""
msgbin0 = common.hex2bin(msg0)
msgbin1 = common.hex2bin(msg1)
# 131072 is 2^17, since CPR lat and lon are 17 bits each.
cprlat_even = common.bin2int(msgbin0[54:71]) / 131072.0
cprlon_even = common.bin2int(msgbin0[71:88]) / 131072.0
cprlat_odd = common.bin2int(msgbin1[54:71]) / 131072.0
cprlon_odd = common.bin2int(msgbin1[71:88]) / 131072.0
air_d_lat_even = 90.0 / 60
air_d_lat_odd = 90.0 / 59
# compute latitude index 'j'
j = common.floor(59 * cprlat_even - 60 * cprlat_odd + 0.5)
# solution for north hemisphere
lat_even_n = float(air_d_lat_even * (j % 60 + cprlat_even))
lat_odd_n = float(air_d_lat_odd * (j % 59 + cprlat_odd))
# solution for north hemisphere
lat_even_s = lat_even_n - 90.0
lat_odd_s = lat_odd_n - 90.0
# chose which solution corrispondes to receiver location
lat_even = lat_even_n if lat_ref > 0 else lat_even_s
lat_odd = lat_odd_n if lat_ref > 0 else lat_odd_s
# check if both are in the same latidude zone, rare but possible
if common.cprNL(lat_even) != common.cprNL(lat_odd):
return None
# compute ni, longitude index m, and longitude
if (t0 > t1):
lat = lat_even
nl = common.cprNL(lat_even)
ni = max(common.cprNL(lat_even) - 0, 1)
m = common.floor(cprlon_even * (nl-1) - cprlon_odd * nl + 0.5)
lon = (90.0 / ni) * (m % ni + cprlon_even)
else:
lat = lat_odd
nl = common.cprNL(lat_odd)
ni = max(common.cprNL(lat_odd) - 1, 1)
m = common.floor(cprlon_even * (nl-1) - cprlon_odd * nl + 0.5)
lon = (90.0 / ni) * (m % ni + cprlon_odd)
# four possible longitude solutions
lons = [lon, lon + 90.0, lon + 180.0, lon + 270.0]
# the closest solution to receiver is the correct one
dls = [abs(lon_ref - l) for l in lons]
imin = min(range(4), key=dls.__getitem__)
lon = lons[imin]
return round(lat, 5), round(lon, 5)
def surface_position_with_ref(msg, lat_ref, lon_ref):
"""Decode surface position with only one message,
knowing reference nearby location, such as previously calculated location,
ground station, or airport location, etc. The reference position shall
be with in 45NM of the true position.
Args:
msg (string): even message (28 bytes hexadecimal string)
lat_ref: previous known latitude
lon_ref: previous known longitude
Returns:
(float, float): (latitude, longitude) of the aircraft
"""
mb = common.hex2bin(msg)[32:]
cprlat = common.bin2int(mb[22:39]) / 131072.0
cprlon = common.bin2int(mb[39:56]) / 131072.0
i = int(mb[21])
d_lat = 90.0/59 if i else 90.0/60
j = common.floor(lat_ref / d_lat) \
+ common.floor(0.5 + ((lat_ref % d_lat) / d_lat) - cprlat)
lat = d_lat * (j + cprlat)
ni = common.cprNL(lat) - i
if ni > 0:
d_lon = 90.0 / ni
else:
d_lon = 90.0
m = common.floor(lon_ref / d_lon) \
+ common.floor(0.5 + ((lon_ref % d_lon) / d_lon) - cprlon)
lon = d_lon * (m + cprlon)
return round(lat, 5), round(lon, 5)
def surface_velocity(msg):
"""Decode surface velocity from from a surface position message
Args:
msg (string): 28 bytes hexadecimal message string
Returns:
(int, float, int, string): speed (kt), ground track (degree),
rate of climb/descend (ft/min), and speed type
('GS' for ground speed, 'AS' for airspeed)
"""
if common.typecode(msg) < 5 or common.typecode(msg) > 8:
raise RuntimeError("%s: Not a surface message, expecting 5<TC<8" % msg)
mb = common.hex2bin(msg)[32:]
# ground track
trk_status = int(mb[12])
if trk_status == 1:
trk = common.bin2int(mb[13:20]) * 360.0 / 128.0
trk = round(trk, 1)
else:
trk = None
# ground movment / speed
mov = common.bin2int(mb[5:12])
if mov == 0 or mov > 124:
spd = None
elif mov == 1:
spd = 0
elif mov == 124:
spd = 175
else:
movs = [2, 9, 13, 39, 94, 109, 124]
kts = [0.125, 1, 2, 15, 70, 100, 175]
i = next(m[0] for m in enumerate(movs) if m[1] > mov)
step = (kts[i] - kts[i-1]) * 1.0 / (movs[i]-movs[i-1])
spd = kts[i-1] + (mov-movs[i-1]) * step
spd = round(spd, 2)
return spd, trk, 0, 'GS'

View File

@@ -0,0 +1,75 @@
# Copyright (C) 2018 Junzi Sun (TU Delft)
# This program is free software: you can redistribute it and/or modify
# it under the terms of the GNU General Public License as published by
# the Free Software Foundation, either version 3 of the License, or
# (at your option) any later version.
# This program is distributed in the hope that it will be useful,
# but WITHOUT ANY WARRANTY; without even the implied warranty of
# MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
# GNU General Public License for more details.
# You should have received a copy of the GNU General Public License
# along with this program. If not, see <http://www.gnu.org/licenses/>.
"""
------------------------------------------
BDS 0,8
ADS-B TC=1-4
Aircraft identitification and category
------------------------------------------
"""
from __future__ import absolute_import, print_function, division
from pyModeS.decoder import common
def category(msg):
"""Aircraft category number
Args:
msg (string): 28 bytes hexadecimal message string
Returns:
int: category number
"""
if common.typecode(msg) < 1 or common.typecode(msg) > 4:
raise RuntimeError("%s: Not a identification message" % msg)
msgbin = common.hex2bin(msg)
return common.bin2int(msgbin[5:8])
def callsign(msg):
"""Aircraft callsign
Args:
msg (string): 28 bytes hexadecimal message string
Returns:
string: callsign
"""
if common.typecode(msg) < 1 or common.typecode(msg) > 4:
raise RuntimeError("%s: Not a identification message" % msg)
chars = '#ABCDEFGHIJKLMNOPQRSTUVWXYZ#####_###############0123456789######'
msgbin = common.hex2bin(msg)
csbin = msgbin[40:96]
cs = ''
cs += chars[common.bin2int(csbin[0:6])]
cs += chars[common.bin2int(csbin[6:12])]
cs += chars[common.bin2int(csbin[12:18])]
cs += chars[common.bin2int(csbin[18:24])]
cs += chars[common.bin2int(csbin[24:30])]
cs += chars[common.bin2int(csbin[30:36])]
cs += chars[common.bin2int(csbin[36:42])]
cs += chars[common.bin2int(csbin[42:48])]
# clean string, remove spaces and marks, if any.
# cs = cs.replace('_', '')
cs = cs.replace('#', '')
return cs

View File

@@ -0,0 +1,117 @@
# Copyright (C) 2018 Junzi Sun (TU Delft)
# This program is free software: you can redistribute it and/or modify
# it under the terms of the GNU General Public License as published by
# the Free Software Foundation, either version 3 of the License, or
# (at your option) any later version.
# This program is distributed in the hope that it will be useful,
# but WITHOUT ANY WARRANTY; without even the implied warranty of
# MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
# GNU General Public License for more details.
# You should have received a copy of the GNU General Public License
# along with this program. If not, see <http://www.gnu.org/licenses/>.
"""
------------------------------------------
BDS 0,9
ADS-B TC=19
Aircraft Airborn velocity
------------------------------------------
"""
from __future__ import absolute_import, print_function, division
from pyModeS.decoder import common
import math
def airborne_velocity(msg):
"""Calculate the speed, track (or heading), and vertical rate
Args:
msg (string): 28 bytes hexadecimal message string
Returns:
(int, float, int, string): speed (kt), ground track or heading (degree),
rate of climb/descend (ft/min), and speed type
('GS' for ground speed, 'AS' for airspeed)
"""
if common.typecode(msg) != 19:
raise RuntimeError("%s: Not a airborne velocity message, expecting TC=19" % msg)
mb = common.hex2bin(msg)[32:]
subtype = common.bin2int(mb[5:8])
if common.bin2int(mb[14:24]) == 0 or common.bin2int(mb[25:35]) == 0:
return None
if subtype in (1, 2):
v_ew_sign = -1 if mb[13]=='1' else 1
v_ew = common.bin2int(mb[14:24]) - 1 # east-west velocity
v_ns_sign = -1 if mb[24]=='1' else 1
v_ns = common.bin2int(mb[25:35]) - 1 # north-south velocity
v_we = v_ew_sign * v_ew
v_sn = v_ns_sign * v_ns
spd = math.sqrt(v_sn*v_sn + v_we*v_we) # unit in kts
spd = int(spd)
trk = math.atan2(v_we, v_sn)
trk = math.degrees(trk) # convert to degrees
trk = trk if trk >= 0 else trk + 360 # no negative val
tag = 'GS'
trk_or_hdg = round(trk, 2)
else:
if mb[13] == '0':
hdg = None
else:
hdg = common.bin2int(mb[14:24]) / 1024.0 * 360.0
hdg = round(hdg, 2)
trk_or_hdg = hdg
spd = common.bin2int(mb[25:35])
spd = None if spd==0 else spd-1
if mb[24]=='0':
tag = 'IAS'
else:
tag = 'TAS'
vr_sign = -1 if mb[36]=='1' else 1
vr = common.bin2int(mb[37:46])
rocd = None if vr==0 else int(vr_sign*(vr-1)*64)
return spd, trk_or_hdg, rocd, tag
def altitude_diff(msg):
"""Decode the differece between GNSS and barometric altitude
Args:
msg (string): 28 bytes hexadecimal message string, TC=19
Returns:
int: Altitude difference in ft. Negative value indicates GNSS altitude
below barometric altitude.
"""
tc = common.typecode(msg)
if tc != 19:
raise RuntimeError("%s: Not a airborne velocity message, expecting TC=19" % msg)
msgbin = common.hex2bin(msg)
sign = -1 if int(msgbin[80]) else 1
value = common.bin2int(msgbin[81:88])
if value == 0 or value == 127:
return None
else:
return sign * (value - 1) * 25 # in ft.

View File

@@ -0,0 +1,66 @@
# Copyright (C) 2018 Junzi Sun (TU Delft)
# This program is free software: you can redistribute it and/or modify
# it under the terms of the GNU General Public License as published by
# the Free Software Foundation, either version 3 of the License, or
# (at your option) any later version.
# This program is distributed in the hope that it will be useful,
# but WITHOUT ANY WARRANTY; without even the implied warranty of
# MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
# GNU General Public License for more details.
# You should have received a copy of the GNU General Public License
# along with this program. If not, see <http://www.gnu.org/licenses/>.
from __future__ import absolute_import, print_function, division
from pyModeS.decoder.common import hex2bin, bin2int, data, allzeros
# ------------------------------------------
# BDS 1,0
# Data link capability report
# ------------------------------------------
def is10(msg):
"""Check if a message is likely to be BDS code 1,0
Args:
msg (String): 28 bytes hexadecimal message string
Returns:
bool: True or False
"""
if allzeros(msg):
return False
d = hex2bin(data(msg))
# first 8 bits must be 0x10
if d[0:8] != '00010000':
return False
# bit 10 to 14 are reserved
if bin2int(d[9:14]) != 0:
return False
# overlay capabilty conflict
if d[14] == '1' and bin2int(d[16:23]) < 5:
return False
if d[14] == '0' and bin2int(d[16:23]) > 4:
return False
return True
def ovc10(msg):
"""Return the overlay control capability
Args:
msg (String): 28 bytes hexadecimal message string
Returns:
int: Whether the transponder is OVC capable
"""
d = hex2bin(data(msg))
return int(d[14])

View File

@@ -0,0 +1,75 @@
# Copyright (C) 2018 Junzi Sun (TU Delft)
# This program is free software: you can redistribute it and/or modify
# it under the terms of the GNU General Public License as published by
# the Free Software Foundation, either version 3 of the License, or
# (at your option) any later version.
# This program is distributed in the hope that it will be useful,
# but WITHOUT ANY WARRANTY; without even the implied warranty of
# MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
# GNU General Public License for more details.
# You should have received a copy of the GNU General Public License
# along with this program. If not, see <http://www.gnu.org/licenses/>.
from __future__ import absolute_import, print_function, division
from pyModeS.decoder.common import hex2bin, bin2int, data, allzeros
"""
------------------------------------------
BDS 1,7
Common usage GICB capability report
------------------------------------------
"""
def is17(msg):
"""Check if a message is likely to be BDS code 1,7
Args:
msg (String): 28 bytes hexadecimal message string
Returns:
bool: True or False
"""
if allzeros(msg):
return False
d = hex2bin(data(msg))
if bin2int(d[28:56]) != 0:
return False
caps = cap17(msg)
# basic BDS codes for ADS-B shall be supported
# assuming ADS-B out is installed (2017EU/2020US mandate)
# if not set(['BDS05', 'BDS06', 'BDS08', 'BDS09', 'BDS20']).issubset(caps):
# return False
# at least you can respond who you are
if 'BDS20' not in caps:
return False
return True
def cap17(msg):
"""Extract capacities from BDS 1,7 message
Args:
msg (String): 28 bytes hexadecimal message string
Returns:
list: list of suport BDS codes
"""
allbds = ['05', '06', '07', '08', '09', '0A', '20', '21', '40', '41',
'42', '43', '44', '45', '48', '50', '51', '52', '53', '54',
'55', '56', '5F', '60', 'NA', 'NA', 'E1', 'E2']
d = hex2bin(data(msg))
idx = [i for i, v in enumerate(d[:28]) if v=='1']
capacity = ['BDS'+allbds[i] for i in idx if allbds[i] is not 'NA']
return capacity

View File

@@ -0,0 +1,73 @@
# Copyright (C) 2018 Junzi Sun (TU Delft)
# This program is free software: you can redistribute it and/or modify
# it under the terms of the GNU General Public License as published by
# the Free Software Foundation, either version 3 of the License, or
# (at your option) any later version.
# This program is distributed in the hope that it will be useful,
# but WITHOUT ANY WARRANTY; without even the implied warranty of
# MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
# GNU General Public License for more details.
# You should have received a copy of the GNU General Public License
# along with this program. If not, see <http://www.gnu.org/licenses/>.
from __future__ import absolute_import, print_function, division
from pyModeS.decoder.common import hex2bin, bin2int, data, allzeros
# ------------------------------------------
# BDS 2,0
# Aircraft identification
# ------------------------------------------
def is20(msg):
"""Check if a message is likely to be BDS code 2,0
Args:
msg (String): 28 bytes hexadecimal message string
Returns:
bool: True or False
"""
if allzeros(msg):
return False
d = hex2bin(data(msg))
if d[0:8] != '00100000':
return False
cs = cs20(msg)
if '#' in cs:
return False
return True
def cs20(msg):
"""Aircraft callsign
Args:
msg (String): 28 bytes hexadecimal message (BDS40) string
Returns:
string: callsign, max. 8 chars
"""
chars = '#ABCDEFGHIJKLMNOPQRSTUVWXYZ#####_###############0123456789######'
d = hex2bin(data(msg))
cs = ''
cs += chars[bin2int(d[8:14])]
cs += chars[bin2int(d[14:20])]
cs += chars[bin2int(d[20:26])]
cs += chars[bin2int(d[26:32])]
cs += chars[bin2int(d[32:38])]
cs += chars[bin2int(d[38:44])]
cs += chars[bin2int(d[44:50])]
cs += chars[bin2int(d[50:56])]
return cs

View File

@@ -0,0 +1,50 @@
# Copyright (C) 2018 Junzi Sun (TU Delft)
# This program is free software: you can redistribute it and/or modify
# it under the terms of the GNU General Public License as published by
# the Free Software Foundation, either version 3 of the License, or
# (at your option) any later version.
# This program is distributed in the hope that it will be useful,
# but WITHOUT ANY WARRANTY; without even the implied warranty of
# MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
# GNU General Public License for more details.
# You should have received a copy of the GNU General Public License
# along with this program. If not, see <http://www.gnu.org/licenses/>.
from __future__ import absolute_import, print_function, division
from pyModeS.decoder.common import hex2bin, bin2int, data, allzeros
# ------------------------------------------
# BDS 3,0
# ACAS active resolution advisory
# ------------------------------------------
def is30(msg):
"""Check if a message is likely to be BDS code 2,0
Args:
msg (String): 28 bytes hexadecimal message string
Returns:
bool: True or False
"""
if allzeros(msg):
return False
d = hex2bin(data(msg))
if d[0:8] != '00110000':
return False
# threat type 3 not assigned
if d[28:30] == '11':
return False
# reserved for ACAS III, in far future
if bin2int(d[15:22]) >= 48:
return False
return True

View File

@@ -0,0 +1,119 @@
# Copyright (C) 2018 Junzi Sun (TU Delft)
# This program is free software: you can redistribute it and/or modify
# it under the terms of the GNU General Public License as published by
# the Free Software Foundation, either version 3 of the License, or
# (at your option) any later version.
# This program is distributed in the hope that it will be useful,
# but WITHOUT ANY WARRANTY; without even the implied warranty of
# MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
# GNU General Public License for more details.
# You should have received a copy of the GNU General Public License
# along with this program. If not, see <http://www.gnu.org/licenses/>.
from __future__ import absolute_import, print_function, division
from pyModeS.decoder.common import hex2bin, bin2int, data, allzeros, wrongstatus
# ------------------------------------------
# BDS 4,0
# Selected vertical intention
# ------------------------------------------
def is40(msg):
"""Check if a message is likely to be BDS code 4,0
Args:
msg (String): 28 bytes hexadecimal message string
Returns:
bool: True or False
"""
if allzeros(msg):
return False
d = hex2bin(data(msg))
# status bit 1, 14, and 27
if wrongstatus(d, 1, 2, 13):
return False
if wrongstatus(d, 14, 15, 26):
return False
if wrongstatus(d, 27, 28, 39):
return False
if wrongstatus(d, 48, 49, 51):
return False
if wrongstatus(d, 54, 55, 56):
return False
# bits 40-47 and 52-53 shall all be zero
if bin2int(d[39:47]) != 0:
return False
if bin2int(d[51:53]) != 0:
return False
return True
def alt40mcp(msg):
"""Selected altitude, MCP/FCU
Args:
msg (String): 28 bytes hexadecimal message (BDS40) string
Returns:
int: altitude in feet
"""
d = hex2bin(data(msg))
if d[0] == '0':
return None
alt = bin2int(d[1:13]) * 16 # ft
return alt
def alt40fms(msg):
"""Selected altitude, FMS
Args:
msg (String): 28 bytes hexadecimal message (BDS40) string
Returns:
int: altitude in feet
"""
d = hex2bin(data(msg))
if d[13] == '0':
return None
alt = bin2int(d[14:26]) * 16 # ft
return alt
def p40baro(msg):
"""Barometric pressure setting
Args:
msg (String): 28 bytes hexadecimal message (BDS40) string
Returns:
float: pressure in millibar
"""
d = hex2bin(data(msg))
if d[26] == '0':
return None
p = bin2int(d[27:39]) * 0.1 + 800 # millibar
return p

View File

@@ -0,0 +1,218 @@
# Copyright (C) 2018 Junzi Sun (TU Delft)
# This program is free software: you can redistribute it and/or modify
# it under the terms of the GNU General Public License as published by
# the Free Software Foundation, either version 3 of the License, or
# (at your option) any later version.
# This program is distributed in the hope that it will be useful,
# but WITHOUT ANY WARRANTY; without even the implied warranty of
# MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
# GNU General Public License for more details.
# You should have received a copy of the GNU General Public License
# along with this program. If not, see <http://www.gnu.org/licenses/>.
from __future__ import absolute_import, print_function, division
from pyModeS.decoder.common import hex2bin, bin2int, data, allzeros, wrongstatus
# ------------------------------------------
# BDS 4,4
# Meteorological routine air report
# ------------------------------------------
def is44(msg, rev=False):
"""Check if a message is likely to be BDS code 4,4
Meteorological routine air report
Args:
msg (String): 28 bytes hexadecimal message string
rev (bool): using revised version
Returns:
bool: True or False
"""
if allzeros(msg):
return False
d = hex2bin(data(msg))
if not rev:
# status bit 5, 35, 47, 50
if wrongstatus(d, 5, 6, 23):
return False
if wrongstatus(d, 35, 36, 46):
return False
if wrongstatus(d, 47, 48, 49):
return False
if wrongstatus(d, 50, 51, 56):
return False
# Bits 1-4 indicate source, values > 4 reserved and should not occur
if bin2int(d[0:4]) > 4:
return False
else:
# status bit 5, 15, 24, 36, 49
if wrongstatus(d, 5, 6, 14):
return False
if wrongstatus(d, 15, 16, 23):
return False
if wrongstatus(d, 24, 25, 35):
return False
if wrongstatus(d, 36, 37, 47):
return False
if wrongstatus(d, 49, 50, 56):
return False
# Bits 1-4 are reserved and should be zero
if bin2int(d[0:4]) != 0:
return False
vw = wind44(msg, rev=rev)
if vw is not None and vw[0] > 250:
return False
if temp44(msg):
if temp44(msg) > 60 or temp44(msg) < -80:
return False
elif temp44(msg) == 0:
return False
return True
def wind44(msg, rev=False):
"""reported wind speed and direction
Args:
msg (String): 28 bytes hexadecimal message (BDS44) string
rev (bool): using revised version
Returns:
(int, float): speed (kt), direction (degree)
"""
d = hex2bin(data(msg))
if not rev:
status = int(d[4])
if not status:
return None
speed = bin2int(d[5:14]) # knots
direction = bin2int(d[14:23]) * 180.0 / 256.0 # degree
else:
spd_status = int(d[4])
dir_status = int(d[14])
if (not spd_status) or (not dir_status):
return None
speed = bin2int(d[5:14]) # knots
direction = bin2int(d[15:23]) * 180.0 / 128.0 # degree
return round(speed, 0), round(direction, 1)
def temp44(msg, rev=False):
"""reported air temperature
Args:
msg (String): 28 bytes hexadecimal message (BDS44) string
rev (bool): using revised version
Returns:
float: tmeperature in Celsius degree
"""
d = hex2bin(data(msg))
if not rev:
# if d[22] == '0':
# return None
sign = int(d[23])
value = bin2int(d[24:34])
if sign:
value = value - 1024
temp = value * 0.125 # celsius
temp = round(temp, 1)
else:
# if d[23] == '0':
# return None
sign = int(d[24])
value = bin2int(d[25:35])
if sign:
value = value - 1024
temp = value * 0.125 # celsius
temp = round(temp, 1)
return temp
def p44(msg, rev=False):
"""reported average static pressure
Args:
msg (String): 28 bytes hexadecimal message (BDS44) string
rev (bool): using revised version
Returns:
int: static pressure in hPa
"""
d = hex2bin(data(msg))
if not rev:
if d[34] == '0':
return None
p = bin2int(d[35:46]) # hPa
else:
if d[35] == '0':
return None
p = bin2int(d[36:47]) # hPa
return p
def hum44(msg, rev=False):
"""reported humidity
Args:
msg (String): 28 bytes hexadecimal message (BDS44) string
rev (bool): using revised version
Returns:
float: percentage of humidity, [0 - 100] %
"""
d = hex2bin(data(msg))
if not rev:
if d[49] == '0':
return None
hm = bin2int(d[50:56]) * 100.0 / 64 # %
else:
if d[48] == '0':
return None
hm = bin2int(d[49:56]) # %
return round(hm, 1)

View File

@@ -0,0 +1,188 @@
# Copyright (C) 2018 Junzi Sun (TU Delft)
# This program is free software: you can redistribute it and/or modify
# it under the terms of the GNU General Public License as published by
# the Free Software Foundation, either version 3 of the License, or
# (at your option) any later version.
# This program is distributed in the hope that it will be useful,
# but WITHOUT ANY WARRANTY; without even the implied warranty of
# MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
# GNU General Public License for more details.
# You should have received a copy of the GNU General Public License
# along with this program. If not, see <http://www.gnu.org/licenses/>.
from __future__ import absolute_import, print_function, division
from pyModeS.decoder.common import hex2bin, bin2int, data, allzeros, wrongstatus
# ------------------------------------------
# BDS 5,0
# Track and turn report
# ------------------------------------------
def is50(msg):
"""Check if a message is likely to be BDS code 5,0
(Track and turn report)
Args:
msg (String): 28 bytes hexadecimal message string
Returns:
bool: True or False
"""
if allzeros(msg):
return False
d = hex2bin(data(msg))
# status bit 1, 12, 24, 35, 46
if wrongstatus(d, 1, 3, 11):
return False
if wrongstatus(d, 12, 13, 23):
return False
if wrongstatus(d, 24, 25, 34):
return False
if wrongstatus(d, 35, 36, 45):
return False
if wrongstatus(d, 46, 47, 56):
return False
roll = roll50(msg)
if (roll is not None) and abs(roll) > 60:
return False
gs = gs50(msg)
if gs is not None and gs > 600:
return False
tas = tas50(msg)
if tas is not None and tas > 500:
return False
if (gs is not None) and (tas is not None) and (abs(tas - gs) > 200):
return False
return True
def roll50(msg):
"""Roll angle, BDS 5,0 message
Args:
msg (String): 28 bytes hexadecimal message (BDS50) string
Returns:
float: angle in degrees,
negative->left wing down, positive->right wing down
"""
d = hex2bin(data(msg))
if d[0] == '0':
return None
sign = int(d[1]) # 1 -> left wing down
value = bin2int(d[2:11])
if sign:
value = value - 512
angle = value * 45.0 / 256.0 # degree
return round(angle, 1)
def trk50(msg):
"""True track angle, BDS 5,0 message
Args:
msg (String): 28 bytes hexadecimal message (BDS50) string
Returns:
float: angle in degrees to true north (from 0 to 360)
"""
d = hex2bin(data(msg))
if d[11] == '0':
return None
sign = int(d[12]) # 1 -> west
value = bin2int(d[13:23])
if sign:
value = value - 1024
trk = value * 90.0 / 512.0
# convert from [-180, 180] to [0, 360]
if trk < 0:
trk = 360 + trk
return round(trk, 3)
def gs50(msg):
"""Ground speed, BDS 5,0 message
Args:
msg (String): 28 bytes hexadecimal message (BDS50) string
Returns:
int: ground speed in knots
"""
d = hex2bin(data(msg))
if d[23] == '0':
return None
spd = bin2int(d[24:34]) * 2 # kts
return spd
def rtrk50(msg):
"""Track angle rate, BDS 5,0 message
Args:
msg (String): 28 bytes hexadecimal message (BDS50) string
Returns:
float: angle rate in degrees/second
"""
d = hex2bin(data(msg))
if d[34] == '0':
return None
if d[36:45] == "111111111":
return None
sign = int(d[35]) # 1 -> negative value, two's complement
value = bin2int(d[36:45])
if sign:
value = value - 512
angle = value * 8.0 / 256.0 # degree / sec
return round(angle, 3)
def tas50(msg):
"""Aircraft true airspeed, BDS 5,0 message
Args:
msg (String): 28 bytes hexadecimal message (BDS50) string
Returns:
int: true airspeed in knots
"""
d = hex2bin(data(msg))
if d[45] == '0':
return None
tas = bin2int(d[46:56]) * 2 # kts
return tas

View File

@@ -0,0 +1,181 @@
# Copyright (C) 2018 Junzi Sun (TU Delft)
# This program is free software: you can redistribute it and/or modify
# it under the terms of the GNU General Public License as published by
# the Free Software Foundation, either version 3 of the License, or
# (at your option) any later version.
# This program is distributed in the hope that it will be useful,
# but WITHOUT ANY WARRANTY; without even the implied warranty of
# MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
# GNU General Public License for more details.
# You should have received a copy of the GNU General Public License
# along with this program. If not, see <http://www.gnu.org/licenses/>.
from __future__ import absolute_import, print_function, division
from pyModeS.decoder.common import hex2bin, bin2int, data, allzeros, wrongstatus
# ------------------------------------------
# BDS 5,3
# Air-referenced state vector
# ------------------------------------------
def is53(msg):
"""Check if a message is likely to be BDS code 5,3
(Air-referenced state vector)
Args:
msg (String): 28 bytes hexadecimal message string
Returns:
bool: True or False
"""
if allzeros(msg):
return False
d = hex2bin(data(msg))
# status bit 1, 13, 24, 34, 47
if wrongstatus(d, 1, 3, 12):
return False
if wrongstatus(d, 13, 14, 23):
return False
if wrongstatus(d, 24, 25, 33):
return False
if wrongstatus(d, 34, 35, 46):
return False
if wrongstatus(d, 47, 49, 56):
return False
ias = ias53(msg)
if ias is not None and ias > 500:
return False
mach = mach53(msg)
if mach is not None and mach > 1:
return False
tas = tas53(msg)
if tas is not None and tas > 500:
return False
vr = vr53(msg)
if vr is not None and abs(vr) > 8000:
return False
return True
def hdg53(msg):
"""Magnetic heading, BDS 5,3 message
Args:
msg (String): 28 bytes hexadecimal message (BDS53) string
Returns:
float: angle in degrees to true north (from 0 to 360)
"""
d = hex2bin(data(msg))
if d[0] == '0':
return None
sign = int(d[1]) # 1 -> west
value = bin2int(d[2:12])
if sign:
value = value - 1024
hdg = value * 90.0 / 512.0 # degree
# convert from [-180, 180] to [0, 360]
if hdg < 0:
hdg = 360 + hdg
return round(hdg, 3)
def ias53(msg):
"""Indicated airspeed, DBS 5,3 message
Args:
msg (String): 28 bytes hexadecimal message
Returns:
int: indicated arispeed in knots
"""
d = hex2bin(data(msg))
if d[12] == '0':
return None
ias = bin2int(d[13:23]) # knots
return ias
def mach53(msg):
"""MACH number, DBS 5,3 message
Args:
msg (String): 28 bytes hexadecimal message
Returns:
float: MACH number
"""
d = hex2bin(data(msg))
if d[23] == '0':
return None
mach = bin2int(d[24:33]) * 0.008
return round(mach, 3)
def tas53(msg):
"""Aircraft true airspeed, BDS 5,3 message
Args:
msg (String): 28 bytes hexadecimal message
Returns:
float: true airspeed in knots
"""
d = hex2bin(data(msg))
if d[33] == '0':
return None
tas = bin2int(d[34:46]) * 0.5 # kts
return round(tas, 1)
def vr53(msg):
"""Vertical rate
Args:
msg (String): 28 bytes hexadecimal message (BDS60) string
Returns:
int: vertical rate in feet/minutes
"""
d = hex2bin(data(msg))
if d[46] == '0':
return None
sign = int(d[47]) # 1 -> negative value, two's complement
value = bin2int(d[48:56])
if value == 0 or value == 255: # all zeros or all ones
return 0
value = value - 256 if sign else value
roc = value * 64 # feet/min
return roc

View File

@@ -0,0 +1,189 @@
# Copyright (C) 2018 Junzi Sun (TU Delft)
# This program is free software: you can redistribute it and/or modify
# it under the terms of the GNU General Public License as published by
# the Free Software Foundation, either version 3 of the License, or
# (at your option) any later version.
# This program is distributed in the hope that it will be useful,
# but WITHOUT ANY WARRANTY; without even the implied warranty of
# MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
# GNU General Public License for more details.
# You should have received a copy of the GNU General Public License
# along with this program. If not, see <http://www.gnu.org/licenses/>.
from __future__ import absolute_import, print_function, division
from pyModeS.decoder.common import hex2bin, bin2int, data, allzeros, wrongstatus
# ------------------------------------------
# BDS 6,0
# Heading and speed report
# ------------------------------------------
def is60(msg):
"""Check if a message is likely to be BDS code 6,0
Args:
msg (String): 28 bytes hexadecimal message string
Returns:
bool: True or False
"""
if allzeros(msg):
return False
d = hex2bin(data(msg))
# status bit 1, 13, 24, 35, 46
if wrongstatus(d, 1, 2, 12):
return False
if wrongstatus(d, 13, 14, 23):
return False
if wrongstatus(d, 24, 25, 34):
return False
if wrongstatus(d, 35, 36, 45):
return False
if wrongstatus(d, 46, 47, 56):
return False
ias = ias60(msg)
if ias is not None and ias > 500:
return False
mach = mach60(msg)
if mach is not None and mach > 1:
return False
vr_baro = vr60baro(msg)
if vr_baro is not None and abs(vr_baro) > 6000:
return False
vr_ins = vr60ins(msg)
if vr_ins is not None and abs(vr_ins) > 6000:
return False
return True
def hdg60(msg):
"""Megnetic heading of aircraft
Args:
msg (String): 28 bytes hexadecimal message (BDS60) string
Returns:
float: heading in degrees to megnetic north (from 0 to 360)
"""
d = hex2bin(data(msg))
if d[0] == '0':
return None
sign = int(d[1]) # 1 -> west
value = bin2int(d[2:12])
if sign:
value = value - 1024
hdg = value * 90 / 512.0 # degree
# convert from [-180, 180] to [0, 360]
if hdg < 0:
hdg = 360 + hdg
return round(hdg, 3)
def ias60(msg):
"""Indicated airspeed
Args:
msg (String): 28 bytes hexadecimal message (BDS60) string
Returns:
int: indicated airspeed in knots
"""
d = hex2bin(data(msg))
if d[12] == '0':
return None
ias = bin2int(d[13:23]) # kts
return ias
def mach60(msg):
"""Aircraft MACH number
Args:
msg (String): 28 bytes hexadecimal message (BDS60) string
Returns:
float: MACH number
"""
d = hex2bin(data(msg))
if d[23] == '0':
return None
mach = bin2int(d[24:34]) * 2.048 / 512.0
return round(mach, 3)
def vr60baro(msg):
"""Vertical rate from barometric measurement, this value may be very noisy.
Args:
msg (String): 28 bytes hexadecimal message (BDS60) string
Returns:
int: vertical rate in feet/minutes
"""
d = hex2bin(data(msg))
if d[34] == '0':
return None
sign = int(d[35]) # 1 -> negative value, two's complement
value = bin2int(d[36:45])
if value == 0 or value == 511: # all zeros or all ones
return 0
value = value - 512 if sign else value
roc = value * 32 # feet/min
return roc
def vr60ins(msg):
"""Vertical rate messured by onbard equiments (IRS, AHRS)
Args:
msg (String): 28 bytes hexadecimal message (BDS60) string
Returns:
int: vertical rate in feet/minutes
"""
d = hex2bin(data(msg))
if d[45] == '0':
return None
sign = int(d[46]) # 1 -> negative value, two's complement
value = bin2int(d[47:56])
if value == 0 or value == 511: # all zeros or all ones
return 0
value = value - 512 if sign else value
roc = value * 32 # feet/min
return roc

15
pyModeS/decoder/commb.py Normal file
View File

@@ -0,0 +1,15 @@
from __future__ import absolute_import, print_function, division
# ELS - elementary surveillance
from pyModeS.decoder.bds.bds10 import *
from pyModeS.decoder.bds.bds17 import *
from pyModeS.decoder.bds.bds20 import *
from pyModeS.decoder.bds.bds30 import *
# ELS - enhanced surveillance
from pyModeS.decoder.bds.bds40 import *
from pyModeS.decoder.bds.bds50 import *
from pyModeS.decoder.bds.bds60 import *
# MRAR
from pyModeS.decoder.bds.bds44 import *

313
pyModeS/decoder/common.py Normal file
View File

@@ -0,0 +1,313 @@
from __future__ import absolute_import, print_function, division
import numpy as np
def hex2bin(hexstr):
"""Convert a hexdecimal string to binary string, with zero fillings. """
num_of_bits = len(hexstr) * 4
binstr = bin(int(hexstr, 16))[2:].zfill(int(num_of_bits))
return binstr
def bin2int(binstr):
"""Convert a binary string to integer. """
return int(binstr, 2)
def hex2int(hexstr):
"""Convert a hexdecimal string to integer. """
return int(hexstr, 16)
def bin2np(binstr):
"""Convert a binary string to numpy array. """
return np.array([int(i) for i in binstr])
def np2bin(npbin):
"""Convert a binary numpy array to string. """
return np.array2string(npbin, separator='')[1:-1]
def df(msg):
"""Decode Downlink Format vaule, bits 1 to 5."""
msgbin = hex2bin(msg)
return min( bin2int(msgbin[0:5]) , 24 )
def crc(msg, encode=False):
"""Mode-S Cyclic Redundancy Check
Detect if bit error occurs in the Mode-S message
Args:
msg (string): 28 bytes hexadecimal message string
encode (bool): True to encode the date only and return the checksum
Returns:
string: message checksum, or partity bits (encoder)
"""
# the polynominal generattor code for CRC [1111111111111010000001001]
generator = np.array([1,1,1,1,1,1,1,1,1,1,1,1,1,0,1,0,0,0,0,0,0,1,0,0,1])
ng = len(generator)
msgnpbin = bin2np(hex2bin(msg))
if encode:
msgnpbin[-24:] = [0] * 24
# loop all bits, except last 24 piraty bits
for i in range(len(msgnpbin)-24):
if msgnpbin[i] == 0:
continue
# perform XOR, when 1
msgnpbin[i:i+ng] = np.bitwise_xor(msgnpbin[i:i+ng], generator)
# last 24 bits
reminder = np2bin(msgnpbin[-24:])
return reminder
def floor(x):
""" Mode-S floor function
Defined as the greatest integer value k, such that k <= x
eg.: floor(3.6) = 3, while floor(-3.6) = -4
"""
return int(np.floor(x))
def icao(msg):
"""Calculate the ICAO address from an Mode-S message
with DF4, DF5, DF20, DF21
Args:
msg (String): 28 bytes hexadecimal message string
Returns:
String: ICAO address in 6 bytes hexadecimal string
"""
DF = df(msg)
if DF in (11, 17, 18):
addr = msg[2:8]
elif DF in (0, 4, 5, 16, 20, 21):
c0 = bin2int(crc(msg, encode=True))
c1 = hex2int(msg[-6:])
addr = '%06X' % (c0 ^ c1)
else:
addr = None
return addr
def is_icao_assigned(icao):
""" Check whether the ICAO address is assigned (Annex 10, Vol 3)"""
if (icao is None) or (not isinstance(icao, str)) or (len(icao)!=6):
return False
icaoint = hex2int(icao)
if 0x200000 < icaoint < 0x27FFFF: return False # AFI
if 0x280000 < icaoint < 0x28FFFF: return False # SAM
if 0x500000 < icaoint < 0x5FFFFF: return False # EUR, NAT
if 0x600000 < icaoint < 0x67FFFF: return False # MID
if 0x680000 < icaoint < 0x6F0000: return False # ASIA
if 0x900000 < icaoint < 0x9FFFFF: return False # NAM, PAC
if 0xB00000 < icaoint < 0xBFFFFF: return False # CAR
if 0xD00000 < icaoint < 0xDFFFFF: return False # future
if 0xF00000 < icaoint < 0xFFFFFF: return False # future
return True
def typecode(msg):
"""Type code of ADS-B message
Args:
msg (string): 28 bytes hexadecimal message string
Returns:
int: type code number
"""
if df(msg) not in (17, 18):
return None
msgbin = hex2bin(msg)
return bin2int(msgbin[32:37])
def cprNL(lat):
"""NL() function in CPR decoding"""
if lat == 0:
return 59
if lat == 87 or lat == -87:
return 2
if lat > 87 or lat < -87:
return 1
nz = 15
a = 1 - np.cos(np.pi / (2 * nz))
b = np.cos(np.pi / 180.0 * abs(lat)) ** 2
nl = 2 * np.pi / (np.arccos(1 - a/b))
NL = floor(nl)
return NL
def idcode(msg):
"""Computes identity (squawk code) from DF5 or DF21 message, bit 20-32.
credit: @fbyrkjeland
Args:
msg (String): 28 bytes hexadecimal message string
Returns:
string: squawk code
"""
if df(msg) not in [5, 21]:
raise RuntimeError("Message must be Downlink Format 5 or 21.")
mbin = hex2bin(msg)
C1 = mbin[19]
A1 = mbin[20]
C2 = mbin[21]
A2 = mbin[22]
C4 = mbin[23]
A4 = mbin[24]
# _ = mbin[25]
B1 = mbin[26]
D1 = mbin[27]
B2 = mbin[28]
D2 = mbin[29]
B4 = mbin[30]
D4 = mbin[31]
byte1 = int(A4+A2+A1, 2)
byte2 = int(B4+B2+B1, 2)
byte3 = int(C4+C2+C1, 2)
byte4 = int(D4+D2+D1, 2)
return str(byte1) + str(byte2) + str(byte3) + str(byte4)
def altcode(msg):
"""Computes the altitude from DF4 or DF20 message, bit 20-32.
credit: @fbyrkjeland
Args:
msg (String): 28 bytes hexadecimal message string
Returns:
int: altitude in ft
"""
if df(msg) not in [0, 4, 16, 20]:
raise RuntimeError("Message must be Downlink Format 0, 4, 16, or 20.")
# Altitude code, bit 20-32
mbin = hex2bin(msg)
mbit = mbin[25] # M bit: 26
qbit = mbin[27] # Q bit: 28
if mbit == '0': # unit in ft
if qbit == '1': # 25ft interval
vbin = mbin[19:25] + mbin[26] + mbin[28:32]
alt = bin2int(vbin) * 25 - 1000
if qbit == '0': # 100ft interval, above 50175ft
C1 = mbin[19]
A1 = mbin[20]
C2 = mbin[21]
A2 = mbin[22]
C4 = mbin[23]
A4 = mbin[24]
# _ = mbin[25]
B1 = mbin[26]
# D1 = mbin[27] # always zero
B2 = mbin[28]
D2 = mbin[29]
B4 = mbin[30]
D4 = mbin[31]
graystr = D2 + D4 + A1 + A2 + A4 + B1 + B2 + B4 + C1 + C2 + C4
alt = gray2alt(graystr)
if mbit == '1': # unit in meter
vbin = mbin[19:25] + mbin[26:31]
alt = int(bin2int(vbin) * 3.28084) # convert to ft
return alt
def gray2alt(codestr):
gc500 = codestr[:8]
n500 = gray2int(gc500)
# in 100-ft step must be converted first
gc100 = codestr[8:]
n100 = gray2int(gc100)
if n100 in [0, 5, 6]:
return None
if n100 == 7:
n100 = 5
if n500%2:
n100 = 6 - n100
alt = (n500*500 + n100*100) - 1300
return alt
def gray2int(graystr):
"""Convert greycode to binary"""
num = bin2int(graystr)
num ^= (num >> 8)
num ^= (num >> 4)
num ^= (num >> 2)
num ^= (num >> 1)
return num
def data(msg):
"""Return the data frame in the message, bytes 9 to 22"""
return msg[8:-6]
def allzeros(msg):
"""check if the data bits are all zeros
Args:
msg (String): 28 bytes hexadecimal message string
Returns:
bool: True or False
"""
d = hex2bin(data(msg))
if bin2int(d) > 0:
return False
else:
return True
def wrongstatus(data, sb, msb, lsb):
"""Check if the status bit and field bits are consistency. This Function
is used for checking BDS code versions.
"""
# status bit, most significant bit, least significant bit
status = int(data[sb-1])
value = bin2int(data[msb-1:lsb])
if not status:
if value != 0:
return True
return False

18
pyModeS/decoder/ehs.py Normal file
View File

@@ -0,0 +1,18 @@
from __future__ import absolute_import, print_function, division
import warnings
from pyModeS.decoder.bds.bds40 import *
from pyModeS.decoder.bds.bds50 import *
from pyModeS.decoder.bds.bds60 import *
from pyModeS.decoder.bds import infer
warnings.simplefilter('once', DeprecationWarning)
warnings.warn("pms.ehs module is deprecated. Please use pms.commb instead.", DeprecationWarning)
def BDS(msg):
warnings.warn("pms.ehs.BDS() is deprecated, use pms.bds.infer() instead.", DeprecationWarning)
return infer(msg)
def icao(msg):
from pyModeS.decoder.common import icao
return icao(msg)

10
pyModeS/decoder/els.py Normal file
View File

@@ -0,0 +1,10 @@
from __future__ import absolute_import, print_function, division
from pyModeS.decoder.bds.bds10 import *
from pyModeS.decoder.bds.bds17 import *
from pyModeS.decoder.bds.bds20 import *
from pyModeS.decoder.bds.bds30 import *
import warnings
warnings.simplefilter('once', DeprecationWarning)
warnings.warn("pms.els module is deprecated. Please use pms.commb instead.", DeprecationWarning)

21
pyModeS/decoder/surv.py Normal file
View File

@@ -0,0 +1,21 @@
# Copyright (C) 2018 Junzi Sun (TU Delft)
# This program is free software: you can redistribute it and/or modify
# it under the terms of the GNU General Public License as published by
# the Free Software Foundation, either version 3 of the License, or
# (at your option) any later version.
# This program is distributed in the hope that it will be useful,
# but WITHOUT ANY WARRANTY; without even the implied warranty of
# MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
# GNU General Public License for more details.
# You should have received a copy of the GNU General Public License
# along with this program. If not, see <http://www.gnu.org/licenses/>.
"""
Warpper for short roll call surveillance replies DF=4/5
"""
from __future__ import absolute_import, print_function, division
from pyModeS.decoder import common

View File

@@ -0,0 +1,120 @@
NA = None
TC_NUCp_lookup = {
0:0, 5:9, 6:8, 7:7, 8:6,
9:9, 10:8, 11:7, 12:6, 13:5, 14:4, 15:3, 16:2, 17:1, 18:0,
20:9, 21:8, 22:0
}
TC_NICv1_lookup = {
5:11, 6:10, 7:9, 8:0,
9:11, 10:10, 11:{1:9, 0:8}, 12:7, 13:6, 14:5, 15:4, 16:{1:3, 0:2}, 17:1, 18:0,
20:11, 21:10, 22:0
}
TC_NICv2_lookup = {
5:11, 6:10, 7:{2:9, 0:8}, 8:{3:7, 2:6, 1:6, 0:0},
9:11, 10:10, 11:{3:9, 0:8}, 12:7, 13:6, 14:5, 15:4, 16:{3:3, 0:2}, 17:1, 18:0,
20:11, 21:10, 22:0
}
NUCp = {
9: {'HPL':7.5, 'RCu':3, 'RCv':4},
8: {'HPL':25, 'RCu':10, 'RCv':15},
7: {'HPL':185, 'RCu':93, 'RCv':NA},
6: {'HPL':370, 'RCu':185, 'RCv':NA},
5: {'HPL':926, 'RCu':463, 'RCv':NA},
4: {'HPL':1852, 'RCu':926, 'RCv':NA},
3: {'HPL':3704, 'RCu':1852, 'RCv':NA},
2: {'HPL':18520, 'RCu':9260, 'RCv':NA},
1: {'HPL':37040, 'RCu':18520, 'RCv':NA},
0: {'HPL':NA, 'RCu':NA, 'RCv':NA},
}
NUCv = {
0: {'HVE':NA, 'VVE':NA},
1: {'HVE':10, 'VVE':15.2},
2: {'HVE':3, 'VVE':4.5},
3: {'HVE':1, 'VVE':1.5},
4: {'HVE':0.3, 'VVE':0.46},
}
NACp = {
11: {'EPU': 3, 'VEPU': 4},
10: {'EPU': 10, 'VEPU': 15},
9: {'EPU': 30, 'VEPU': 45},
8: {'EPU': 93, 'VEPU': NA},
7: {'EPU': 185, 'VEPU': NA},
6: {'EPU': 556, 'VEPU': NA},
5: {'EPU': 926, 'VEPU': NA},
4: {'EPU': 1852, 'VEPU': NA},
3: {'EPU': 3704, 'VEPU': NA},
2: {'EPU': 7408, 'VEPU': NA},
1: {'EPU': 18520, 'VEPU': NA},
0: {'EPU': NA, 'VEPU': NA},
}
NACv = {
0: {'HFOMr':NA, 'VFOMr':NA},
1: {'HFOMr':10, 'VFOMr':15.2},
2: {'HFOMr':3, 'VFOMr':4.5},
3: {'HFOMr':1, 'VFOMr':1.5},
4: {'HFOMr':0.3, 'VFOMr':0.46},
}
SIL = {
3: {'PE_RCu': 1e-7, 'PE_VPL': 2e-7},
2: {'PE_RCu': 1e-5, 'PE_VPL': 1e-5},
1: {'PE_RCu': 1e-3, 'PE_VPL': 1e-3},
0: {'PE_RCu': NA, 'PE_VPL': NA},
}
NICv1 = {
# NIC is used as the index at second Level
11: {0: {'Rc': 7.5, 'VPL': 11}},
10: {0: {'Rc': 25, 'VPL': 37.5}},
9: {1: {'Rc': 75, 'VPL': 112}},
8: {0: {'Rc': 185, 'VPL': NA}},
7: {0: {'Rc': 370, 'VPL': NA}},
6: {
0: {'Rc': 926, 'VPL': NA},
1: {'Rc': 1111, 'VPL': NA},
},
5: {0: {'Rc': 1852, 'VPL': NA}},
4: {0: {'Rc': 3702, 'VPL': NA}},
3: {1: {'Rc': 7408, 'VPL': NA}},
2: {0: {'Rc': 14008, 'VPL': NA}},
1: {0: {'Rc': 37000, 'VPL': NA}},
0: {0: {'Rc': NA, 'VPL': NA}},
}
NICv2 = {
# Decimal value of [NICa NICb/NICc] is used as the index at second Level
11: {0: {'Rc': 7.5}},
10: {0: {'Rc': 25}},
9: {
2: {'Rc': 75},
3: {'Rc': 75},
},
8: {0: {'Rc': 185}},
7: {
0: {'Rc': 370},
3: {'Rc': 370},
},
6: {
0: {'Rc': 926},
1: {'Rc': 556},
2: {'Rc': 556},
3: {'Rc': 1111},
},
5: {0: {'Rc': 1852}},
4: {0: {'Rc': 3702}},
3: {3: {'Rc': 7408}},
2: {0: {'Rc': 14008}},
1: {0: {'Rc': 37000}},
0: {0: {'Rc': NA}},
}

View File

@@ -1,416 +0,0 @@
"""
A python package for decoding ModeS (DF20, DF21) messages.
Copyright (C) 2016 Junzi Sun (TU Delft)
This program is free software: you can redistribute it and/or modify
it under the terms of the GNU General Public License as published by
the Free Software Foundation, either version 3 of the License, or
(at your option) any later version.
This program is distributed in the hope that it will be useful,
but WITHOUT ANY WARRANTY; without even the implied warranty of
MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
GNU General Public License for more details.
You should have received a copy of the GNU General Public License
along with this program. If not, see <http://www.gnu.org/licenses/>.
"""
from . import util
from .util import crc
def df(msg):
"""Get the downlink format (DF) number
Args:
msg (String): 28 bytes hexadecimal message string
Returns:
int: DF number
"""
return util.df(msg)
def data(msg):
"""Return the data frame in the message, bytes 9 to 22"""
return msg[8:22]
def icao(msg):
"""Calculate the ICAO address from an Mode-S message
with DF4, DF5, DF20, DF21
Args:
msg (String): 28 bytes hexadecimal message string
Returns:
String: ICAO address in 6 bytes hexadecimal string
"""
if df(msg) not in (4, 5, 20, 21):
# raise RuntimeError("Message DF must be in (4, 5, 20, 21)")
return None
c0 = util.bin2int(crc(msg, encode=True))
c1 = util.hex2int(msg[-6:])
icao = '%06X' % (c0 ^ c1)
return icao
def checkbits(data, sb, msb, lsb):
"""Check if the status bit and field bits are consistency. This Function
is used for checking BDS code versions.
"""
# status bit, most significant bit, least significant bit
status = int(data[sb-1])
value = util.bin2int(data[msb-1:lsb])
if not status:
if value != 0:
return False
return True
# ------------------------------------------
# DF 20/21, BDS 2,0
# ------------------------------------------
def isBDS20(msg):
"""Check if a message is likely to be BDS code 2,0
Args:
msg (String): 28 bytes hexadecimal message string
Returns:
bool: True or False
"""
# status bit 1, 14, and 27
d = util.hex2bin(data(msg))
result = True
if util.bin2int(d[0:4]) != 2 or util.bin2int(d[4:8]) != 0:
result &= False
cs = callsign(msg)
if '#' in cs:
result &= False
return result
def callsign(msg):
"""Aircraft callsign
Args:
msg (String): 28 bytes hexadecimal message (BDS40) string
Returns:
string: callsign, max. 8 chars
"""
chars = '#ABCDEFGHIJKLMNOPQRSTUVWXYZ#####_###############0123456789######'
d = util.hex2bin(data(msg))
cs = ''
cs += chars[util.bin2int(d[8:14])]
cs += chars[util.bin2int(d[14:20])]
cs += chars[util.bin2int(d[20:26])]
cs += chars[util.bin2int(d[26:32])]
cs += chars[util.bin2int(d[32:38])]
cs += chars[util.bin2int(d[38:44])]
cs += chars[util.bin2int(d[44:50])]
cs += chars[util.bin2int(d[50:56])]
return cs
# ------------------------------------------
# DF 20/21, BDS 4,0
# ------------------------------------------
def isBDS40(msg):
"""Check if a message is likely to be BDS code 4,0
Args:
msg (String): 28 bytes hexadecimal message string
Returns:
bool: True or False
"""
# status bit 1, 14, and 27
d = util.hex2bin(data(msg))
result = True
result = result & checkbits(d, 1, 2, 13) \
& checkbits(d, 14, 15, 26) & checkbits(d, 27, 28, 39)
# bits 40-47 and 52-53 shall all be zero
if util.bin2int(d[39:47]) != 0:
result &= False
if util.bin2int(d[51:53]) != 0:
result &= False
return result
def alt_mcp(msg):
"""Selected altitude, MCP/FCU
Args:
msg (String): 28 bytes hexadecimal message (BDS40) string
Returns:
int: altitude in feet
"""
d = util.hex2bin(data(msg))
alt = util.bin2int(d[1:13]) * 16 # ft
return alt
def alt_fms(msg):
"""Selected altitude, FMS
Args:
msg (String): 28 bytes hexadecimal message (BDS40) string
Returns:
int: altitude in feet
"""
d = util.hex2bin(data(msg))
alt = util.bin2int(d[14:26]) * 16 # ft
return alt
def pbaro(msg):
"""Barometric pressure setting
Args:
msg (String): 28 bytes hexadecimal message (BDS40) string
Returns:
float: pressure in millibar
"""
d = util.hex2bin(data(msg))
p = util.bin2int(d[27:39]) * 0.1 + 800 # millibar
return p
# ------------------------------------------
# DF 20/21, BDS 5,0
# ------------------------------------------
def isBDS50(msg):
"""Check if a message is likely to be BDS code 5,0
Args:
msg (String): 28 bytes hexadecimal message string
Returns:
bool: True or False
"""
# status bit 1, 12, 24, 35, 46
d = util.hex2bin(data(msg))
result = True
result = result & checkbits(d, 1, 3, 11) & checkbits(d, 12, 13, 23) \
& checkbits(d, 24, 25, 34) & checkbits(d, 35, 36, 45) \
& checkbits(d, 46, 47, 56)
if d[2:11] == "000000000":
result &= True
else:
if abs(roll(msg)) > 30:
result &= False
if gs(msg) > 500:
result &= False
if tas(msg) > 500:
result &= False
if abs(tas(msg) - gs(msg)) > 100:
result &= False
return result
def roll(msg):
"""Aircraft roll angle
Args:
msg (String): 28 bytes hexadecimal message (BDS50) string
Returns:
float: angle in degrees,
negative->left wing down, positive->right wing down
"""
d = util.hex2bin(data(msg))
sign = int(d[1]) # 1 -> left wing down
value = util.bin2int(d[2:11]) * 45 / 256.0 # degree
angle = -1 * value if sign else value
return round(angle, 1)
def track(msg):
"""True track angle
Args:
msg (String): 28 bytes hexadecimal message (BDS50) string
Returns:
float: angle in degrees to true north (from 0 to 360)
"""
d = util.hex2bin(data(msg))
sign = int(d[12]) # 1 -> west
value = util.bin2int(d[13:23]) * 90 / 512.0 # degree
angle = 360 - value if sign else value
return round(angle, 1)
def gs(msg):
"""Aircraft ground speed
Args:
msg (String): 28 bytes hexadecimal message (BDS50) string
Returns:
int: ground speed in knots
"""
d = util.hex2bin(data(msg))
spd = util.bin2int(d[24:34]) * 2 # kts
return spd
def rtrack(msg):
"""Track angle rate
Args:
msg (String): 28 bytes hexadecimal message (BDS50) string
Returns:
float: angle rate in degrees/second
"""
d = util.hex2bin(data(msg))
sign = int(d[35]) # 1 -> minus
value = util.bin2int(d[36:45]) * 8 / 256.0 # degree / sec
angle = -1 * value if sign else value
return round(angle, 3)
def tas(msg):
"""Aircraft true airspeed
Args:
msg (String): 28 bytes hexadecimal message (BDS50) string
Returns:
int: true airspeed in knots
"""
d = util.hex2bin(data(msg))
spd = util.bin2int(d[46:56]) * 2 # kts
return spd
# ------------------------------------------
# DF 20/21, BDS 6,0
# ------------------------------------------
def isBDS60(msg):
"""Check if a message is likely to be BDS code 6,0
Args:
msg (String): 28 bytes hexadecimal message string
Returns:
bool: True or False
"""
# status bit 1, 13, 24, 35, 46
d = util.hex2bin(data(msg))
result = True
result = result & checkbits(d, 1, 2, 12) & checkbits(d, 13, 14, 23) \
& checkbits(d, 24, 25, 34) & checkbits(d, 35, 36, 45) \
& checkbits(d, 46, 47, 56)
if not (1 < ias(msg) < 500):
result &= False
if not (0.0 < mach(msg) < 1.0):
result &= False
if abs(baro_vr(msg)) > 5000:
result &= False
if abs(ins_vr(msg)) > 5000:
result &= False
return result
def heading(msg):
"""Megnetic heading of aircraft
Args:
msg (String): 28 bytes hexadecimal message (BDS60) string
Returns:
float: heading in degrees to megnetic north (from 0 to 360)
"""
d = util.hex2bin(data(msg))
sign = int(d[1]) # 1 -> west
value = util.bin2int(d[2:12]) * 90 / 512.0 # degree
hdg = 360 - value if sign else value
return round(hdg, 1)
def ias(msg):
"""Indicated airspeed
Args:
msg (String): 28 bytes hexadecimal message (BDS60) string
Returns:
int: indicated airspeed in knots
"""
d = util.hex2bin(data(msg))
ias = util.bin2int(d[13:23]) # kts
return ias
def mach(msg):
"""Aircraft MACH number
Args:
msg (String): 28 bytes hexadecimal message (BDS60) string
Returns:
float: MACH number
"""
d = util.hex2bin(data(msg))
mach = util.bin2int(d[24:34]) * 2.048 / 512.0
return round(mach, 3)
def baro_vr(msg):
"""Vertical rate from barometric measurement
Args:
msg (String): 28 bytes hexadecimal message (BDS60) string
Returns:
int: vertical rate in feet/minutes
"""
d = util.hex2bin(data(msg))
sign = d[35] # 1 -> minus
value = util.bin2int(d[36:45]) * 32 # feet/min
roc = -1*value if sign else value
return roc
def ins_vr(msg):
"""Vertical rate messured by onbard equiments (IRS, AHRS)
Args:
msg (String): 28 bytes hexadecimal message (BDS60) string
Returns:
int: vertical rate in feet/minutes
"""
d = util.hex2bin(data(msg))
sign = d[46] # 1 -> minus
value = util.bin2int(d[47:56]) * 32 # feet/min
roc = -1*value if sign else value
return roc
def BDS(msg):
"""Estimate the most likely BDS code of an message
Args:
msg (String): 28 bytes hexadecimal message string
Returns:
String|None: Version: "BDS40", "BDS50", or "BDS60". Or None, if nothing
matched
"""
is2 = isBDS20(msg)
is4 = isBDS40(msg)
is5 = isBDS50(msg)
is6 = isBDS60(msg)
if is2 and not is4 and not is5 and not is6:
return "BDS20"
elif not is2 and is4 and not is5 and not is6:
return "BDS40"
elif not is2 and not is4 and is5 and not is6:
return "BDS50"
elif not is2 and not is4 and not is5 and is6:
return "BDS60"
else:
return None

View File

@@ -0,0 +1 @@
from __future__ import absolute_import, print_function, division

178
pyModeS/extra/aero.py Normal file
View File

@@ -0,0 +1,178 @@
"""
Functions for aeronautics in this module
- physical quantities always in SI units
- lat,lon,course and heading in degrees
International Standard Atmosphere
p,rho,T = atmos(H) # atmos as function of geopotential altitude H [m]
a = vsound(H) # speed of sound [m/s] as function of H[m]
p = pressure(H) # calls atmos but retruns only pressure [Pa]
T = temperature(H) # calculates temperature [K]
rho = density(H) # calls atmos but retruns only pressure [Pa]
Speed conversion at altitude H[m] in ISA:
Mach = tas2mach(Vtas,H) # true airspeed (Vtas) to mach number conversion
Vtas = mach2tas(Mach,H) # true airspeed (Vtas) to mach number conversion
Vtas = eas2tas(Veas,H) # equivalent airspeed to true airspeed, H in [m]
Veas = tas2eas(Vtas,H) # true airspeed to equivent airspeed, H in [m]
Vtas = cas2tas(Vcas,H) # Vcas to Vtas conversion both m/s, H in [m]
Vcas = tas2cas(Vtas,H) # Vtas to Vcas conversion both m/s, H in [m]
Vcas = mach2cas(Mach,H) # Mach to Vcas conversion Vcas in m/s, H in [m]
Mach = cas2mach(Vcas,H) # Vcas to mach copnversion Vcas in m/s, H in [m]
"""
import numpy as np
"""Aero and geo Constants """
kts = 0.514444 # knot -> m/s
ft = 0.3048 # ft -> m
fpm = 0.00508 # ft/min -> m/s
inch = 0.0254 # inch -> m
sqft = 0.09290304 # 1 square foot
nm = 1852. # nautical mile -> m
lbs = 0.453592 # pound -> kg
g0 = 9.80665 # m/s2, Sea level gravity constant
R = 287.05287 # m2/(s2 x K), gas constant, sea level ISA
p0 = 101325. # Pa, air pressure, sea level ISA
rho0 = 1.225 # kg/m3, air density, sea level ISA
T0 = 288.15 # K, temperature, sea level ISA
gamma = 1.40 # cp/cv for air
gamma1 = 0.2 # (gamma-1)/2 for air
gamma2 = 3.5 # gamma/(gamma-1) for air
beta = -0.0065 # [K/m] ISA temp gradient below tropopause
r_earth = 6371000. # m, average earth radius
a0 = 340.293988 # m/s, sea level speed of sound ISA, sqrt(gamma*R*T0)
def atmos(H):
# H in metres
T = np.maximum(288.15 - 0.0065 * H, 216.65)
rhotrop = 1.225 * (T / 288.15)**4.256848030018761
dhstrat = np.maximum(0., H - 11000.0)
rho = rhotrop * np.exp(-dhstrat / 6341.552161)
p = rho * R * T
return p, rho, T
def temperature(H):
p, r, T = atmos(H)
return T
def pressure(H):
p, r, T = atmos(H)
return p
def density(H):
p, r, T = atmos(H)
return r
def vsound(H):
"""Speed of sound"""
T = temperature(H)
a = np.sqrt(gamma * R * T)
return a
def distance(lat1, lon1, lat2, lon2, H=0):
"""
Compute spherical distance from spherical coordinates.
For two locations in spherical coordinates
(1, theta, phi) and (1, theta', phi')
cosine( arc length ) =
sin phi sin phi' cos(theta-theta') + cos phi cos phi'
distance = rho * arc length
"""
# phi = 90 - latitude
phi1 = np.radians(90.0 - lat1)
phi2 = np.radians(90.0 - lat2)
# theta = longitude
theta1 = np.radians(lon1)
theta2 = np.radians(lon2)
cos = np.sin(phi1) * np.sin(phi2) * np.cos(theta1 - theta2) + np.cos(phi1) * np.cos(phi2)
cos = np.where(cos>1, 1, cos)
arc = np.arccos(cos)
dist = arc * (r_earth + H) # meters, radius of earth
return dist
def bearing(lat1, lon1, lat2, lon2):
lat1 = np.radians(lat1)
lon1 = np.radians(lon1)
lat2 = np.radians(lat2)
lon2 = np.radians(lon2)
x = np.sin(lon2-lon1) * np.cos(lat2)
y = np.cos(lat1) * np.sin(lat2) \
- np.sin(lat1) * np.cos(lat2) * np.cos(lon2-lon1)
initial_bearing = np.arctan2(x, y)
initial_bearing = np.degrees(initial_bearing)
bearing = (initial_bearing + 360) % 360
return bearing
# -----------------------------------------------------
# Speed conversions, altitude H all in meters
# -----------------------------------------------------
def tas2mach(Vtas, H):
"""True Airspeed to Mach number"""
a = vsound(H)
Mach = Vtas/a
return Mach
def mach2tas(Mach, H):
"""Mach number to True Airspeed"""
a = vsound(H)
Vtas = Mach*a
return Vtas
def eas2tas(Veas, H):
"""Equivalent Airspeed to True Airspeed"""
rho = density(H)
Vtas = Veas * np.sqrt(rho0/rho)
return Vtas
def tas2eas(Vtas, H):
"""True Airspeed to Equivalent Airspeed"""
rho = density(H)
Veas = Vtas * np.sqrt(rho/rho0)
return Veas
def cas2tas(Vcas, H):
"""Calibrated Airspeed to True Airspeed"""
p, rho, T = atmos(H)
qdyn = p0*((1.+rho0*Vcas*Vcas/(7.*p0))**3.5-1.)
Vtas = np.sqrt(7.*p/rho*((1.+qdyn/p)**(2./7.)-1.))
return Vtas
def tas2cas(Vtas, H):
"""True Airspeed to Calibrated Airspeed"""
p, rho, T = atmos(H)
qdyn = p*((1.+rho*Vtas*Vtas/(7.*p))**3.5-1.)
Vcas = np.sqrt(7.*p0/rho0*((qdyn/p0+1.)**(2./7.)-1.))
return Vcas
def mach2cas(Mach, H):
"""Mach number to Calibrated Airspeed"""
Vtas = mach2tas(Mach, H)
Vcas = tas2cas(Vtas, H)
return Vcas
def cas2mach(Vcas, H):
"""Calibrated Airspeed to Mach number"""
Vtas = cas2tas(Vcas, H)
Mach = tas2mach(Vtas, H)
return Mach

278
pyModeS/extra/tcpclient.py Normal file
View File

@@ -0,0 +1,278 @@
'''
Stream beast raw data from a TCP server, convert to mode-s messages
'''
from __future__ import print_function, division
import os
import sys
import socket
import time
from threading import Thread
if (sys.version_info > (3, 0)):
PY_VERSION = 3
else:
PY_VERSION = 2
class BaseClient(Thread):
def __init__(self, host, port, rawtype):
Thread.__init__(self)
self.host = host
self.port = port
self.buffer = []
self.rawtype = rawtype
if self.rawtype not in ['avr', 'beast', 'skysense']:
print("rawtype must be either avr, beast or skysense")
os._exit(1)
def connect(self):
while True:
try:
s = socket.socket(socket.AF_INET, socket.SOCK_STREAM)
s.settimeout(10) # 10 second timeout
s.connect((self.host, self.port))
print("Server connected - %s:%s" % (self.host, self.port))
print("collecting ADS-B messages...")
return s
except socket.error as err:
print("Socket connection error: %s. reconnecting..." % err)
time.sleep(3)
def read_avr_buffer(self):
# -- testing --
# for b in self.buffer:
# print(chr(b), b)
# Append message with 0-9,A-F,a-f, until stop sign
messages = []
msg_stop = False
for b in self.buffer:
if b == 59:
msg_stop = True
ts = time.time()
messages.append([self.current_msg, ts])
if b == 42:
msg_stop = False
self.current_msg = ''
if (not msg_stop) and (48<=b<=57 or 65<=b<=70 or 97<=b<=102):
self.current_msg = self.current_msg + chr(b)
self.buffer = []
return messages
def read_beast_buffer(self):
'''
<esc> "1" : 6 byte MLAT timestamp, 1 byte signal level,
2 byte Mode-AC
<esc> "2" : 6 byte MLAT timestamp, 1 byte signal level,
7 byte Mode-S short frame
<esc> "3" : 6 byte MLAT timestamp, 1 byte signal level,
14 byte Mode-S long frame
<esc> "4" : 6 byte MLAT timestamp, status data, DIP switch
configuration settings (not on Mode-S Beast classic)
<esc><esc>: true 0x1a
<esc> is 0x1a, and "1", "2" and "3" are 0x31, 0x32 and 0x33
timestamp:
wiki.modesbeast.com/Radarcape:Firmware_Versions#The_GPS_timestamp
'''
messages_mlat = []
msg = []
i = 0
# process the buffer until the last divider <esc> 0x1a
# then, reset the self.buffer with the remainder
while i < len(self.buffer):
if (self.buffer[i:i+2] == [0x1a, 0x1a]):
msg.append(0x1a)
i += 1
elif (i == len(self.buffer) - 1) and (self.buffer[i] == 0x1a):
# special case where the last bit is 0x1a
msg.append(0x1a)
elif self.buffer[i] == 0x1a:
if i == len(self.buffer) - 1:
# special case where the last bit is 0x1a
msg.append(0x1a)
elif len(msg) > 0:
messages_mlat.append(msg)
msg = []
else:
msg.append(self.buffer[i])
i += 1
# save the reminder for next reading cycle, if not empty
if len(msg) > 0:
reminder = []
for i, m in enumerate(msg):
if (m == 0x1a) and (i < len(msg)-1):
# rewind 0x1a, except when it is at the last bit
reminder.extend([m, m])
else:
reminder.append(m)
self.buffer = [0x1a] + msg
else:
self.buffer = []
# extract messages
messages = []
for mm in messages_mlat:
ts = time.time()
msgtype = mm[0]
# print(''.join('%02X' % i for i in mm))
if msgtype == 0x32:
# Mode-S Short Message, 7 byte, 14-len hexstr
msg = ''.join('%02X' % i for i in mm[8:15])
elif msgtype == 0x33:
# Mode-S Long Message, 14 byte, 28-len hexstr
msg = ''.join('%02X' % i for i in mm[8:22])
else:
# Other message tupe
continue
if len(msg) not in [14, 28]:
# incomplete message
continue
messages.append([msg, ts])
return messages
def read_skysense_buffer(self):
"""
----------------------------------------------------------------------------------
Field SS MS MS MS MS MS MS MS MS MS MS MS MS MS MS TS TS TS TS TS TS RS RS RS
----------------------------------------------------------------------------------
Position: 0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23
----------------------------------------------------------------------------------
SS field - Start character
Position 0:
1 byte = 8 bits
Start character '$'
MS field - Payload
Postion 1 through 14:
14 bytes = 112 bits
Mode-S payload
In case of DF types that only carry 7 bytes of information position 8 through 14 are set to 0x00.
TS field - Time stamp
Position 15 through 20:
6 bytes = 48 bits
Time stamp with fields as:
Lock Status - Status of internal time keeping mechanism
Equal to 1 if operating normally
Bit 47 - 1 bit
Time of day in UTC seconds, between 0 and 86399
Bits 46 through 30 - 17 bits
Nanoseconds into current second, between 0 and 999999999
Bits 29 through 0 - 30 bits
RS field - Signal Level
Position 21 through 23:
3 bytes = 24 bits
RSSI (received signal strength indication) and relative noise level with fields
RNL, Q12.4 unsigned fixed point binary with 4 fractional bits and 8 integer bits.
This is and indication of the noise level of the message. Roughly 40 counts per 10dBm.
Bits 23 through 12 - 12 bits
RSSI, Q12.4 unsigned fixed point binary with 4 fractional bits and 8 integer bits.
This is an indication of the signal level of the received message in ADC counts. Roughly 40 counts per 10dBm.
Bits 11 through 0 - 12 bits
"""
SS_MSGLENGTH = 24
SS_STARTCHAR = 0x24
if len(self.buffer) <= SS_MSGLENGTH:
return None
messages = []
while len(self.buffer) > SS_MSGLENGTH:
i = 0
if self.buffer[i] == SS_STARTCHAR and self.buffer[i+SS_MSGLENGTH] == SS_STARTCHAR:
i += 1
if (self.buffer[i]>>7):
#Long message
payload = self.buffer[i:i+14]
else:
#Short message
payload = self.buffer[i:i+7]
msg = ''.join('%02X' % j for j in payload)
i += 14 #Both message types use 14 bytes
tsbin = self.buffer[i:i+6]
sec = ( (tsbin[0] & 0x7f) << 10) | (tsbin[1] << 2 ) | (tsbin[2] >> 6)
nano = ( (tsbin[2] & 0x3f) << 24) | (tsbin[3] << 16) | (tsbin[4] << 8) | tsbin[5]
ts = sec + nano*1.0e-9
i += 6
#Signal and noise level - Don't care for now
i += 3
self.buffer = self.buffer[SS_MSGLENGTH:]
messages.append( [msg,ts] )
else:
self.buffer = self.buffer[1:]
return messages
def handle_messages(self, messages):
"""re-implement this method to handle the messages"""
for msg, t in messages:
print("%15.9f %s" % (t, msg))
def run(self):
sock = self.connect()
while True:
try:
received = sock.recv(1024)
if PY_VERSION == 2:
received = [ord(i) for i in received]
self.buffer.extend(received)
# print(''.join(x.encode('hex') for x in self.buffer))
# process self.buffer when it is longer enough
# if len(self.buffer) < 2048:
# continue
# -- Removed!! Cause delay in low data rate scenario --
if self.rawtype == 'beast':
messages = self.read_beast_buffer()
elif self.rawtype == 'avr':
messages = self.read_avr_buffer()
elif self.rawtype == 'skysense':
messages = self.read_skysense_buffer()
if not messages:
continue
else:
self.handle_messages(messages)
time.sleep(0.001)
except Exception as e:
print("Unexpected Error:", e)
try:
sock = self.connect()
except Exception as e:
print("Unexpected Error:", e)
if __name__ == '__main__':
# for testing purpose only
host = sys.argv[1]
port = int(sys.argv[2])
rawtype = sys.argv[3]
client = BaseClient(host=host, port=port, rawtype=rawtype)
client.daemon = True
client.run()

View File

120
pyModeS/streamer/modeslive Executable file
View File

@@ -0,0 +1,120 @@
#!/usr/bin/env python
from __future__ import print_function, division
import os
import sys
import time
import argparse
import curses
from threading import Lock
import pyModeS as pms
from pyModeS.extra.tcpclient import BaseClient
from pyModeS.streamer.stream import Stream
from pyModeS.streamer.screen import Screen
LOCK = Lock()
ADSB_MSG = []
ADSB_TS = []
COMMB_MSG = []
COMMB_TS = []
parser = argparse.ArgumentParser()
parser.add_argument('--server', help='server address or IP', required=True)
parser.add_argument('--port', help='raw data port', required=True)
parser.add_argument('--rawtype', help='beast, avr or skysense', required=True)
parser.add_argument('--latlon', help='receiver position', nargs=2, metavar=('LAT', 'LON'), required=True)
parser.add_argument('--show-uncertainty', dest='uncertainty', help='display uncertaint values, default off', action='store_true', required=False, default=False)
parser.add_argument('--dumpto', help='folder to dump decoded output', required=False, default=None)
args = parser.parse_args()
SERVER = args.server
PORT = int(args.port)
RAWTYPE = args.rawtype
LAT0 = float(args.latlon[0])
LON0 = float(args.latlon[1])
UNCERTAINTY = args.uncertainty
DUMPTO = args.dumpto
if DUMPTO is not None:
# append to current folder except root is given
if DUMPTO[0] != '/':
DUMPTO = os.getcwd() + '/' + DUMPTO
if not os.path.isdir(DUMPTO):
print('Error: dump folder (%s) does not exist' % DUMPTO)
sys.exit(1)
class ModesClient(BaseClient):
def __init__(self, host, port, rawtype):
super(ModesClient, self).__init__(host, port, rawtype)
def handle_messages(self, messages):
local_buffer_adsb_msg = []
local_buffer_adsb_ts = []
local_buffer_ehs_msg = []
local_buffer_ehs_ts = []
for msg, t in messages:
if len(msg) < 28: # only process long messages
continue
df = pms.df(msg)
if df == 17 or df == 18:
local_buffer_adsb_msg.append(msg)
local_buffer_adsb_ts.append(t)
elif df == 20 or df == 21:
local_buffer_ehs_msg.append(msg)
local_buffer_ehs_ts.append(t)
else:
continue
LOCK.acquire()
ADSB_MSG.extend(local_buffer_adsb_msg)
ADSB_TS.extend(local_buffer_adsb_ts)
COMMB_MSG.extend(local_buffer_ehs_msg)
COMMB_TS.extend(local_buffer_ehs_ts)
LOCK.release()
# redirect all stdout to null, avoiding messing up with the screen
sys.stdout = open(os.devnull, 'w')
client = ModesClient(host=SERVER, port=PORT, rawtype=RAWTYPE)
client.daemon = True
client.start()
stream = Stream(lat0=LAT0, lon0=LON0, dumpto=DUMPTO)
try:
screen = Screen(uncertainty=UNCERTAINTY)
screen.daemon = True
screen.start()
while True:
if len(ADSB_MSG) > 200:
LOCK.acquire()
stream.process_raw(ADSB_TS, ADSB_MSG, COMMB_TS, COMMB_MSG)
ADSB_MSG = []
ADSB_TS = []
COMMB_MSG = []
COMMB_TS = []
LOCK.release()
acs = stream.get_aircraft()
try:
screen.update_data(acs)
screen.update()
time.sleep(0.02)
except KeyboardInterrupt:
raise
except:
continue
except KeyboardInterrupt:
sys.exit(0)
finally:
curses.endwin()

183
pyModeS/streamer/screen.py Normal file
View File

@@ -0,0 +1,183 @@
from __future__ import print_function, division
import os
import curses
import numpy as np
import time
from threading import Thread
COLUMNS = [
('call', 10),
('lat', 10),
('lon', 10),
('alt', 7),
('gs', 5),
('tas', 5),
('ias', 5),
('mach', 7),
('roc', 7),
('trk', 10),
('hdg', 10),
('live', 6),
]
UNCERTAINTY_COLUMNS = [
('|', 5),
('ver', 4),
('HPL', 5),
('RCu', 5),
('RCv', 5),
('HVE', 5),
('VVE', 5),
('Rc', 4),
('VPL', 5),
('EPU', 5),
('VEPU', 6),
('HFOMr', 7),
('VFOMr', 7),
('PE_RCu', 8),
('PE_VPL', 8),
]
class Screen(Thread):
def __init__(self, uncertainty=False):
Thread.__init__(self)
self.screen = curses.initscr()
curses.noecho()
curses.mousemask(1)
self.screen.keypad(True)
self.y = 3
self.x = 1
self.offset = 0
self.acs = {}
self.lock_icao = None
self.columns = COLUMNS
if uncertainty:
self.columns.extend(UNCERTAINTY_COLUMNS)
def reset_cursor_pos(self):
self.screen.move(self.y, self.x)
def update_data(self, acs):
self.acs = acs
def draw_frame(self):
self.screen.border(0)
self.screen.addstr(0, 2, "Online aircraft [%d] ('Ctrl+C' to exit, 'Enter' to lock one)" % len(self.acs))
def update(self):
if len(self.acs) == 0:
return
resized = curses.is_term_resized(self.scr_h, self.scr_w)
if resized is True:
self.scr_h, self.scr_w = self.screen.getmaxyx()
self.screen.clear()
curses.resizeterm(self.scr_h, self.scr_w)
self.screen.refresh()
self.draw_frame()
row = 1
header = ' icao'
for c, cw in self.columns:
header += (cw-len(c))*' ' + c
# fill end with spaces
header += (self.scr_w - 2 - len(header)) * ' '
if len(header) > self.scr_w - 2:
header = header[:self.scr_w-3] + '>'
self.screen.addstr(row, 1, header)
row +=1
self.screen.addstr(row, 1, '-'*(self.scr_w-2))
icaos = np.array(list(self.acs.keys()))
icaos = np.sort(icaos)
for row in range(3, self.scr_h - 3):
icao = None
idx = row + self.offset - 3
if idx > len(icaos) - 1:
line = ' '*(self.scr_w-2)
else:
line = ''
icao = icaos[idx]
ac = self.acs[icao]
line += icao
for c, cw in self.columns:
if c=='|':
val = '|'
elif c=='live':
val = str(int(time.time() - ac[c]))+'s'
elif ac[c] is None:
val = ''
else:
val = ac[c]
val_str = str(val)
line += (cw-len(val_str))*' ' + val_str
# fill end with spaces
line += (self.scr_w - 2 - len(line)) * ' '
if len(line) > self.scr_w - 2:
line = line[:self.scr_w-3] + '>'
if (icao is not None) and (self.lock_icao == icao):
self.screen.addstr(row, 1, line, curses.A_STANDOUT)
elif row == self.y:
self.screen.addstr(row, 1, line, curses.A_BOLD)
else:
self.screen.addstr(row, 1, line)
self.screen.addstr(self.scr_h-3, 1, '-'*(self.scr_w-2))
total_page = len(icaos) // (self.scr_h - 4) + 1
current_page = self.offset // (self.scr_h - 4) + 1
self.screen.addstr(self.scr_h-2, 1, '(%d / %d)' % (current_page, total_page))
self.reset_cursor_pos()
def run(self):
self.draw_frame()
self.scr_h, self.scr_w = self.screen.getmaxyx()
while True:
c = self.screen.getch()
if c == curses.KEY_HOME:
self.x = 1
self.y = 1
elif c == curses.KEY_NPAGE:
offset_intent = self.offset + (self.scr_h - 4)
if offset_intent < len(self.acs) - 5:
self.offset = offset_intent
elif c == curses.KEY_PPAGE:
offset_intent = self.offset - (self.scr_h - 4)
if offset_intent > 0:
self.offset = offset_intent
else:
self.offset = 0
elif c == curses.KEY_DOWN :
y_intent = self.y + 1
if y_intent < self.scr_h - 3:
self.y = y_intent
elif c == curses.KEY_UP:
y_intent = self.y - 1
if y_intent > 2:
self.y = y_intent
elif c == curses.KEY_ENTER or c == 10 or c == 13:
self.lock_icao = (self.screen.instr(self.y, 1, 6)).decode()
elif c == curses.KEY_F5:
self.screen.refresh()
self.draw_frame()

255
pyModeS/streamer/stream.py Normal file
View File

@@ -0,0 +1,255 @@
from __future__ import absolute_import, print_function, division
import os
import time
import datetime
import csv
import pyModeS as pms
class Stream():
def __init__(self, lat0, lon0, dumpto=None):
self.acs = dict()
self.lat0 = lat0
self.lon0 = lon0
self.t = 0
self.cache_timeout = 60 # seconds
if dumpto is not None and os.path.isdir(dumpto):
self.dumpto = dumpto
else:
self.dumpto = None
def process_raw(self, adsb_ts, adsb_msgs, commb_ts, commb_msgs, tnow=None):
"""process a chunk of adsb and commb messages recieved in the same
time period.
"""
if tnow is None:
tnow = time.time()
self.t = tnow
local_updated_acs_buffer = []
output_buffer = []
# process adsb message
for t, msg in zip(adsb_ts, adsb_msgs):
icao = pms.icao(msg)
tc = pms.adsb.typecode(msg)
if icao not in self.acs:
self.acs[icao] = {
'live': None,
'call': None,
'lat': None,
'lon': None,
'alt': None,
'gs': None,
'trk': None,
'roc': None,
'tas': None,
'roll': None,
'rtrk': None,
'ias': None,
'mach': None,
'hdg': None,
'ver' : None,
'HPL' : None,
'RCu' : None,
'RCv' : None,
'HVE' : None,
'VVE' : None,
'Rc' : None,
'VPL' : None,
'EPU' : None,
'VEPU' : None,
'HFOMr' : None,
'VFOMr' : None,
'PE_RCu' : None,
'PE_VPL' : None,
}
self.acs[icao]['t'] = t
self.acs[icao]['live'] = int(t)
if 1 <= tc <= 4:
cs = pms.adsb.callsign(msg)
self.acs[icao]['call'] = cs
output_buffer.append([t, icao, 'cs', cs])
if (5 <= tc <= 8) or (tc == 19):
vdata = pms.adsb.velocity(msg)
if vdata is None:
continue
spd, trk, roc, tag = vdata
if tag != 'GS':
continue
if (spd is None) or (trk is None):
continue
self.acs[icao]['gs'] = spd
self.acs[icao]['trk'] = trk
self.acs[icao]['roc'] = roc
self.acs[icao]['tv'] = t
output_buffer.append([t, icao, 'gs', spd])
output_buffer.append([t, icao, 'trk', trk])
output_buffer.append([t, icao, 'roc', roc])
if (5 <= tc <= 18):
oe = pms.adsb.oe_flag(msg)
self.acs[icao][oe] = msg
self.acs[icao]['t'+str(oe)] = t
if ('tpos' in self.acs[icao]) and (t - self.acs[icao]['tpos'] < 180):
# use single message decoding
rlat = self.acs[icao]['lat']
rlon = self.acs[icao]['lon']
latlon = pms.adsb.position_with_ref(msg, rlat, rlon)
elif ('t0' in self.acs[icao]) and ('t1' in self.acs[icao]) and \
(abs(self.acs[icao]['t0'] - self.acs[icao]['t1']) < 10):
# use multi message decoding
try:
latlon = pms.adsb.position(
self.acs[icao][0],
self.acs[icao][1],
self.acs[icao]['t0'],
self.acs[icao]['t1'],
self.lat0, self.lon0
)
except:
# mix of surface and airborne position message
continue
else:
latlon = None
if latlon is not None:
self.acs[icao]['tpos'] = t
self.acs[icao]['lat'] = latlon[0]
self.acs[icao]['lon'] = latlon[1]
alt = pms.adsb.altitude(msg)
self.acs[icao]['alt'] = alt
output_buffer.append([t, icao, 'lat', latlon[0]])
output_buffer.append([t, icao, 'lon', latlon[1]])
output_buffer.append([t, icao, 'alt', alt])
local_updated_acs_buffer.append(icao)
# Uncertainty & accuracy
ac = self.acs[icao]
if 9 <= tc <= 18:
ac['nic_bc'] = pms.adsb.nic_b(msg)
if (5 <= tc <= 8) or (9 <= tc <= 18) or (20 <= tc <= 22):
ac['HPL'], ac['RCu'], ac['RCv'] = pms.adsb.nuc_p(msg)
if (ac['ver'] == 1) and ('nic_s' in ac.keys()):
ac['Rc'], ac['VPL'] = pms.adsb.nic_v1(msg, ac['nic_s'])
elif (ac['ver'] == 2) and ('nic_a' in ac.keys()) and ('nic_bc' in ac.keys()):
ac['Rc'] = pms.adsb.nic_v2(msg, ac['nic_a'], ac['nic_bc'])
if tc == 19:
ac['HVE'], ac['VVE'] = pms.adsb.nuc_v(msg)
if ac['ver'] in [1, 2]:
ac['HFOMr'], ac['VFOMr'] = pms.adsb.nac_v(msg)
if tc == 29:
ac['PE_RCu'], ac['PE_VPL'], ac['base'] = pms.adsb.sil(msg, ac['ver'])
ac['EPU'], ac['VEPU'] = pms.adsb.nac_p(msg)
if tc == 31:
ac['ver'] = pms.adsb.version(msg)
ac['EPU'], ac['VEPU'] = pms.adsb.nac_p(msg)
ac['PE_RCu'], ac['PE_VPL'], ac['sil_base'] = pms.adsb.sil(msg, ac['ver'])
if ac['ver'] == 1:
ac['nic_s'] = pms.adsb.nic_s(msg)
elif ac['ver'] == 2:
ac['nic_a'], ac['nic_bc'] = pms.adsb.nic_a_c(msg)
# process commb message
for t, msg in zip(commb_ts, commb_msgs):
icao = pms.icao(msg)
if icao not in self.acs:
continue
bds = pms.bds.infer(msg)
if bds == 'BDS50':
roll50 = pms.commb.roll50(msg)
trk50 = pms.commb.trk50(msg)
rtrk50 = pms.commb.rtrk50(msg)
gs50 = pms.commb.gs50(msg)
tas50 = pms.commb.tas50(msg)
self.acs[icao]['t50'] = t
if tas50:
self.acs[icao]['tas'] = tas50
output_buffer.append([t, icao, 'tas50', tas50])
if roll50:
self.acs[icao]['roll'] = roll50
output_buffer.append([t, icao, 'roll50', roll50])
if rtrk50:
self.acs[icao]['rtrk'] = rtrk50
output_buffer.append([t, icao, 'rtrk50', rtrk50])
if trk50:
output_buffer.append([t, icao, 'trk50', trk50])
if gs50:
output_buffer.append([t, icao, 'gs50', gs50])
elif bds == 'BDS60':
ias60 = pms.commb.ias60(msg)
hdg60 = pms.commb.hdg60(msg)
mach60 = pms.commb.mach60(msg)
roc60baro = pms.commb.vr60baro(msg)
roc60ins = pms.commb.vr60ins(msg)
if ias60 or hdg60 or mach60:
self.acs[icao]['t60'] = t
if ias60:
self.acs[icao]['ias'] = ias60
if hdg60:
self.acs[icao]['hdg'] = hdg60
if mach60:
self.acs[icao]['mach'] = mach60
if roc60baro:
output_buffer.append([t, icao, 'roc60baro', roc60baro])
if roc60ins:
output_buffer.append([t, icao, 'roc60ins', roc60ins])
# clear up old data
for icao in list(self.acs.keys()):
if self.t - self.acs[icao]['live'] > self.cache_timeout:
del self.acs[icao]
continue
if self.dumpto is not None:
dh = str(datetime.datetime.now().strftime("%Y%m%d_%H"))
fn = self.dumpto + '/pymodes_dump_%s.csv' % dh
output_buffer.sort(key=lambda x: x[0])
with open(fn, "a") as f:
writer = csv.writer(f)
writer.writerows(output_buffer)
return
def get_aircraft(self):
"""all aircraft that are stored in memeory"""
acs = self.acs
icaos = list(acs.keys())
for icao in icaos:
if acs[icao]['lat'] is None:
acs.pop(icao)
return acs

View File

@@ -1,81 +0,0 @@
"""
Common functions for ADS-B and Mode-S EHS decoder
Copyright (C) 2015 Junzi Sun (TU Delft)
This program is free software: you can redistribute it and/or modify
it under the terms of the GNU General Public License as published by
the Free Software Foundation, either version 3 of the License, or
(at your option) any later version.
This program is distributed in the hope that it will be useful,
but WITHOUT ANY WARRANTY; without even the implied warranty of
MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
GNU General Public License for more details.
You should have received a copy of the GNU General Public License
along with this program. If not, see <http://www.gnu.org/licenses/>.
"""
import math
# the polynominal generattor code for CRC
GENERATOR = "1111111111111010000001001"
def hex2bin(hexstr):
"""Convert a hexdecimal string to binary string, with zero fillings. """
scale = 16
num_of_bits = len(hexstr) * math.log(scale, 2)
binstr = bin(int(hexstr, scale))[2:].zfill(int(num_of_bits))
return binstr
def bin2int(binstr):
return int(binstr, 2)
def hex2int(hexstr):
return int(hexstr, 16)
def df(msg):
"""Decode Downlink Format vaule, bits 1 to 5."""
msgbin = hex2bin(msg)
return bin2int(msgbin[0:5])
def crc(msg, encode=False):
"""Mode-S Cyclic Redundancy Check
Detect if bit error occurs in the Mode-S message
Args:
msg (string): 28 bytes hexadecimal message string
encode (bool): True to encode the date only and return the checksum
Returns:
string: message checksum, or partity bits (encoder)
"""
msgbin = list(hex2bin(msg))
if encode:
msgbin[-24:] = ['0'] * 24
# loop all bits, except last 24 piraty bits
for i in range(len(msgbin)-24):
# if 1, perform modulo 2 multiplication,
if msgbin[i] == '1':
for j in range(len(GENERATOR)):
# modulo 2 multiplication = XOR
msgbin[i+j] = str((int(msgbin[i+j]) ^ int(GENERATOR[j])))
# last 24 bits
reminder = ''.join(msgbin[-24:])
return reminder
def floor(x):
""" Mode-S floor function
Defined as the greatest integer value k, such that k <= x
eg.: floor(3.6) = 3, while floor(-3.6) = -4
"""
return int(math.floor(x))

View File

@@ -3,6 +3,13 @@
See:
https://packaging.python.org/en/latest/distributing.html
https://github.com/pypa/sampleproject
Steps for deploying a new verison:
1. Increase the version number
2. remove the old deployment under [dist] folder
3. run: python setup.py sdist
run: python setup.py bdist_wheel --universal
4. twine upload dist/*
"""
# Always prefer setuptools over distutils
@@ -23,9 +30,9 @@ setup(
# Versions should comply with PEP440. For a discussion on single-sourcing
# the version across setup.py and the project code, see
# https://packaging.python.org/en/latest/single_source_version.html
version='1.0.5',
version='2.0',
description='Python Mode-S Decoder',
description='Python ADS-B/Mode-S Decoder',
long_description=long_description,
# The project's main homepage.
@@ -56,12 +63,12 @@ setup(
# Specify the Python versions you support here. In particular, ensure
# that you indicate whether you support Python 2, Python 3 or both.
'Programming Language :: Python :: 2',
'Programming Language :: Python :: 2.6',
'Programming Language :: Python :: 2.7',
'Programming Language :: Python :: 3',
'Programming Language :: Python :: 3.3',
'Programming Language :: Python :: 3.4',
'Programming Language :: Python :: 3.5',
'Programming Language :: Python :: 3.6',
],
# What does your project relate to?
@@ -79,7 +86,7 @@ setup(
# your project is installed. For an analysis of "install_requires" vs pip's
# requirements files see:
# https://packaging.python.org/en/latest/requirements.html
install_requires=[''],
install_requires=['numpy', 'argparse'],
# List additional groups of dependencies here (e.g. development
# dependencies). You can install these using the following syntax,
@@ -111,4 +118,6 @@ setup(
# 'sample=sample:main',
# ],
# },
scripts=['pyModeS/streamer/modeslive'],
)

View File

@@ -1,3 +0,0 @@
# the inclusion of the tests module is not meant to offer best practices for
# testing in general, but rather to support the `find_packages` example in
# setup.py that excludes installing the "tests" package

File diff suppressed because it is too large Load Diff

File diff suppressed because it is too large Load Diff

File diff suppressed because it is too large Load Diff

View File

@@ -1,202 +0,0 @@
import os, sys, inspect
currentdir = os.path.dirname(os.path.abspath(
inspect.getfile(inspect.currentframe())))
parentdir = os.path.dirname(currentdir)
sys.path.insert(0, parentdir)
import pyModeS as pms
from pyModeS import adsb
from pyModeS import ehs
from pyModeS import util
# === TEST common functions ===
def test_hex2bin():
assert util.hex2bin('6E406B') == "011011100100000001101011"
def test_crc():
# crc decoder
checksum = util.crc("8D406B902015A678D4D220AA4BDA")
assert checksum == "000000000000000000000000"
# crc encoder
parity = util.crc("8D406B902015A678D4D220AA4BDA", encode=True)
assert util.hex2bin("AA4BDA") == parity
# === TEST ADS-B package ===
def test_adsb_icao():
assert adsb.icao("8D406B902015A678D4D220AA4BDA") == "406B90"
def test_adsb_category():
assert adsb.category("8D406B902015A678D4D220AA4BDA") == 5
def test_adsb_callsign():
assert adsb.callsign("8D406B902015A678D4D220AA4BDA") == "EZY85MH_"
def test_adsb_airborne_position():
pos = adsb.airborne_position("8D40058B58C901375147EFD09357",
"8D40058B58C904A87F402D3B8C59",
1446332400, 1446332405)
assert pos == (49.81755, 6.08442)
def test_adsb_airborne_position_with_ref():
pos = adsb.airborne_position_with_ref("8D40058B58C901375147EFD09357",
49.0, 6.0)
assert pos == (49.82410, 6.06785)
pos = adsb.airborne_position_with_ref("8D40058B58C904A87F402D3B8C59",
49.0, 6.0)
assert pos == (49.81755, 6.08442)
def test_adsb_surface_position_with_ref():
pos = adsb.surface_position_with_ref("8FC8200A3AB8F5F893096B22B4A8",
-43.5, 172.5)
assert pos == (-43.48564, 175.87195)
def test_adsb_alt():
assert adsb.altitude("8D40058B58C901375147EFD09357") == 39000
def test_adsb_velocity():
vgs = adsb.velocity("8D485020994409940838175B284F")
vas = adsb.velocity("8DA05F219B06B6AF189400CBC33F")
assert vgs == (159, 182.9, -14, 'GS')
assert vas == (376, 244.0, -37, 'AS')
def test_nic():
assert adsb.nic('8D3C70A390AB11F55B8C57F65FE6') == 0
assert adsb.nic('8DE1C9738A4A430B427D219C8225') == 1
assert adsb.nic('8D44058880B50006B1773DC2A7E9') == 2
assert adsb.nic('8D44058881B50006B1773DC2A7E9') == 3
assert adsb.nic('8D4AB42A78000640000000FA0D0A') == 4
assert adsb.nic('8D4405887099F5D9772F37F86CB6') == 5
assert adsb.nic('8D4841A86841528E72D9B472DAC2') == 6
assert adsb.nic('8D44057560B9760C0B840A51C89F') == 7
assert adsb.nic('8D40621D58C382D690C8AC2863A7') == 8
assert adsb.nic('8F48511C598D04F12CCF82451642') == 9
assert adsb.nic('8DA4D53A50DBF8C6330F3B35458F') == 10
assert adsb.nic('8D3C4ACF4859F1736F8E8ADF4D67') == 11
# === TEST Mode-S EHS package ===
def test_ehs_icao():
assert ehs.icao("A0001839CA3800315800007448D9") == '400940'
assert ehs.icao("A000139381951536E024D4CCF6B5") == '3C4DD2'
assert ehs.icao("A000029CFFBAA11E2004727281F1") == '4243D0'
def test_ehs_BDS():
assert ehs.BDS("A0001838201584F23468207CDFA5") == 'BDS20'
assert ehs.BDS("A0001839CA3800315800007448D9") == 'BDS40'
assert ehs.BDS("A000139381951536E024D4CCF6B5") == 'BDS50'
assert ehs.BDS("A000029CFFBAA11E2004727281F1") == 'BDS60'
assert ehs.BDS("A0281838CAE9E12FA03FFF2DDDE5") is None
def test_ehs_BDS20_callsign():
assert ehs.callsign("A000083E202CC371C31DE0AA1CCF") == 'KLM1017_'
assert ehs.callsign("A0001993202422F2E37CE038738E") == 'IBK2873_'
def test_ehs_BDS40_functions():
assert ehs.alt_mcp("A000029C85E42F313000007047D3") == 3008
assert ehs.alt_fms("A000029C85E42F313000007047D3") == 3008
assert ehs.pbaro("A000029C85E42F313000007047D3") == 1020.0
def test_ehs_BDS50_functions():
assert ehs.roll("A000139381951536E024D4CCF6B5") == 2.1
assert ehs.track("A000139381951536E024D4CCF6B5") == 114.3
assert ehs.gs("A000139381951536E024D4CCF6B5") == 438
assert ehs.rtrack("A000139381951536E024D4CCF6B5") == 0.125
assert ehs.tas("A000139381951536E024D4CCF6B5") == 424
def test_ehs_BDS60_functions():
assert ehs.heading("A000029CFFBAA11E2004727281F1") == 180.9
assert ehs.ias("A000029CFFBAA11E2004727281F1") == 336
assert ehs.mach("A000029CFFBAA11E2004727281F1") == 0.48
assert ehs.baro_vr("A000029CFFBAA11E2004727281F1") == 0
assert ehs.ins_vr("A000029CFFBAA11E2004727281F1") == -3648
# === Decode sample data file ===
def adsb_decode_all(n=None):
print("===== Decode all ADS-B sample data=====")
import csv
f = open('adsb.csv', 'rt')
msg0 = None
msg1 = None
for i, r in enumerate(csv.reader(f)):
if n and i > n:
break
ts = r[0]
m = r[1]
icao = adsb.icao(m)
tc = adsb.typecode(m)
if 1 <= tc <= 4:
print(ts, m, icao, tc, adsb.category(m), adsb.callsign(m))
if tc == 19:
print(ts, m, icao, tc, adsb.velocity(m))
if 5 <= tc <= 18:
if adsb.oe_flag(m):
msg1 = m
t1 = ts
else:
msg0 = m
t0 = ts
if msg0 and msg1:
pos = adsb.position(msg0, msg1, t0, t1)
alt = adsb.altitude(m)
print(ts, m, icao, tc, pos, alt)
def ehs_decode_all(n=None):
print("===== Decode all Mode-S EHS sample data=====")
import csv
f = open('ehs.csv', 'rt')
for i, r in enumerate(csv.reader(f)):
if n and i > n:
break
ts = r[1]
m = r[2]
icao = ehs.icao(m)
vBDS = ehs.BDS(m)
if vBDS:
if vBDS == "BDS20":
print(ts, m, icao, vBDS, ehs.callsign(m))
if vBDS == "BDS40":
print(ts, m, icao, vBDS, ehs.alt_mcp(m), \
ehs.alt_fms(m), ehs.pbaro(m))
if vBDS == "BDS50":
print(ts, m, icao, vBDS, ehs.roll(m), ehs.track(m), \
ehs.gs(m), ehs.rtrack(m), ehs.tas(m))
if vBDS == "BDS60":
print(ts, m, icao, vBDS, ehs.heading(m), ehs.ias(m), \
ehs.mach(m), ehs.baro_vr(m), ehs.ins_vr(m))
else:
print(ts, m, icao, vBDS)
if __name__ == '__main__':
adsb_decode_all(100)
ehs_decode_all(100)

41
tests/sample_run_adsb.py Normal file
View File

@@ -0,0 +1,41 @@
from __future__ import print_function
from pyModeS import adsb, ehs
# === Decode sample data file ===
def adsb_decode_all(n=None):
print("===== Decode ADS-B sample data=====")
import csv
f = open('tests/data/sample_data_adsb.csv', 'rt')
msg0 = None
msg1 = None
for i, r in enumerate(csv.reader(f)):
if n and i > n:
break
ts = r[0]
m = r[1]
icao = adsb.icao(m)
tc = adsb.typecode(m)
if 1 <= tc <= 4:
print(ts, m, icao, tc, adsb.category(m), adsb.callsign(m))
if tc == 19:
print(ts, m, icao, tc, adsb.velocity(m))
if 5 <= tc <= 18:
if adsb.oe_flag(m):
msg1 = m
t1 = ts
else:
msg0 = m
t0 = ts
if msg0 and msg1:
pos = adsb.position(msg0, msg1, t0, t1)
alt = adsb.altitude(m)
print(ts, m, icao, tc, pos, alt)
if __name__ == '__main__':
adsb_decode_all(n=100)

75
tests/sample_run_commb.py Normal file
View File

@@ -0,0 +1,75 @@
from __future__ import print_function
from pyModeS import commb, common, bds
# === Decode sample data file ===
def bds_info(BDS, m):
if BDS == "BDS10":
info = [commb.ovc10(m)]
elif BDS == "BDS17":
info = ([i[-2:] for i in commb.cap17(m)])
elif BDS == "BDS20":
info = [commb.cs20(m)]
elif BDS == "BDS40":
info = (commb.alt40mcp(m), commb.alt40fms(m), commb.p40baro(m))
elif BDS == "BDS44":
info = (commb.wind44(m), commb.temp44(m), commb.p44(m), commb.hum44(m))
elif BDS == "BDS44REV":
info = (commb.wind44(m, rev=True), commb.temp44(m, rev=True), commb.p44(m, rev=True), commb.hum44(m, rev=True))
elif BDS == "BDS50":
info = (commb.roll50(m), commb.trk50(m), commb.gs50(m), commb.rtrk50(m), commb.tas50(m))
elif BDS == "BDS60":
info = (commb.hdg60(m), commb.ias60(m), commb.mach60(m), commb.vr60baro(m), commb.vr60ins(m))
else:
info = None
return info
def commb_decode_all(df, n=None):
import csv
print("===== Decode Comm-B sample data (DF=%s)=====" % df)
f = open('tests/data/sample_data_commb_df%s.csv' % df, 'rt')
for i, r in enumerate(csv.reader(f)):
if n and i > n:
break
ts = r[0]
m = r[2]
df = common.df(m)
icao = common.icao(m)
BDS = bds.infer(m)
code = common.altcode(m) if df == 20 else common.idcode(m)
if not BDS:
print(ts, m, icao, df, '%5s'%code, 'UNKNOWN')
continue
if len(BDS.split(",")) > 1:
print(ts, m, icao, df, '%5s' % code, end=' ')
for i, _bds in enumerate(BDS.split(",")):
if i == 0:
print(_bds, *bds_info(_bds, m))
else:
print(' ' * 55, _bds, *bds_info(_bds, m))
else:
print(ts, m, icao, df, '%5s'%code, BDS, *bds_info(BDS, m))
if __name__ == '__main__':
commb_decode_all(df=20, n=100)
commb_decode_all(df=21, n=100)

79
tests/test_adsb.py Normal file
View File

@@ -0,0 +1,79 @@
from pyModeS import adsb
# === TEST ADS-B package ===
def test_adsb_icao():
assert adsb.icao("8D406B902015A678D4D220AA4BDA") == "406B90"
def test_adsb_category():
assert adsb.category("8D406B902015A678D4D220AA4BDA") == 5
def test_adsb_callsign():
assert adsb.callsign("8D406B902015A678D4D220AA4BDA") == "EZY85MH_"
def test_adsb_position():
pos = adsb.position("8D40058B58C901375147EFD09357",
"8D40058B58C904A87F402D3B8C59",
1446332400, 1446332405)
assert pos == (49.81755, 6.08442)
def test_adsb_position_with_ref():
pos = adsb.position_with_ref("8D40058B58C901375147EFD09357", 49.0, 6.0)
assert pos == (49.82410, 6.06785)
pos = adsb.position_with_ref("8FC8200A3AB8F5F893096B000000", -43.5, 172.5)
assert pos == (-43.48564, 172.53942)
def test_adsb_airborne_position_with_ref():
pos = adsb.airborne_position_with_ref("8D40058B58C901375147EFD09357",
49.0, 6.0)
assert pos == (49.82410, 6.06785)
pos = adsb.airborne_position_with_ref("8D40058B58C904A87F402D3B8C59",
49.0, 6.0)
assert pos == (49.81755, 6.08442)
def test_adsb_surface_position_with_ref():
pos = adsb.surface_position_with_ref("8FC8200A3AB8F5F893096B000000",
-43.5, 172.5)
assert pos == (-43.48564, 172.53942)
def test_adsb_surface_position():
pos = adsb.surface_position("8CC8200A3AC8F009BCDEF2000000",
"8FC8200A3AB8F5F893096B000000",
0, 2,
-43.496, 172.558)
assert pos == (-43.48564, 172.53942)
def test_adsb_alt():
assert adsb.altitude("8D40058B58C901375147EFD09357") == 39000
def test_adsb_velocity():
vgs = adsb.velocity("8D485020994409940838175B284F")
vas = adsb.velocity("8DA05F219B06B6AF189400CBC33F")
vgs_surface = adsb.velocity("8FC8200A3AB8F5F893096B000000")
assert vgs == (159, 182.88, -832, 'GS')
assert vas == (375, 243.98, -2304, 'TAS')
assert vgs_surface == (19.0, 42.2, 0 , 'GS')
assert adsb.altitude_diff('8D485020994409940838175B284F') == 550
# def test_nic():
# assert adsb.nic('8D3C70A390AB11F55B8C57F65FE6') == 0
# assert adsb.nic('8DE1C9738A4A430B427D219C8225') == 1
# assert adsb.nic('8D44058880B50006B1773DC2A7E9') == 2
# assert adsb.nic('8D44058881B50006B1773DC2A7E9') == 3
# assert adsb.nic('8D4AB42A78000640000000FA0D0A') == 4
# assert adsb.nic('8D4405887099F5D9772F37F86CB6') == 5
# assert adsb.nic('8D4841A86841528E72D9B472DAC2') == 6
# assert adsb.nic('8D44057560B9760C0B840A51C89F') == 7
# assert adsb.nic('8D40621D58C382D690C8AC2863A7') == 8
# assert adsb.nic('8F48511C598D04F12CCF82451642') == 9
# assert adsb.nic('8DA4D53A50DBF8C6330F3B35458F') == 10
# assert adsb.nic('8D3C4ACF4859F1736F8E8ADF4D67') == 11

View File

@@ -0,0 +1,20 @@
from pyModeS import bds
def test_bds_infer():
assert bds.infer("8D406B902015A678D4D220AA4BDA") == 'BDS08'
assert bds.infer("8FC8200A3AB8F5F893096B000000") == 'BDS06'
assert bds.infer("8D40058B58C901375147EFD09357") == 'BDS05'
assert bds.infer("8D485020994409940838175B284F") == 'BDS09'
assert bds.infer("A800178D10010080F50000D5893C") == 'BDS10'
assert bds.infer("A0000638FA81C10000000081A92F") == 'BDS17'
assert bds.infer("A0001838201584F23468207CDFA5") == 'BDS20'
assert bds.infer("A0001839CA3800315800007448D9") == 'BDS40'
assert bds.infer("A000139381951536E024D4CCF6B5") == 'BDS50'
assert bds.infer("A00004128F39F91A7E27C46ADC21") == 'BDS60'
def test_bds_is50or60():
assert bds.is50or60("A0001838201584F23468207CDFA5", 0, 0, 0) == None
assert bds.is50or60("A0000000FFDA9517000464000000", 182, 237, 1250) == 'BDS50'
assert bds.is50or60("A0000000919A5927E23444000000", 413, 54, 18700) == 'BDS60'

49
tests/test_commb.py Normal file
View File

@@ -0,0 +1,49 @@
from pyModeS import bds, commb
# from pyModeS import ehs, els # deprecated
def test_bds20_callsign():
assert bds.bds20.cs20("A000083E202CC371C31DE0AA1CCF") == 'KLM1017_'
assert bds.bds20.cs20("A0001993202422F2E37CE038738E") == 'IBK2873_'
assert commb.cs20("A000083E202CC371C31DE0AA1CCF") == 'KLM1017_'
assert commb.cs20("A0001993202422F2E37CE038738E") == 'IBK2873_'
def test_bds40_functions():
assert bds.bds40.alt40mcp("A000029C85E42F313000007047D3") == 3008
assert bds.bds40.alt40fms("A000029C85E42F313000007047D3") == 3008
assert bds.bds40.p40baro("A000029C85E42F313000007047D3") == 1020.0
assert commb.alt40mcp("A000029C85E42F313000007047D3") == 3008
assert commb.alt40fms("A000029C85E42F313000007047D3") == 3008
assert commb.p40baro("A000029C85E42F313000007047D3") == 1020.0
def test_bds50_functions():
assert bds.bds50.roll50("A000139381951536E024D4CCF6B5") == 2.1
assert bds.bds50.roll50("A0001691FFD263377FFCE02B2BF9") == -0.4 # signed value
assert bds.bds50.trk50("A000139381951536E024D4CCF6B5") == 114.258
assert bds.bds50.gs50("A000139381951536E024D4CCF6B5") == 438
assert bds.bds50.rtrk50("A000139381951536E024D4CCF6B5") == 0.125
assert bds.bds50.tas50("A000139381951536E024D4CCF6B5") == 424
assert commb.roll50("A000139381951536E024D4CCF6B5") == 2.1
assert commb.roll50("A0001691FFD263377FFCE02B2BF9") == -0.4 # signed value
assert commb.trk50("A000139381951536E024D4CCF6B5") == 114.258
assert commb.gs50("A000139381951536E024D4CCF6B5") == 438
assert commb.rtrk50("A000139381951536E024D4CCF6B5") == 0.125
assert commb.tas50("A000139381951536E024D4CCF6B5") == 424
def test_bds60_functions():
assert bds.bds60.hdg60("A00004128F39F91A7E27C46ADC21") == 42.715
assert bds.bds60.ias60("A00004128F39F91A7E27C46ADC21") == 252
assert bds.bds60.mach60("A00004128F39F91A7E27C46ADC21") == 0.42
assert bds.bds60.vr60baro("A00004128F39F91A7E27C46ADC21") == -1920
assert bds.bds60.vr60ins("A00004128F39F91A7E27C46ADC21") == -1920
assert commb.hdg60("A00004128F39F91A7E27C46ADC21") == 42.715
assert commb.ias60("A00004128F39F91A7E27C46ADC21") == 252
assert commb.mach60("A00004128F39F91A7E27C46ADC21") == 0.42
assert commb.vr60baro("A00004128F39F91A7E27C46ADC21") == -1920
assert commb.vr60ins("A00004128F39F91A7E27C46ADC21") == -1920

42
tests/test_common.py Normal file
View File

@@ -0,0 +1,42 @@
from pyModeS import common
def test_hex2bin():
assert common.hex2bin('6E406B') == "011011100100000001101011"
def test_crc_decode():
checksum = common.crc("8D406B902015A678D4D220AA4BDA")
assert checksum == "000000000000000000000000"
def test_crc_encode():
parity = common.crc("8D406B902015A678D4D220AA4BDA", encode=True)
assert common.hex2bin("AA4BDA") == parity
def test_icao():
assert common.icao("8D406B902015A678D4D220AA4BDA") == "406B90"
assert common.icao("A0001839CA3800315800007448D9") == '400940'
assert common.icao("A000139381951536E024D4CCF6B5") == '3C4DD2'
assert common.icao("A000029CFFBAA11E2004727281F1") == '4243D0'
def test_modes_altcode():
assert common.altcode("A02014B400000000000000F9D514") == 32300
def test_modes_idcode():
assert common.idcode("A800292DFFBBA9383FFCEB903D01") == '1346'
def test_graycode_to_altitude():
assert common.gray2alt('00000000010') == -1000
assert common.gray2alt('00000001010') == -500
assert common.gray2alt('00000011011') == -100
assert common.gray2alt('00000011010') == 0
assert common.gray2alt('00000011110') == 100
assert common.gray2alt('00000010011') == 600
assert common.gray2alt('00000110010') == 1000
assert common.gray2alt('00001001001') == 5800
assert common.gray2alt('00011100100') == 10300
assert common.gray2alt('01100011010') == 32000
assert common.gray2alt('01110000100') == 46300
assert common.gray2alt('01010101100') == 50200
assert common.gray2alt('11011110100') == 73200
assert common.gray2alt('10000000011') == 126600
assert common.gray2alt('10000000001') == 126700

9
tox.ini Normal file
View File

@@ -0,0 +1,9 @@
[tox]
toxworkdir = /tmp/tox
envlist = py2,py3
[testenv]
deps =
pytest
numpy
commands = py.test