gr-air-modes/python/modes_parse.py

256 lines
8.6 KiB
Python

#
# Copyright 2010 Nick Foster
#
# This file is part of gr-air-modes
#
# gr-air-modes 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, or (at your option)
# any later version.
#
# gr-air-modes 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 gr-air-modes; see the file COPYING. If not, write to
# the Free Software Foundation, Inc., 51 Franklin Street,
# Boston, MA 02110-1301, USA.
#
import time, os, sys
from string import split, join
from altitude import decode_alt
from cpr import cpr_decode
import math
class modes_parse:
def __init__(self, mypos):
self.my_location = mypos
self.cpr_decoder = cpr_decoder(self.my_location)
def parse0(self, shortdata, parity, ecc):
# shortdata = long(shortdata, 16)
#parity = long(parity)
vs = bool(shortdata >> 26 & 0x1) #ground sensor -- airborne when 0
cc = bool(shortdata >> 25 & 0x1) #crosslink capability, binary
sl = shortdata >> 21 & 0x07 #operating sensitivity of onboard TCAS system. 0 means no TCAS sensitivity reported, 1-7 give TCAS sensitivity
ri = shortdata >> 15 & 0x0F #speed coding: 0 = no onboard TCAS, 1 = NA, 2 = TCAS w/inhib res, 3 = TCAS w/vert only, 4 = TCAS w/vert+horiz, 5-7 = NA, 8 = no max A/S avail,
#9 = A/S <= 75kt, 10 = A/S (75-150]kt, 11 = (150-300]kt, 12 = (300-600]kt, 13 = (600-1200]kt, 14 = >1200kt, 15 = NA
altitude = decode_alt(shortdata & 0x1FFF, True) #bit 13 is set for type 0
return [vs, cc, sl, ri, altitude]
def parse4(self, shortdata, parity, ecc):
# shortdata = long(shortdata, 16)
fs = shortdata >> 24 & 0x07 #flight status: 0 is airborne normal, 1 is ground normal, 2 is airborne alert, 3 is ground alert, 4 is alert SPI, 5 is normal SPI
dr = shortdata >> 19 & 0x1F #downlink request: 0 means no req, bit 0 is Comm-B msg rdy bit, bit 1 is TCAS info msg rdy, bit 2 is Comm-B bcast #1 msg rdy, bit2+bit0 is Comm-B bcast #2 msg rdy,
#bit2+bit1 is TCAS info and Comm-B bcast #1 msg rdy, bit2+bit1+bit0 is TCAS info and Comm-B bcast #2 msg rdy, 8-15 N/A, 16-31 req to send N-15 segments
um = shortdata >> 13 & 0x3F #transponder status readouts, no decoding information available
altitude = decode_alt(shortdata & 0x1FFF, True)
return [fs, dr, um, altitude]
def parse5(self, shortdata, parity, ecc):
# shortdata = long(shortdata, 16)
fs = shortdata >> 24 & 0x07 #flight status: 0 is airborne normal, 1 is ground normal, 2 is airborne alert, 3 is ground alert, 4 is alert SPI, 5 is normal SPI
dr = shortdata >> 19 & 0x1F #downlink request: 0 means no req, bit 0 is Comm-B msg rdy bit, bit 1 is TCAS info msg rdy, bit 2 is Comm-B bcast #1 msg rdy, bit2+bit0 is Comm-B bcast #2 msg rdy,
#bit2+bit1 is TCAS info and Comm-B bcast #1 msg rdy, bit2+bit1+bit0 is TCAS info and Comm-B bcast #2 msg rdy, 8-15 N/A, 16-31 req to send N-15 segments
um = shortdata >> 13 & 0x3F #transponder status readouts, no decoding information available
return [fs, dr, um]
def parse11(self, shortdata, parity, ecc):
# shortdata = long(shortdata, 16)
interrogator = ecc & 0x0F
ca = shortdata >> 13 & 0x3F #capability
icao24 = shortdata & 0xFFFFFF
return [icao24, interrogator, ca]
#def parse17(self, shortdata, longdata, parity, ecc):
# shortdata = long(shortdata, 16)
# longdata = long(longdata, 16)
# parity = long(parity, 16)
# ecc = long(ecc, 16)
# subtype = (longdata >> 51) & 0x1F;
#the subtypes are:
#0: No position information
#1: Identification (Category set D)
#2: Identification (Category set C)
#3: "" (B)
#4: "" (A)
#5: Surface position accurate to 7.5m
#6: "" to 25m
#7: "" to 185.2m (0.1nm)
#8: "" above 185.2m
#9: Airborne position to 7.5m
#10-18: Same with less accuracy
#19: Airborne velocity
#20: Airborne position w/GNSS height above earth
#21: same to 25m
#22: same above 25m
#23: Reserved
#24: Reserved for surface system status
#25-27: Reserved
#28: Extended squitter aircraft status
#29: Current/next trajectory change point
#30: Aircraft operational coordination
#31: Aircraft operational status
# if subtype == 4:
# retstr = parseBDS08(shortdata, longdata, parity, ecc)
# elif subtype >= 9 and subtype <= 18:
# retstr = parseBDS05(shortdata, longdata, parity, ecc)
# elif subtype == 19:
# subsubtype = (longdata >> 48) & 0x07
# if subsubtype == 0:
# retstr = parseBDS09_0(shortdata, longdata, parity, ecc)
# elif subsubtype == 1:
# retstr = parseBDS09_1(shortdata, longdata, parity, ecc)
# else:
# retstr = "BDS09 subtype " + str(subsubtype) + " not implemented"
# else:
# retstr = "Type 17, subtype " + str(subtype) + " not implemented"
# return retstr
def parseBDS08(self, shortdata, longdata, parity, ecc):
icao24 = shortdata & 0xFFFFFF
msg = ""
for i in range(0, 8):
msg += self.charmap( longdata >> (42-6*i) & 0x3F)
#retstr = "Type 17 subtype 04 (ident) from " + "%x" % icao24 + " with data " + msg
return msg
def charmap(self, d):
if d > 0 and d < 27:
retval = chr(ord("A")+d-1)
elif d == 32:
retval = " "
elif d > 47 and d < 58:
retval = chr(ord("0")+d-48)
else:
retval = " "
return retval
def parseBDS05(self, shortdata, longdata, parity, ecc):
icao24 = shortdata & 0xFFFFFF
encoded_lon = longdata & 0x1FFFF
encoded_lat = (longdata >> 17) & 0x1FFFF
cpr_format = (longdata >> 34) & 1
enc_alt = (longdata >> 36) & 0x0FFF
altitude = decode_alt(enc_alt, False)
[decoded_lat, decoded_lon, rnge, bearing] = cpr_decoder.decode(icao24, encoded_lat, encoded_lon, cpr_format, 0)
return [altitude, decoded_lat, decoded_lon, rnge, bearing]
#welp turns out it looks like there's only 17 bits in the BDS0,6 ground packet after all. fuck.
def parseBDS06(self, shortdata, longdata, parity, ecc):
icao24 = shortdata & 0xFFFFFF
encoded_lon = longdata & 0x1FFFF
encoded_lat = (longdata >> 17) & 0x1FFFF
cpr_format = (longdata >> 34) & 1
# enc_alt = (longdata >> 36) & 0x0FFF
altitude = 0
[decoded_lat, decoded_lon, rnge, bearing] = cpr_decoder.decode(icao24, encoded_lat, encoded_lon, cpr_format, 1)
return [altitude, decoded_lat, decoded_lon, rnge, bearing]
def parseBDS09_0(self, shortdata, longdata, parity, ecc):
icao24 = shortdata & 0xFFFFFF
vert_spd = ((longdata >> 6) & 0x1FF) * 32
ud = bool((longdata >> 15) & 1)
if ud:
vert_spd = 0 - vert_spd
turn_rate = (longdata >> 16) & 0x3F
turn_rate = turn_rate * 15/62
rl = bool((longdata >> 22) & 1)
if rl:
turn_rate = 0 - turn_rate
ns_vel = (longdata >> 23) & 0x7FF - 1
ns = bool((longdata >> 34) & 1)
ew_vel = (longdata >> 35) & 0x7FF - 1
ew = bool((longdata >> 46) & 1)
subtype = (longdata >> 48) & 0x07
velocity = math.hypot(ns_vel, ew_vel)
if ew:
ew_vel = 0 - ew_vel
if ns:
ns_vel = 0 - ns_vel
heading = math.atan2(ew_vel, ns_vel) * (180.0 / math.pi)
if heading < 0:
heading += 360
#retstr = "Type 17 subtype 09-0 (track report) from " + "%x" % icao24 + " with velocity " + "%.0f" % velocity + "kt heading " + "%.0f" % heading + " VS " + "%.0f" % vert_spd
return [velocity, heading, vert_spd]
def parseBDS09_1(self, shortdata, longdata, parity, ecc):
icao24 = shortdata & 0xFFFFFF
alt_geo_diff = longdata & 0x7F - 1
above_below = bool((longdata >> 7) & 1)
if above_below:
alt_geo_diff = 0 - alt_geo_diff;
vert_spd = float((longdata >> 10) & 0x1FF - 1)
ud = bool((longdata >> 19) & 1)
if ud:
vert_spd = 0 - vert_spd
vert_src = bool((longdata >> 20) & 1)
ns_vel = float((longdata >> 21) & 0x3FF - 1)
ns = bool((longdata >> 31) & 1)
ew_vel = float((longdata >> 32) & 0x3FF - 1)
ew = bool((longdata >> 42) & 1)
subtype = (longdata >> 48) & 0x07
if subtype == 0x02:
ns_vel *= 4
ew_vel *= 4
vert_spd *= 64
alt_geo_diff *= 25
velocity = math.hypot(ns_vel, ew_vel)
if ew:
ew_vel = 0 - ew_vel
if ns_vel == 0:
heading = 0
else:
heading = math.atan(float(ew_vel) / float(ns_vel)) * (180.0 / math.pi)
if ns:
heading = 180 - heading
if heading < 0:
heading += 360
#retstr = "Type 17 subtype 09-1 (track report) from " + "%x" % icao24 + " with velocity " + "%.0f" % velocity + "kt heading " + "%.0f" % heading + " VS " + "%.0f" % vert_spd
return [velocity, heading, vert_spd]