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dump1090/mode_s.c

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// Part of dump1090, a Mode S message decoder for RTLSDR devices.
//
// mode_s.c: Mode S message decoding.
//
// Copyright (c) 2014-2016 Oliver Jowett <oliver@mutability.co.uk>
//
// This file is free software: you may copy, redistribute and/or modify it
// under the terms of the GNU General Public License as published by the
// Free Software Foundation, either version 2 of the License, or (at your
// option) any later version.
//
// This file 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/>.
// This file incorporates work covered by the following copyright and
// permission notice:
//
// Copyright (C) 2012 by Salvatore Sanfilippo <antirez@gmail.com>
//
// All rights reserved.
//
// Redistribution and use in source and binary forms, with or without
// modification, are permitted provided that the following conditions are
// met:
//
// * Redistributions of source code must retain the above copyright
// notice, this list of conditions and the following disclaimer.
//
// * Redistributions in binary form must reproduce the above copyright
// notice, this list of conditions and the following disclaimer in the
// documentation and/or other materials provided with the distribution.
//
// THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
// "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
// LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS FOR
// A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE COPYRIGHT
// HOLDER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, INCIDENTAL,
// SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, BUT NOT
// LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS OF USE,
// DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED AND ON ANY
// THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT LIABILITY, OR TORT
// (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN ANY WAY OUT OF THE USE
// OF THIS SOFTWARE, EVEN IF ADVISED OF THE POSSIBILITY OF SUCH DAMAGE.
#include "dump1090.h"
/* for PRIX64 */
#include <inttypes.h>
//
// ===================== Mode S detection and decoding ===================
//
//
//
/* A timestamp that indicates the data is synthetic, created from a
* multilateration result
*/
#define MAGIC_MLAT_TIMESTAMP 0xFF004D4C4154ULL
//=========================================================================
//
// Given the Downlink Format (DF) of the message, return the message length in bits.
//
// All known DF's 16 or greater are long. All known DF's 15 or less are short.
// There are lots of unused codes in both category, so we can assume ICAO will stick to
// these rules, meaning that the most significant bit of the DF indicates the length.
//
int modesMessageLenByType(int type) {
return (type & 0x10) ? MODES_LONG_MSG_BITS : MODES_SHORT_MSG_BITS ;
}
//
//=========================================================================
//
// In the squawk (identity) field bits are interleaved as follows in
// (message bit 20 to bit 32):
//
// C1-A1-C2-A2-C4-A4-ZERO-B1-D1-B2-D2-B4-D4
//
// So every group of three bits A, B, C, D represent an integer from 0 to 7.
//
// The actual meaning is just 4 octal numbers, but we convert it into a hex
// number tha happens to represent the four octal numbers.
//
// For more info: http://en.wikipedia.org/wiki/Gillham_code
//
static int decodeID13Field(int ID13Field) {
int hexGillham = 0;
if (ID13Field & 0x1000) {hexGillham |= 0x0010;} // Bit 12 = C1
if (ID13Field & 0x0800) {hexGillham |= 0x1000;} // Bit 11 = A1
if (ID13Field & 0x0400) {hexGillham |= 0x0020;} // Bit 10 = C2
if (ID13Field & 0x0200) {hexGillham |= 0x2000;} // Bit 9 = A2
if (ID13Field & 0x0100) {hexGillham |= 0x0040;} // Bit 8 = C4
if (ID13Field & 0x0080) {hexGillham |= 0x4000;} // Bit 7 = A4
//if (ID13Field & 0x0040) {hexGillham |= 0x0800;} // Bit 6 = X or M
if (ID13Field & 0x0020) {hexGillham |= 0x0100;} // Bit 5 = B1
if (ID13Field & 0x0010) {hexGillham |= 0x0001;} // Bit 4 = D1 or Q
if (ID13Field & 0x0008) {hexGillham |= 0x0200;} // Bit 3 = B2
if (ID13Field & 0x0004) {hexGillham |= 0x0002;} // Bit 2 = D2
if (ID13Field & 0x0002) {hexGillham |= 0x0400;} // Bit 1 = B4
if (ID13Field & 0x0001) {hexGillham |= 0x0004;} // Bit 0 = D4
return (hexGillham);
}
//
//=========================================================================
//
// Decode the 13 bit AC altitude field (in DF 20 and others).
// Returns the altitude, and set 'unit' to either UNIT_METERS or UNIT_FEET.
//
static int decodeAC13Field(int AC13Field, altitude_unit_t *unit) {
int m_bit = AC13Field & 0x0040; // set = meters, clear = feet
int q_bit = AC13Field & 0x0010; // set = 25 ft encoding, clear = Gillham Mode C encoding
if (!m_bit) {
*unit = UNIT_FEET;
if (q_bit) {
// N is the 11 bit integer resulting from the removal of bit Q and M
int n = ((AC13Field & 0x1F80) >> 2) |
((AC13Field & 0x0020) >> 1) |
(AC13Field & 0x000F);
// The final altitude is resulting number multiplied by 25, minus 1000.
return ((n * 25) - 1000);
} else {
// N is an 11 bit Gillham coded altitude
int n = ModeAToModeC(decodeID13Field(AC13Field));
if (n < -12) {
return INVALID_ALTITUDE;
}
return (100 * n);
}
} else {
*unit = UNIT_METERS;
// TODO: Implement altitude when meter unit is selected
return INVALID_ALTITUDE;
}
}
//
//=========================================================================
//
// Decode the 12 bit AC altitude field (in DF 17 and others).
//
static int decodeAC12Field(int AC12Field, altitude_unit_t *unit) {
int q_bit = AC12Field & 0x10; // Bit 48 = Q
*unit = UNIT_FEET;
if (q_bit) {
/// N is the 11 bit integer resulting from the removal of bit Q at bit 4
int n = ((AC12Field & 0x0FE0) >> 1) |
(AC12Field & 0x000F);
// The final altitude is the resulting number multiplied by 25, minus 1000.
return ((n * 25) - 1000);
} else {
// Make N a 13 bit Gillham coded altitude by inserting M=0 at bit 6
int n = ((AC12Field & 0x0FC0) << 1) |
(AC12Field & 0x003F);
n = ModeAToModeC(decodeID13Field(n));
if (n < -12) {
return INVALID_ALTITUDE;
}
return (100 * n);
}
}
//
//=========================================================================
//
// Decode the 7 bit ground movement field PWL exponential style scale
//
static int decodeMovementField(int movement) {
int gspeed;
// Note : movement codes 0,125,126,127 are all invalid, but they are
// trapped for before this function is called.
if (movement > 123) gspeed = 199; // > 175kt
else if (movement > 108) gspeed = ((movement - 108) * 5) + 100;
else if (movement > 93) gspeed = ((movement - 93) * 2) + 70;
else if (movement > 38) gspeed = ((movement - 38) ) + 15;
else if (movement > 12) gspeed = ((movement - 11) >> 1) + 2;
else if (movement > 8) gspeed = ((movement - 6) >> 2) + 1;
else gspeed = 0;
return (gspeed);
}
// Correct a decoded native-endian Address Announced field
// (from bits 8-31) if it is affected by the given error
// syndrome. Updates *addr and returns >0 if changed, 0 if
// it was unaffected.
static int correct_aa_field(uint32_t *addr, struct errorinfo *ei)
{
int i;
int addr_errors = 0;
if (!ei)
return 0;
for (i = 0; i < ei->errors; ++i) {
if (ei->bit[i] >= 8 && ei->bit[i] <= 31) {
*addr ^= 1 << (31 - ei->bit[i]);
++addr_errors;
}
}
return addr_errors;
}
// Score how plausible this ModeS message looks.
// The more positive, the more reliable the message is
// 1000: DF 0/4/5/16/24 with a CRC-derived address matching a known aircraft
// 1800: DF17/18 with good CRC and an address matching a known aircraft
// 1400: DF17/18 with good CRC and an address not matching a known aircraft
// 900: DF17/18 with 1-bit error and an address matching a known aircraft
// 700: DF17/18 with 1-bit error and an address not matching a known aircraft
// 450: DF17/18 with 2-bit error and an address matching a known aircraft
// 350: DF17/18 with 2-bit error and an address not matching a known aircraft
// 1600: DF11 with IID==0, good CRC and an address matching a known aircraft
// 800: DF11 with IID==0, 1-bit error and an address matching a known aircraft
// 750: DF11 with IID==0, good CRC and an address not matching a known aircraft
// 375: DF11 with IID==0, 1-bit error and an address not matching a known aircraft
// 1000: DF11 with IID!=0, good CRC and an address matching a known aircraft
// 500: DF11 with IID!=0, 1-bit error and an address matching a known aircraft
// 1000: DF20/21 with a CRC-derived address matching a known aircraft
// 500: DF20/21 with a CRC-derived address matching a known aircraft (bottom 16 bits only - overlay control in use)
// -1: message might be valid, but we couldn't validate the CRC against a known ICAO
// -2: bad message or unrepairable CRC error
int scoreModesMessage(unsigned char *msg, int validbits)
{
int msgtype, msgbits, crc, iid;
uint32_t addr;
struct errorinfo *ei;
static unsigned char all_zeros[14] = { 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0 };
if (validbits < 56)
return -2;
msgtype = msg[0] >> 3; // Downlink Format
msgbits = modesMessageLenByType(msgtype);
if (validbits < msgbits)
return -2;
if (!memcmp(all_zeros, msg, msgbits/8))
return -2;
crc = modesChecksum(msg, msgbits);
switch (msgtype) {
case 0: // short air-air surveillance
case 4: // surveillance, altitude reply
case 5: // surveillance, altitude reply
case 16: // long air-air surveillance
case 24: // Comm-D (ELM)
case 25: // Comm-D (ELM)
case 26: // Comm-D (ELM)
case 27: // Comm-D (ELM)
case 28: // Comm-D (ELM)
case 29: // Comm-D (ELM)
case 30: // Comm-D (ELM)
case 31: // Comm-D (ELM)
return icaoFilterTest(crc) ? 1000 : -1;
case 11: // All-call reply
iid = crc & 0x7f;
crc = crc & 0xffff80;
addr = (msg[1] << 16) | (msg[2] << 8) | (msg[3]);
ei = modesChecksumDiagnose(crc, msgbits);
if (!ei)
return -2; // can't correct errors
// see crc.c comments: we do not attempt to fix
// more than single-bit errors, as two-bit
// errors are ambiguous in DF11.
if (ei->errors > 1)
return -2; // can't correct errors
// fix any errors in the address field
correct_aa_field(&addr, ei);
// validate address
if (iid == 0) {
if (icaoFilterTest(addr))
return 1600 / (ei->errors + 1);
else
return 750 / (ei->errors + 1);
} else {
if (icaoFilterTest(addr))
return 1000 / (ei->errors + 1);
else
return -1;
}
case 17: // Extended squitter
case 18: // Extended squitter/non-transponder
ei = modesChecksumDiagnose(crc, msgbits);
if (!ei)
return -2; // can't correct errors
// fix any errors in the address field
addr = (msg[1] << 16) | (msg[2] << 8) | (msg[3]);
correct_aa_field(&addr, ei);
if (icaoFilterTest(addr))
return 1800 / (ei->errors+1);
else
return 1400 / (ei->errors+1);
case 20: // Comm-B, altitude reply
case 21: // Comm-B, identity reply
if (icaoFilterTest(crc))
return 1000; // Address/Parity
#if 0
// This doesn't seem useful, as we mistake a lot of CRC errors
// for overlay control
if (icaoFilterTestFuzzy(crc))
return 500; // Data/Parity
#endif
return -2;
default:
// unknown message type
return -2;
}
}
//
//=========================================================================
//
// Decode a raw Mode S message demodulated as a stream of bytes by detectModeS(),
// and split it into fields populating a modesMessage structure.
//
static void decodeExtendedSquitter(struct modesMessage *mm);
static void decodeCommB(struct modesMessage *mm);
static char *ais_charset = "@ABCDEFGHIJKLMNOPQRSTUVWXYZ[\\]^_ !\"#$%&'()*+,-./0123456789:;<=>?";
// return 0 if all OK
// -1: message might be valid, but we couldn't validate the CRC against a known ICAO
// -2: bad message or unrepairable CRC error
int decodeModesMessage(struct modesMessage *mm, unsigned char *msg)
{
// Work on our local copy.
memcpy(mm->msg, msg, MODES_LONG_MSG_BYTES);
if (Modes.net_verbatim) {
// Preserve the original uncorrected copy for later forwarding
memcpy(mm->verbatim, msg, MODES_LONG_MSG_BYTES);
}
msg = mm->msg;
// Get the message type ASAP as other operations depend on this
mm->msgtype = msg[0] >> 3; // Downlink Format
mm->msgbits = modesMessageLenByType(mm->msgtype);
mm->crc = modesChecksum(msg, mm->msgbits);
mm->correctedbits = 0;
mm->addr = 0;
// Do checksum work and set fields that depend on the CRC
switch (mm->msgtype) {
case 0: // short air-air surveillance
case 4: // surveillance, altitude reply
case 5: // surveillance, altitude reply
case 16: // long air-air surveillance
case 24: // Comm-D (ELM)
case 25: // Comm-D (ELM)
case 26: // Comm-D (ELM)
case 27: // Comm-D (ELM)
case 28: // Comm-D (ELM)
case 29: // Comm-D (ELM)
case 30: // Comm-D (ELM)
case 31: // Comm-D (ELM)
// These message types use Address/Parity, i.e. our CRC syndrome is the sender's ICAO address.
// We can't tell if the CRC is correct or not as we don't know the correct address.
// Accept the message if it appears to be from a previously-seen aircraft
if (!icaoFilterTest(mm->crc)) {
return -1;
}
mm->source = SOURCE_MODE_S;
mm->addr = mm->crc;
break;
case 11: // All-call reply
// This message type uses Parity/Interrogator, i.e. our CRC syndrome is CL + IC from the uplink message
// which we can't see. So we don't know if the CRC is correct or not.
//
// however! CL + IC only occupy the lower 7 bits of the CRC. So if we ignore those bits when testing
// the CRC we can still try to detect/correct errors.
mm->IID = mm->crc & 0x7f;
if (mm->crc & 0xffff80) {
int addr;
struct errorinfo *ei = modesChecksumDiagnose(mm->crc & 0xffff80, mm->msgbits);
if (!ei) {
return -2; // couldn't fix it
}
// see crc.c comments: we do not attempt to fix
// more than single-bit errors, as two-bit
// errors are ambiguous in DF11.
if (ei->errors > 1)
return -2; // can't correct errors
mm->correctedbits = ei->errors;
modesChecksumFix(msg, ei);
// check whether the corrected message looks sensible
// we are conservative here: only accept corrected messages that
// match an existing aircraft.
addr = (msg[1] << 16) | (msg[2] << 8) | (msg[3]);
if (!icaoFilterTest(addr)) {
return -1;
}
}
mm->source = SOURCE_MODE_S_CHECKED;
break;
case 17: // Extended squitter
case 18: { // Extended squitter/non-transponder
struct errorinfo *ei;
int addr1, addr2;
// These message types use Parity/Interrogator, but are specified to set II=0
if (mm->crc != 0) {
ei = modesChecksumDiagnose(mm->crc, mm->msgbits);
if (!ei) {
return -2; // couldn't fix it
}
addr1 = (msg[1] << 16) | (msg[2] << 8) | (msg[3]);
mm->correctedbits = ei->errors;
modesChecksumFix(msg, ei);
addr2 = (msg[1] << 16) | (msg[2] << 8) | (msg[3]);
// we are conservative here: only accept corrected messages that
// match an existing aircraft.
if (addr1 != addr2 && !icaoFilterTest(addr2)) {
return -1;
}
}
mm->source = SOURCE_ADSB; // TIS-B decoding will override this if needed
break;
}
case 20: // Comm-B, altitude reply
case 21: // Comm-B, identity reply
// These message types either use Address/Parity (see DF0 etc)
// or Data Parity where the requested BDS is also xored into the top byte.
// So not only do we not know whether the CRC is right, we also don't know if
// the ICAO is right! Ow.
// Try an exact match
if (icaoFilterTest(mm->crc)) {
// OK.
mm->source = SOURCE_MODE_S;
mm->addr = mm->crc;
break;
}
// BDS / overlay control just doesn't work out.
return -1; // no good
default:
// All other message types, we don't know how to handle their CRCs, give up
return -2;
}
// decode the bulk of the message
// AA (Address announced)
if (mm->msgtype == 11 || mm->msgtype == 17 || mm->msgtype == 18) {
mm->AA = mm->addr = (msg[1] << 16) | (msg[2] << 8) | (msg[3]);
}
// AC (Altitude Code)
if (mm->msgtype == 0 || mm->msgtype == 4 || mm->msgtype == 16 || mm->msgtype == 20) {
mm->AC = ((msg[2] << 8) | msg[3]) & 0x1FFF;
if (mm->AC) { // Only attempt to decode if a valid (non zero) altitude is present
mm->altitude = decodeAC13Field(mm->AC, &mm->altitude_unit);
if (mm->altitude != INVALID_ALTITUDE)
mm->altitude_valid = 1;
mm->altitude_source = ALTITUDE_BARO;
}
}
// AF (DF19 Application Field) not decoded
// CA (Capability)
if (mm->msgtype == 11 || mm->msgtype == 17) {
mm->CA = (msg[0] & 0x07);
switch (mm->CA) {
case 0:
mm->airground = AG_UNCERTAIN;
break;
case 4:
mm->airground = AG_GROUND;
break;
case 5:
mm->airground = AG_AIRBORNE;
break;
case 6:
mm->airground = AG_UNCERTAIN;
break;
case 7:
mm->airground = AG_UNCERTAIN;
break;
}
}
// CC (Cross-link capability)
if (mm->msgtype == 0) {
mm->CC = (msg[0] & 0x02) ? 1 : 0;
}
// CF (Control field)
if (mm->msgtype == 18) {
mm->CF = msg[0] & 7;
}
// DR (Downlink Request)
if (mm->msgtype == 4 || mm->msgtype == 5 || mm->msgtype == 20 || mm->msgtype == 21) {
mm->DR = (msg[1] >> 3) & 0x1F;
}
// FS (Flight Status)
if (mm->msgtype == 4 || mm->msgtype == 5 || mm->msgtype == 20 || mm->msgtype == 21) {
mm->FS = msg[0] & 7;
mm->alert_valid = 1;
mm->spi_valid = 1;
switch (mm->FS) {
case 0:
mm->airground = AG_UNCERTAIN;
break;
case 1:
mm->airground = AG_GROUND;
break;
case 2:
mm->airground = AG_UNCERTAIN;
mm->alert = 1;
break;
case 3:
mm->airground = AG_GROUND;
mm->alert = 1;
break;
case 4:
mm->airground = AG_UNCERTAIN;
mm->alert = 1;
mm->spi = 1;
break;
case 5:
mm->airground = AG_UNCERTAIN;
mm->spi = 1;
break;
default:
mm->spi_valid = 0;
mm->alert_valid = 0;
break;
}
}
// ID (Identity)
if (mm->msgtype == 5 || mm->msgtype == 21) {
// Gillham encoded Squawk
mm->ID = ((msg[2] << 8) | msg[3]) & 0x1FFF;
if (mm->ID) {
mm->squawk = decodeID13Field(mm->ID);
mm->squawk_valid = 1;
}
}
// KE (Control, ELM)
if (mm->msgtype >= 24 && mm->msgtype <= 31) {
mm->KE = (msg[0] & 0x10) ? 1 : 0;
}
// MB (messsage, Comm-B)
if (mm->msgtype == 20 || mm->msgtype == 21) {
memcpy(mm->MB, &msg[4], 7);
decodeCommB(mm);
}
// MD (message, Comm-D)
if (mm->msgtype >= 24 && mm->msgtype <= 31) {
memcpy(mm->MD, &msg[1], 10);
}
// ME (message, extended squitter)
if (mm->msgtype == 17 || mm->msgtype == 18) {
memcpy(mm->ME, &msg[4], 7);
decodeExtendedSquitter(mm);
}
// MV (message, ACAS)
if (mm->msgtype == 16) {
memcpy(mm->MV, &msg[4], 7);
}
// ND (number of D-segment, Comm-D)
if (mm->msgtype >= 24 && mm->msgtype <= 31) {
mm->ND = msg[0] & 0x0F;
}
// RI (Reply information, ACAS)
if (mm->msgtype == 0 || mm->msgtype == 16) {
mm->RI = ((msg[2] & 0x07) << 1) | ((msg[3] >> 7) & 0x01);
}
// SL (Sensitivity level, ACAS)
if (mm->msgtype == 0 || mm->msgtype == 16) {
mm->SL = (msg[1] >> 5) & 0x07;
}
// UM (Utility Message)
if (mm->msgtype == 4 || mm->msgtype == 5 || mm->msgtype == 20 || mm->msgtype == 21) {
mm->UM = ((msg[1] & 0x07) << 3) | ((msg[2] >> 5) & 0x07);
}
// VS (Vertical Status)
if (mm->msgtype == 0 || mm->msgtype == 16) {
mm->VS = (msg[0] & 0x04) ? 1 : 0;
if (mm->VS)
mm->airground = AG_GROUND;
else
mm->airground = AG_UNCERTAIN;
}
if (!mm->correctedbits && (mm->msgtype == 17 || mm->msgtype == 18 || (mm->msgtype == 11 && mm->IID == 0))) {
// No CRC errors seen, and either it was an DF17/18 extended squitter
// or a DF11 acquisition squitter with II = 0. We probably have the right address.
// We wait until here to do this as we may have needed to decode an ES to note
// the type of address in DF18 messages.
// NB this is the only place that adds addresses!
icaoFilterAdd(mm->addr);
}
// MLAT overrides all other sources
if (mm->remote && mm->timestampMsg == MAGIC_MLAT_TIMESTAMP)
mm->source = SOURCE_MLAT;
// all done
return 0;
}
// Decode BDS2,0 carried in Comm-B or ES
static void decodeBDS20(struct modesMessage *mm)
{
uint32_t chars1, chars2;
unsigned char *msg = mm->msg;
chars1 = (msg[5] << 16) | (msg[6] << 8) | (msg[7]);
chars2 = (msg[8] << 16) | (msg[9] << 8) | (msg[10]);
// A common failure mode seems to be to intermittently send
// all zeros. Catch that here.
if (chars1 == 0 && chars2 == 0)
return;
mm->callsign_valid = 1;
mm->callsign[3] = ais_charset[chars1 & 0x3F]; chars1 = chars1 >> 6;
mm->callsign[2] = ais_charset[chars1 & 0x3F]; chars1 = chars1 >> 6;
mm->callsign[1] = ais_charset[chars1 & 0x3F]; chars1 = chars1 >> 6;
mm->callsign[0] = ais_charset[chars1 & 0x3F];
mm->callsign[7] = ais_charset[chars2 & 0x3F]; chars2 = chars2 >> 6;
mm->callsign[6] = ais_charset[chars2 & 0x3F]; chars2 = chars2 >> 6;
mm->callsign[5] = ais_charset[chars2 & 0x3F]; chars2 = chars2 >> 6;
mm->callsign[4] = ais_charset[chars2 & 0x3F];
mm->callsign[8] = '\0';
}
static void decodeExtendedSquitter(struct modesMessage *mm)
{
unsigned char *msg = mm->msg;
unsigned char *me = mm->ME;
int metype = mm->metype = msg[4] >> 3; // Extended squitter message type
int mesub = mm->mesub = (metype == 29 ? ((msg[4]&6)>>1) : (msg[4] & 7)); // Extended squitter message subtype
int check_imf = 0;
// Check CF on DF18 to work out the format of the ES and whether we need to look for an IMF bit
if (mm->msgtype == 18) {
switch (mm->CF) {
case 0: // ADS-B ES/NT devices that report the ICAO 24-bit address in the AA field
break;
case 1: // Reserved for ADS-B for ES/NT devices that use other addressing techniques in the AA field
mm->addr |= MODES_NON_ICAO_ADDRESS;
break;
case 2: // Fine TIS-B message (formats are close enough to DF17 for our purposes)
mm->source = SOURCE_TISB;
check_imf = 1;
break;
case 3: // Coarse TIS-B airborne position and velocity.
// TODO: decode me.
// For now we only look at the IMF bit.
mm->source = SOURCE_TISB;
if (msg[4] & 0x80)
mm->addr |= MODES_NON_ICAO_ADDRESS;
return;
case 5: // TIS-B messages that relay ADS-B Messages using anonymous 24-bit addresses (format not explicitly defined, but it seems to follow DF17)
mm->source = SOURCE_TISB;
mm->addr |= MODES_NON_ICAO_ADDRESS;
break;
case 6: // ADS-B rebroadcast using the same type codes and message formats as defined for DF = 17 ADS-B messages
check_imf = 1;
break;
default: // All others, we don't know the format.
mm->addr |= MODES_NON_ICAO_ADDRESS; // assume non-ICAO
return;
}
}
switch (metype) {
case 1: case 2: case 3: case 4: {
// Aircraft Identification and Category
uint32_t chars1, chars2;
chars1 = (msg[5] << 16) | (msg[6] << 8) | (msg[7]);
chars2 = (msg[8] << 16) | (msg[9] << 8) | (msg[10]);
// A common failure mode seems to be to intermittently send
// all zeros. Catch that here.
if (chars1 != 0 || chars2 != 0) {
mm->callsign_valid = 1;
mm->callsign[3] = ais_charset[chars1 & 0x3F]; chars1 = chars1 >> 6;
mm->callsign[2] = ais_charset[chars1 & 0x3F]; chars1 = chars1 >> 6;
mm->callsign[1] = ais_charset[chars1 & 0x3F]; chars1 = chars1 >> 6;
mm->callsign[0] = ais_charset[chars1 & 0x3F];
mm->callsign[7] = ais_charset[chars2 & 0x3F]; chars2 = chars2 >> 6;
mm->callsign[6] = ais_charset[chars2 & 0x3F]; chars2 = chars2 >> 6;
mm->callsign[5] = ais_charset[chars2 & 0x3F]; chars2 = chars2 >> 6;
mm->callsign[4] = ais_charset[chars2 & 0x3F];
mm->callsign[8] = '\0';
}
mm->category = ((0x0E - metype) << 4) | mesub;
mm->category_valid = 1;
break;
}
case 19: { // Airborne Velocity Message
if (check_imf && (msg[5] & 0x80))
mm->addr |= MODES_NON_ICAO_ADDRESS;
if ( (mesub >= 1) && (mesub <= 4) ) {
int vert_rate = ((msg[8] & 0x07) << 6) | (msg[9] >> 2);
if (vert_rate) {
--vert_rate;
if (msg[8] & 0x08)
{vert_rate = 0 - vert_rate;}
mm->vert_rate = vert_rate * 64;
mm->vert_rate_valid = 1;
}
mm->vert_rate_source = (msg[8] & 0x10 ? ALTITUDE_GNSS : ALTITUDE_BARO);
}
if ((mesub == 1) || (mesub == 2)) {
unsigned ew_raw = ((msg[5] & 0x03) << 8) | msg[6];
unsigned ns_raw = ((msg[7] & 0x7F) << 3) | (msg[8] >> 5);
if (ew_raw && ns_raw) {
int ew_vel = (ew_raw - 1) * ((msg[5] & 0x04) ? -1 : 1) * ((mesub == 2) ? 4 : 1);
int ns_vel = (ns_raw - 1) * ((msg[7] & 0x80) ? -1 : 1) * ((mesub == 2) ? 4 : 1);
// Compute velocity and angle from the two speed components
mm->speed = (unsigned) sqrt((ns_vel * ns_vel) + (ew_vel * ew_vel) + 0.5);
mm->speed_valid = 1;
if (mm->speed) {
int heading = (int) (atan2(ew_vel, ns_vel) * 180.0 / M_PI + 0.5);
// We don't want negative values but a 0-360 scale
if (heading < 0)
heading += 360;
mm->heading = (unsigned) heading;
mm->heading_source = HEADING_TRUE;
mm->heading_valid = 1;
}
mm->speed_source = SPEED_GROUNDSPEED;
}
} else if (mesub == 3 || mesub == 4) {
unsigned airspeed = ((msg[7] & 0x7f) << 3) | (msg[8] >> 5);
if (airspeed) {
--airspeed;
if (mesub == 4) { // If (supersonic) unit is 4 kts
airspeed *= 4;
}
mm->speed = airspeed;
mm->speed_source = (msg[7] & 0x80) ? SPEED_TAS : SPEED_IAS;
mm->speed_valid = 1;
}
if (msg[5] & 0x04) {
mm->heading = ((((msg[5] & 0x03) << 8) | msg[6]) * 45) >> 7;
mm->heading_source = HEADING_MAGNETIC;
mm->heading_valid = 1;
}
}
if (msg[10] & 0x7f) {
mm->gnss_delta_valid = 1;
mm->gnss_delta = ((msg[10] & 0x80) ? -25 : 25) * ((msg[10] & 0x7f) - 1);
}
break;
}
case 5: case 6: case 7: case 8: {
// Ground position
int movement;
if (check_imf && (msg[6] & 0x08))
mm->addr |= MODES_NON_ICAO_ADDRESS;
mm->airground = AG_GROUND; // definitely.
mm->cpr_lat = ((msg[6] & 3) << 15) | (msg[7] << 7) | (msg[8] >> 1);
mm->cpr_lon = ((msg[8] & 1) << 16) | (msg[9] << 8) | (msg[10]);
if (mm->msg[6] & 0x04)
mm->cpr_odd = 1;
mm->cpr_nucp = (14 - metype);
mm->cpr_valid = 1;
movement = ((msg[4] << 4) | (msg[5] >> 4)) & 0x007F;
if ((movement) && (movement < 125)) {
mm->speed_valid = 1;
mm->speed = decodeMovementField(movement);
mm->speed_source = SPEED_GROUNDSPEED;
}
if (msg[5] & 0x08) {
mm->heading_valid = 1;
mm->heading_source = HEADING_TRUE;
mm->heading = ((((msg[5] << 4) | (msg[6] >> 4)) & 0x007F) * 45) >> 4;
}
break;
}
case 0: // Airborne position, baro altitude only
case 9: case 10: case 11: case 12: case 13: case 14: case 15: case 16: case 17: case 18: // Airborne position, baro
case 20: case 21: case 22: { // Airborne position, GNSS altitude (HAE or MSL)
int AC12Field = ((msg[5] << 4) | (msg[6] >> 4)) & 0x0FFF;
if (check_imf && (msg[4] & 0x01))
mm->addr |= MODES_NON_ICAO_ADDRESS;
if (metype == 0) {
mm->cpr_nucp = 0;
} else {
// Catch some common failure modes and don't mark them as valid
// (so they won't be used for positioning)
mm->cpr_lat = ((msg[6] & 3) << 15) | (msg[7] << 7) | (msg[8] >> 1);
mm->cpr_lon = ((msg[8] & 1) << 16) | (msg[9] << 8) | (msg[10]);
if (AC12Field == 0 && mm->cpr_lon == 0 && (mm->cpr_lat & 0x0fff) == 0 && mm->metype == 15) {
// Seen from at least:
// 400F3F (Eurocopter ECC155 B1) - Bristow Helicopters
// 4008F3 (BAE ATP) - Atlantic Airlines
// 400648 (BAE ATP) - Atlantic Airlines
// altitude == 0, longitude == 0, type == 15 and zeros in latitude LSB.
// Can alternate with valid reports having type == 14
Modes.stats_current.cpr_filtered++;
} else {
// Otherwise, assume it's valid.
mm->cpr_valid = 1;
if (mm->msg[6] & 0x04)
mm->cpr_odd = 1;
if (metype == 18 || metype == 22)
mm->cpr_nucp = 0;
else if (metype < 18)
mm->cpr_nucp = (18 - metype);
else
mm->cpr_nucp = (29 - metype);
}
}
if (AC12Field) {// Only attempt to decode if a valid (non zero) altitude is present
mm->altitude = decodeAC12Field(AC12Field, &mm->altitude_unit);
if (mm->altitude != INVALID_ALTITUDE) {
mm->altitude_valid = 1;
}
mm->altitude_source = (metype == 20 || metype == 21 || metype == 22) ? ALTITUDE_GNSS : ALTITUDE_BARO;
}
break;
}
case 23: { // Test message
if (mesub == 7) { // (see 1090-WP-15-20)
int ID13Field = (((msg[5] << 8) | msg[6]) & 0xFFF1)>>3;
if (ID13Field) {
mm->squawk_valid = 1;
mm->squawk = decodeID13Field(ID13Field);
}
}
break;
}
case 24: // Reserved for Surface System Status
break;
case 28: { // Extended Squitter Aircraft Status
if (mesub == 1) { // Emergency status squawk field
int ID13Field = (((msg[5] << 8) | msg[6]) & 0x1FFF);
if (ID13Field) {
mm->squawk_valid = 1;
mm->squawk = decodeID13Field(ID13Field);
}
if (check_imf && (msg[10] & 0x01))
mm->addr |= MODES_NON_ICAO_ADDRESS;
}
break;
}
case 29: // Aircraft Trajectory Intent
if (mesub == 1) { // Target state and status, V2
mm->tss.valid = 1;
mm->tss.sil_type = (me[0] & 0x01) ? SIL_PER_SAMPLE : SIL_PER_HOUR;
mm->tss.altitude_type = (me[1] & 0x80) ? TSS_ALTITUDE_FMS : TSS_ALTITUDE_MCP;
unsigned alt_bits = ((me[1] << 4) | (me[2] >> 4)) & 0x7FF;
if (alt_bits == 0) {
mm->tss.altitude_valid = 0;
} else {
mm->tss.altitude_valid = 1;
mm->tss.altitude = (alt_bits - 1) * 32;
}
unsigned baro_bits = ((me[2] << 5) | (me[3] >> 3)) & 0x1FF;
if (baro_bits == 0) {
mm->tss.baro_valid = 0;
} else {
mm->tss.baro_valid = 1;
mm->tss.baro = 800.0 + (baro_bits - 1) * 0.8;
}
mm->tss.heading_valid = (me[3] & 0x04) != 0;
if (mm->tss.heading_valid) {
// two's complement -180..+180, which is conveniently
// also the same as unsigned 0..360
unsigned heading_bits = ((me[3] << 7) | (me[4] >> 1)) & 0x1ff;
mm->tss.heading = heading_bits * 180 / 256;
}
mm->tss.nac_p = ((me[4] << 3) | (me[5] >> 5)) & 0x0f;
mm->tss.nic_baro = (me[5] & 0x10) ? 1 : 0;
mm->tss.sil = (me[5] >> 2) & 0x03;
mm->tss.mode_valid = (me[5] & 0x02) ? 1 : 0;
if (mm->tss.mode_valid) {
mm->tss.mode_autopilot = (me[5] & 0x01) != 0;
mm->tss.mode_vnav = (me[6] & 0x80) != 0;
mm->tss.mode_alt_hold = (me[6] & 0x40) != 0;
mm->tss.mode_approach = (me[6] & 0x10) != 0;
}
mm->tss.acas_operational = (me[6] & 0x08) != 0;
}
break;
case 30: // Aircraft Operational Coordination
break;
case 31: // Aircraft Operational Status
if (check_imf && (msg[10] & 0x01))
mm->addr |= MODES_NON_ICAO_ADDRESS;
if (mm->mesub == 0 || mm->mesub == 1) {
mm->opstatus.valid = 1;
mm->opstatus.version = (me[5] >> 5) & 0x07;
switch (mm->opstatus.version) {
case 0:
break;
case 1:
if ((me[3] & 0xC0) == 0) {
mm->opstatus.om_acas_ra = (me[3] & 0x20) != 0;
mm->opstatus.om_ident = (me[3] & 0x10) != 0;
mm->opstatus.om_atc = (me[3] & 0x08) != 0;
}
if (mm->mesub == 0 && (me[1] & 0xCC) == 0) {
// airborne
mm->opstatus.cc_acas = (me[1] & 0x20) == 0;
mm->opstatus.cc_cdti = (me[1] & 0x10) != 0;
mm->opstatus.cc_arv = (me[1] & 0x02) != 0;
mm->opstatus.cc_ts = (me[1] & 0x01) != 0;
mm->opstatus.cc_tc = (me[2] >> 6) & 0x03;
} else if (mm->mesub == 1 && (me[1] & 0xCC) == 0) {
// surface
mm->opstatus.cc_poa = (me[1] & 0x20) != 0;
mm->opstatus.cc_cdti = (me[1] & 0x10) != 0;
mm->opstatus.cc_b2_low = (me[1] & 0x02) != 0;
mm->opstatus.cc_lw_valid = 1;
mm->opstatus.cc_lw = me[2] & 0x0F;
}
mm->opstatus.nic_supp_a = (me[5] & 0x10) ? 1 : 0;
mm->opstatus.nac_p = me[5] & 0x0F;
mm->opstatus.sil = (me[6] >> 4) & 0x03;
if (mm->mesub == 0) {
mm->opstatus.nic_baro = (me[6] & 0x08) ? 1 : 0;
} else {
mm->opstatus.track_angle = (me[6] & 0x08) ? ANGLE_TRACK : ANGLE_HEADING;
}
mm->opstatus.hrd = (me[6] & 0x04) ? HEADING_MAGNETIC : HEADING_TRUE;
break;
case 2:
default:
if ((me[3] & 0xC0) == 0) {
mm->opstatus.om_acas_ra = (me[3] & 0x20) != 0;
mm->opstatus.om_ident = (me[3] & 0x10) != 0;
mm->opstatus.om_atc = (me[3] & 0x08) != 0;
mm->opstatus.om_saf = (me[3] & 0x04) != 0;
mm->opstatus.om_sda = (me[3] & 0x03);
}
if (mm->mesub == 0 && (me[1] & 0xCC) == 0) {
// airborne
mm->opstatus.cc_acas = (me[1] & 0x20) != 0;
mm->opstatus.cc_1090_in = (me[1] & 0x10) != 0;
mm->opstatus.cc_arv = (me[1] & 0x02) != 0;
mm->opstatus.cc_ts = (me[1] & 0x01) != 0;
mm->opstatus.cc_tc = (me[2] >> 6) & 0x03;
mm->opstatus.cc_uat_in = (me[2] & 0x20) != 0;
} else if (mm->mesub == 1 && (me[1] & 0xCC) == 0) {
// surface
mm->opstatus.cc_poa = (me[1] & 0x20) != 0;
mm->opstatus.cc_1090_in = (me[1] & 0x10) != 0;
mm->opstatus.cc_b2_low = (me[1] & 0x02) != 0;
mm->opstatus.cc_uat_in = (me[1] & 0x01) != 0;
mm->opstatus.cc_nac_v = (me[2] >> 5) & 0x07;
mm->opstatus.cc_nic_supp_c = (me[2] & 0x10) ? 1 : 0;
mm->opstatus.cc_lw_valid = 1;
mm->opstatus.cc_lw = me[2] & 0x0F;
mm->opstatus.cc_antenna_offset = me[3];
}
mm->opstatus.nic_supp_a = (me[5] & 0x10) ? 1 : 0;
mm->opstatus.nac_p = me[5] & 0x0F;
mm->opstatus.sil = (me[6] >> 4) & 0x03;
if (mm->mesub == 0) {
mm->opstatus.gva = (me[6] >> 6) & 0x03;
mm->opstatus.nic_baro = (me[6] & 0x08) ? 1 : 0;
} else {
mm->opstatus.track_angle = (me[6] & 0x08) ? ANGLE_TRACK : ANGLE_HEADING;
}
mm->opstatus.hrd = (me[6] & 0x04) ? HEADING_MAGNETIC : HEADING_TRUE;
mm->opstatus.sil_type = (me[6] & 0x02) ? SIL_PER_SAMPLE : SIL_PER_HOUR;
break;
}
}
break;
default:
break;
}
}
static void decodeCommB(struct modesMessage *mm)
{
unsigned char *msg = mm->msg;
// This is a bit hairy as we don't know what the requested register was
if (msg[4] == 0x20) { // BDS 2,0 Aircraft Identification
decodeBDS20(mm);
}
}
static const char *df_names[33] = {
/* 0 */ "Short Air-Air Surveillance",
/* 1 */ NULL,
/* 2 */ NULL,
/* 3 */ NULL,
/* 4 */ "Survelliance, Altitude Reply",
/* 5 */ "Survelliance, Identity Reply",
/* 6 */ NULL,
/* 7 */ NULL,
/* 8 */ NULL,
/* 9 */ NULL,
/* 10 */ NULL,
/* 11 */ "All Call Reply",
/* 12 */ NULL,
/* 13 */ NULL,
/* 14 */ NULL,
/* 15 */ NULL,
/* 16 */ "Long Air-Air ACAS",
/* 17 */ "Extended Squitter",
/* 18 */ "Extended Squitter (Non-Transponder)",
/* 19 */ "Extended Squitter (Military)",
/* 20 */ "Comm-B, Altitude Reply",
/* 21 */ "Comm-B, Identity Reply",
/* 22 */ "Military Use",
/* 23 */ NULL,
/* 24 */ "Comm-D Extended Length Message",
/* 25 */ "Comm-D Extended Length Message",
/* 26 */ "Comm-D Extended Length Message",
/* 27 */ "Comm-D Extended Length Message",
/* 28 */ "Comm-D Extended Length Message",
/* 29 */ "Comm-D Extended Length Message",
/* 30 */ "Comm-D Extended Length Message",
/* 31 */ "Comm-D Extended Length Message",
/* 32 */ "Mode A/C Reply",
};
static const char *df_to_string(unsigned df) {
if (df > 32)
return "out of range";
if (!df_names[df])
return "reserved";
return df_names[df];
}
static const char *altitude_unit_to_string(altitude_unit_t unit) {
switch (unit) {
case UNIT_FEET:
return "ft";
case UNIT_METERS:
return "m";
default:
return "(unknown altitude unit)";
}
}
static const char *altitude_source_to_string(altitude_source_t source) {
switch (source) {
case ALTITUDE_BARO:
return "barometric";
case ALTITUDE_GNSS:
return "GNSS";
default:
return "(unknown altitude source)";
}
}
static const char *airground_to_string(airground_t airground) {
switch (airground) {
case AG_GROUND:
return "ground";
case AG_AIRBORNE:
return "airborne";
case AG_INVALID:
return "invalid";
case AG_UNCERTAIN:
return "airborne?";
default:
return "(unknown airground state)";
}
}
static const char *speed_source_to_string(speed_source_t speed) {
switch (speed) {
case SPEED_GROUNDSPEED:
return "groundspeed";
case SPEED_IAS:
return "IAS";
case SPEED_TAS:
return "TAS";
default:
return "(unknown speed type)";
}
}
static void print_hex_bytes(unsigned char *data, size_t len) {
size_t i;
for (i = 0; i < len; ++i) {
printf("%02X", (unsigned)data[i]);
}
}
static int esTypeHasSubtype(unsigned metype)
{
if (metype <= 18) {
return 0;
}
if (metype >= 20 && metype <= 22) {
return 0;
}
return 1;
}
static const char *esTypeName(unsigned metype, unsigned mesub)
{
switch (metype) {
case 0:
return "No position information (airborne or surface)";
case 1: case 2: case 3: case 4:
return "Aircraft identification and category";
case 5: case 6: case 7: case 8:
return "Surface position";
case 9: case 10: case 11: case 12:
case 13: case 14: case 15: case 16:
case 17: case 18:
return "Airborne position (barometric altitude)";
case 19:
switch (mesub) {
case 1:
return "Airborne velocity over ground, subsonic";
case 2:
return "Airborne velocity over ground, supersonic";
case 3:
return "Airspeed and heading, subsonic";
case 4:
return "Airspeed and heading, supersonic";
default:
return "Unknown";
}
case 20: case 21: case 22:
return "Airborne position (GNSS altitude)";
case 23:
switch (mesub) {
case 0:
return "Test message";
case 7:
return "National use / 1090-WP-15-20 Mode A squawk";
default:
return "Unknown";
}
case 24:
return "Reserved for surface system status";
case 27:
return "Reserved for trajectory change";
case 28:
switch (mesub) {
case 1:
return "Emergency/priority status";
case 2:
return "ACAS RA broadcast";
default:
return "Unknown";
}
case 29:
switch (mesub) {
case 1:
return "Target state and status";
default:
return "Unknown";
}
case 31: // Aircraft Operational Status
switch (mesub) {
case 0:
return "Aircraft operational status (airborne)";
case 1:
return "Aircraft operational status (surface)";
default:
return "Unknown";
}
default:
return "Unknown";
}
}
void displayModesMessage(struct modesMessage *mm) {
int j;
// Handle only addresses mode first.
if (Modes.onlyaddr) {
printf("%06x\n", mm->addr);
return; // Enough for --onlyaddr mode
}
// Show the raw message.
if (Modes.mlat && mm->timestampMsg) {
printf("@%012" PRIX64, mm->timestampMsg);
} else
printf("*");
for (j = 0; j < mm->msgbits/8; j++) printf("%02x", mm->msg[j]);
printf(";\n");
if (Modes.raw) {
fflush(stdout); // Provide data to the reader ASAP
return; // Enough for --raw mode
}
if (mm->msgtype < 32)
printf("CRC: %06x\n", mm->crc);
if (mm->correctedbits != 0)
printf("No. of bit errors fixed: %d\n", mm->correctedbits);
if (mm->signalLevel > 0)
printf("RSSI: %.1f dBFS\n", 10 * log10(mm->signalLevel));
if (mm->score)
printf("Score: %d\n", mm->score);
if (mm->timestampMsg) {
if (mm->timestampMsg == MAGIC_MLAT_TIMESTAMP)
printf("This is a synthetic MLAT message.\n");
else
printf("Time: %.2fus\n", mm->timestampMsg / 12.0);
}
switch (mm->msgtype) {
case 0:
printf("DF:0 addr:%06X VS:%u CC:%u SL:%u RI:%u AC:%u\n",
mm->addr, mm->VS, mm->CC, mm->SL, mm->RI, mm->AC);
break;
case 4:
printf("DF:4 addr:%06X FS:%u DR:%u UM:%u AC:%u\n",
mm->addr, mm->FS, mm->DR, mm->UM, mm->AC);
break;
case 5:
printf("DF:5 addr:%06X FS:%u DR:%u UM:%u ID:%u\n",
mm->addr, mm->FS, mm->DR, mm->UM, mm->ID);
break;
case 11:
printf("DF:11 AA:%06X IID:%u CA:%u\n",
mm->AA, mm->IID, mm->CA);
break;
case 16:
printf("DF:16 addr:%06x VS:%u SL:%u RI:%u AC:%u MV:",
mm->addr, mm->VS, mm->SL, mm->RI, mm->AC);
print_hex_bytes(mm->MV, sizeof(mm->MV));
printf("\n");
break;
case 17:
printf("DF:17 AA:%06X CA:%u ME:",
mm->AA, mm->CA);
print_hex_bytes(mm->ME, sizeof(mm->ME));
printf("\n");
break;
case 18:
printf("DF:18 AA:%06X CF:%u ME:",
mm->AA, mm->CF);
print_hex_bytes(mm->ME, sizeof(mm->ME));
printf("\n");
break;
case 20:
printf("DF:20 addr:%06X FS:%u DR:%u UM:%u AC:%u MB:",
mm->addr, mm->FS, mm->DR, mm->UM, mm->AC);
print_hex_bytes(mm->MB, sizeof(mm->MB));
printf("\n");
break;
case 21:
printf("DF:21 addr:%06x FS:%u DR:%u UM:%u ID:%u MB:",
mm->addr, mm->FS, mm->DR, mm->UM, mm->ID);
print_hex_bytes(mm->MB, sizeof(mm->MB));
printf("\n");
break;
case 24:
case 25:
case 26:
case 27:
case 28:
case 29:
case 30:
case 31:
printf("DF:24 addr:%06x KE:%u ND:%u MD:",
mm->addr, mm->KE, mm->ND);
print_hex_bytes(mm->MD, sizeof(mm->MD));
printf("\n");
break;
}
printf(" %s", df_to_string(mm->msgtype));
if (mm->msgtype == 17 || mm->msgtype == 18) {
if (esTypeHasSubtype(mm->metype)) {
printf(" %s (%u/%u)",
esTypeName(mm->metype, mm->mesub),
mm->metype,
mm->mesub);
} else {
printf(" %s (%u)",
esTypeName(mm->metype, mm->mesub),
mm->metype);
}
}
printf("\n");
if (mm->addr & MODES_NON_ICAO_ADDRESS) {
printf(" Other Address: %06X\n", mm->addr);
} else {
printf(" ICAO Address: %06X\n", mm->addr);
}
if (mm->airground != AG_INVALID) {
printf(" Air/Ground: %s\n",
airground_to_string(mm->airground));
}
if (mm->altitude_valid) {
printf(" Altitude: %d %s %s\n",
mm->altitude,
altitude_unit_to_string(mm->altitude_unit),
altitude_source_to_string(mm->altitude_source));
}
if (mm->gnss_delta_valid) {
printf(" GNSS delta: %d ft\n",
mm->gnss_delta);
}
if (mm->heading_valid) {
printf(" Heading: %u\n", mm->heading);
}
if (mm->speed_valid) {
printf(" Speed: %u kt %s\n",
mm->speed,
speed_source_to_string(mm->speed_source));
}
if (mm->vert_rate_valid) {
printf(" Vertical rate: %d ft/min %s\n",
mm->vert_rate,
altitude_source_to_string(mm->vert_rate_source));
}
if (mm->squawk_valid) {
printf(" Squawk: %04x\n",
mm->squawk);
}
if (mm->callsign_valid) {
printf(" Ident: %s\n",
mm->callsign);
}
if (mm->category_valid) {
printf(" Category: %02X\n",
mm->category);
}
if (mm->msgtype == 17 || mm->msgtype == 18) {
}
if (mm->cpr_valid) {
printf(" CPR odd flag: %s\n"
" CPR NUCp/NIC: %u\n",
mm->cpr_odd ? "odd" : "even",
mm->cpr_nucp);
if (mm->cpr_decoded) {
printf(" CPR latitude: %.5f (%u)\n"
" CPR longitude: %.5f (%u)\n"
" CPR decoding: %s\n",
mm->decoded_lat,
mm->cpr_lat,
mm->decoded_lon,
mm->cpr_lon,
mm->cpr_relative ? "local" : "global");
} else {
printf(" CPR latitude: (%u)\n"
" CPR longitude: (%u)\n"
" CPR decoding: none\n",
mm->cpr_lat,
mm->cpr_lon);
}
}
if (mm->opstatus.valid) {
printf(" Aircraft Operational Status:\n");
printf(" Version: %d\n", mm->opstatus.version);
printf(" Capability classes: ");
if (mm->opstatus.cc_acas) printf("ACAS ");
if (mm->opstatus.cc_cdti) printf("CDTI ");
if (mm->opstatus.cc_1090_in) printf("1090IN ");
if (mm->opstatus.cc_arv) printf("ARV ");
if (mm->opstatus.cc_ts) printf("TS ");
if (mm->opstatus.cc_tc) printf("TC=%d ", mm->opstatus.cc_tc);
if (mm->opstatus.cc_uat_in) printf("UATIN ");
if (mm->opstatus.cc_poa) printf("POA ");
if (mm->opstatus.cc_b2_low) printf("B2-LOW ");
if (mm->opstatus.cc_nac_v) printf("NACv=%d ", mm->opstatus.cc_nac_v);
if (mm->opstatus.cc_nic_supp_c) printf("NIC-C=1 ");
if (mm->opstatus.cc_lw_valid) printf("L/W=%d ", mm->opstatus.cc_lw);
if (mm->opstatus.cc_antenna_offset) printf("GPS-OFFSET=%d ", mm->opstatus.cc_antenna_offset);
printf("\n");
printf(" Operational modes: ");
if (mm->opstatus.om_acas_ra) printf("ACASRA ");
if (mm->opstatus.om_ident) printf("IDENT ");
if (mm->opstatus.om_atc) printf("ATC ");
if (mm->opstatus.om_saf) printf("SAF ");
if (mm->opstatus.om_sda) printf("SDA=%d ", mm->opstatus.om_sda);
printf("\n");
if (mm->opstatus.nic_supp_a) printf(" NIC-A: %d\n", mm->opstatus.nic_supp_a);
if (mm->opstatus.nac_p) printf(" NACp: %d\n", mm->opstatus.nac_p);
if (mm->opstatus.gva) printf(" GVA: %d\n", mm->opstatus.gva);
if (mm->opstatus.sil) printf(" SIL: %d (%s)\n", mm->opstatus.sil, (mm->opstatus.sil_type == SIL_PER_HOUR ? "per hour" : "per sample"));
if (mm->opstatus.nic_baro) printf(" NICbaro: %d\n", mm->opstatus.nic_baro);
if (mm->mesub == 1)
printf(" Heading type: %s\n", (mm->opstatus.track_angle == ANGLE_HEADING ? "heading" : "track angle"));
printf(" Heading reference: %s\n", (mm->opstatus.hrd == HEADING_TRUE ? "true north" : "magnetic north"));
}
if (mm->tss.valid) {
printf(" Target State and Status:\n");
if (mm->tss.altitude_valid)
printf(" Target altitude: %s, %d ft\n", (mm->tss.altitude_type == TSS_ALTITUDE_MCP ? "MCP" : "FMS"), mm->tss.altitude);
if (mm->tss.baro_valid)
printf(" Altimeter setting: %.1f millibars\n", mm->tss.baro);
if (mm->tss.heading_valid)
printf(" Target heading: %d\n", mm->tss.heading);
if (mm->tss.mode_valid) {
printf(" Active modes: ");
if (mm->tss.mode_autopilot) printf("autopilot ");
if (mm->tss.mode_vnav) printf("VNAV ");
if (mm->tss.mode_alt_hold) printf("altitude-hold ");
if (mm->tss.mode_approach) printf("approach ");
printf("\n");
}
printf(" ACAS: %s\n", mm->tss.acas_operational ? "operational" : "NOT operational");
printf(" NACp: %d\n", mm->tss.nac_p);
printf(" NICbaro: %d\n", mm->tss.nic_baro);
printf(" SIL: %d (%s)\n", mm->tss.sil, (mm->opstatus.sil_type == SIL_PER_HOUR ? "per hour" : "per sample"));
}
printf("\n");
fflush(stdout);
}
//
//=========================================================================
//
// When a new message is available, because it was decoded from the RTL device,
// file, or received in the TCP input port, or any other way we can receive a
// decoded message, we call this function in order to use the message.
//
// Basically this function passes a raw message to the upper layers for further
// processing and visualization
//
void useModesMessage(struct modesMessage *mm) {
struct aircraft *a;
++Modes.stats_current.messages_total;
// Track aircraft state
a = trackUpdateFromMessage(mm);
// In non-interactive non-quiet mode, display messages on standard output
if (!Modes.interactive && !Modes.quiet && (!Modes.show_only || mm->addr == Modes.show_only)) {
displayModesMessage(mm);
}
// Feed output clients.
// If in --net-verbatim mode, do this for all messages.
// Otherwise, apply a sanity-check filter and only
// forward messages when we have seen two of them.
if (Modes.net) {
if (Modes.net_verbatim || mm->msgtype == 32) {
// Unconditionally send
modesQueueOutput(mm, a);
} else if (a->messages > 1) {
// If this is the second message, and we
// squelched the first message, then re-emit the
// first message now.
if (!Modes.net_verbatim && a->messages == 2) {
modesQueueOutput(&a->first_message, a);
}
modesQueueOutput(mm, a);
}
}
}
//
// ===================== Mode S detection and decoding ===================
//
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