1350 lines
42 KiB
C
1350 lines
42 KiB
C
// Part of dump1090, a Mode S message decoder for RTLSDR devices.
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//
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// track.c: aircraft state tracking
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//
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// Copyright (c) 2014-2016 Oliver Jowett <oliver@mutability.co.uk>
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//
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// This file is free software: you may copy, redistribute and/or modify it
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// under the terms of the GNU General Public License as published by the
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// Free Software Foundation, either version 2 of the License, or (at your
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// option) any later version.
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//
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// This file is distributed in the hope that it will be useful, but
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// WITHOUT ANY WARRANTY; without even the implied warranty of
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// MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
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// General Public License for more details.
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//
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// You should have received a copy of the GNU General Public License
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// along with this program. If not, see <http://www.gnu.org/licenses/>.
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// This file incorporates work covered by the following copyright and
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// permission notice:
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//
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// Copyright (C) 2012 by Salvatore Sanfilippo <antirez@gmail.com>
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//
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// All rights reserved.
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//
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// Redistribution and use in source and binary forms, with or without
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// modification, are permitted provided that the following conditions are
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// met:
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//
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// * Redistributions of source code must retain the above copyright
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// notice, this list of conditions and the following disclaimer.
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//
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// * Redistributions in binary form must reproduce the above copyright
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// notice, this list of conditions and the following disclaimer in the
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// documentation and/or other materials provided with the distribution.
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//
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// THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
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// "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
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// LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS FOR
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// A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE COPYRIGHT
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// HOLDER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, INCIDENTAL,
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// SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, BUT NOT
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// LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS OF USE,
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// DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED AND ON ANY
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// THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT LIABILITY, OR TORT
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// (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN ANY WAY OUT OF THE USE
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// OF THIS SOFTWARE, EVEN IF ADVISED OF THE POSSIBILITY OF SUCH DAMAGE.
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#include "dump1090.h"
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#include <inttypes.h>
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/* #define DEBUG_CPR_CHECKS */
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uint32_t modeAC_count[4096];
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uint32_t modeAC_lastcount[4096];
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uint32_t modeAC_match[4096];
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uint32_t modeAC_age[4096];
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//
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// Return a new aircraft structure for the linked list of tracked
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// aircraft
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//
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struct aircraft *trackCreateAircraft(struct modesMessage *mm) {
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static struct aircraft zeroAircraft;
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struct aircraft *a = (struct aircraft *) malloc(sizeof(*a));
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int i;
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// Default everything to zero/NULL
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*a = zeroAircraft;
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// Now initialise things that should not be 0/NULL to their defaults
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a->addr = mm->addr;
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a->addrtype = mm->addrtype;
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for (i = 0; i < 8; ++i)
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a->signalLevel[i] = 1e-5;
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a->signalNext = 0;
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// defaults until we see a message otherwise
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a->adsb_version = -1;
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a->adsb_hrd = HEADING_MAGNETIC;
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a->adsb_tah = HEADING_GROUND_TRACK;
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// prime FATSV defaults we only emit on change
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// start off with the "last emitted" ACAS RA being blank (just the BDS 3,0
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// or ES type code)
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a->fatsv_emitted_bds_30[0] = 0x30;
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a->fatsv_emitted_es_acas_ra[0] = 0xE2;
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a->fatsv_emitted_adsb_version = -1;
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a->fatsv_emitted_addrtype = ADDR_UNKNOWN;
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// don't immediately emit, let some data build up
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a->fatsv_last_emitted = a->fatsv_last_force_emit = messageNow();
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// Copy the first message so we can emit it later when a second message arrives.
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a->first_message = *mm;
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// initialize data validity ages
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#define F(f,s,e) do { a->f##_valid.stale_interval = (s) * 1000; a->f##_valid.expire_interval = (e) * 1000; } while (0)
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F(callsign, 60, 70); // ADS-B or Comm-B
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F(altitude_baro, 15, 70); // ADS-B or Mode S
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F(altitude_geom, 60, 70); // ADS-B only
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F(geom_delta, 60, 70); // ADS-B only
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F(gs, 60, 70); // ADS-B or Comm-B
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F(ias, 60, 70); // ADS-B (rare) or Comm-B
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F(tas, 60, 70); // ADS-B (rare) or Comm-B
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F(mach, 60, 70); // Comm-B only
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F(track, 60, 70); // ADS-B or Comm-B
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F(track_rate, 60, 70); // Comm-B only
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F(roll, 60, 70); // Comm-B only
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F(mag_heading, 60, 70); // ADS-B (rare) or Comm-B
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F(true_heading, 60, 70); // ADS-B only (rare)
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F(baro_rate, 60, 70); // ADS-B or Comm-B
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F(geom_rate, 60, 70); // ADS-B or Comm-B
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F(squawk, 15, 70); // ADS-B or Mode S
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F(airground, 15, 70); // ADS-B or Mode S
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F(nav_qnh, 60, 70); // Comm-B only
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F(nav_altitude, 60, 70); // ADS-B or Comm-B
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F(nav_heading, 60, 70); // ADS-B or Comm-B
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F(nav_modes, 60, 70); // ADS-B or Comm-B
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F(cpr_odd, 60, 70); // ADS-B only
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F(cpr_even, 60, 70); // ADS-B only
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F(position, 60, 70); // ADS-B only
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F(nic_a, 60, 70); // ADS-B only
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F(nic_c, 60, 70); // ADS-B only
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F(nic_baro, 60, 70); // ADS-B only
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F(nac_p, 60, 70); // ADS-B only
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F(nac_v, 60, 70); // ADS-B only
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F(sil, 60, 70); // ADS-B only
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F(gva, 60, 70); // ADS-B only
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F(sda, 60, 70); // ADS-B only
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#undef F
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Modes.stats_current.unique_aircraft++;
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return (a);
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}
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//
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//=========================================================================
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//
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// Return the aircraft with the specified address, or NULL if no aircraft
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// exists with this address.
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//
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struct aircraft *trackFindAircraft(uint32_t addr) {
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struct aircraft *a = Modes.aircrafts;
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while(a) {
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if (a->addr == addr) return (a);
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a = a->next;
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}
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return (NULL);
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}
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// Should we accept some new data from the given source?
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// If so, update the validity and return 1
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static int accept_data(data_validity *d, datasource_t source)
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{
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if (messageNow() < d->updated)
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return 0;
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if (source < d->source && messageNow() < d->stale)
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return 0;
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d->source = source;
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d->updated = messageNow();
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d->stale = messageNow() + (d->stale_interval ? d->stale_interval : 60000);
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d->expires = messageNow() + (d->expire_interval ? d->expire_interval : 70000);
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return 1;
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}
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// Given two datasources, produce a third datasource for data combined from them.
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static void combine_validity(data_validity *to, const data_validity *from1, const data_validity *from2) {
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if (from1->source == SOURCE_INVALID) {
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*to = *from2;
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return;
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}
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if (from2->source == SOURCE_INVALID) {
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*to = *from1;
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return;
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}
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to->source = (from1->source < from2->source) ? from1->source : from2->source; // the worse of the two input sources
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to->updated = (from1->updated > from2->updated) ? from1->updated : from2->updated; // the *later* of the two update times
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to->stale = (from1->stale < from2->stale) ? from1->stale : from2->stale; // the earlier of the two stale times
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to->expires = (from1->expires < from2->expires) ? from1->expires : from2->expires; // the earlier of the two expiry times
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}
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static int compare_validity(const data_validity *lhs, const data_validity *rhs) {
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if (messageNow() < lhs->stale && lhs->source > rhs->source)
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return 1;
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else if (messageNow() < rhs->stale && lhs->source < rhs->source)
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return -1;
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else if (lhs->updated > rhs->updated)
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return 1;
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else if (lhs->updated < rhs->updated)
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return -1;
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else
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return 0;
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}
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//
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// CPR position updating
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//
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// Distance between points on a spherical earth.
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// This has up to 0.5% error because the earth isn't actually spherical
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// (but we don't use it in situations where that matters)
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static double greatcircle(double lat0, double lon0, double lat1, double lon1)
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{
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double dlat, dlon;
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lat0 = lat0 * M_PI / 180.0;
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lon0 = lon0 * M_PI / 180.0;
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lat1 = lat1 * M_PI / 180.0;
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lon1 = lon1 * M_PI / 180.0;
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dlat = fabs(lat1 - lat0);
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dlon = fabs(lon1 - lon0);
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// use haversine for small distances for better numerical stability
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if (dlat < 0.001 && dlon < 0.001) {
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double a = sin(dlat/2) * sin(dlat/2) + cos(lat0) * cos(lat1) * sin(dlon/2) * sin(dlon/2);
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return 6371e3 * 2 * atan2(sqrt(a), sqrt(1.0 - a));
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}
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// spherical law of cosines
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return 6371e3 * acos(sin(lat0) * sin(lat1) + cos(lat0) * cos(lat1) * cos(dlon));
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}
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static void update_range_histogram(double lat, double lon)
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{
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if (Modes.stats_range_histo && (Modes.bUserFlags & MODES_USER_LATLON_VALID)) {
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double range = greatcircle(Modes.fUserLat, Modes.fUserLon, lat, lon);
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int bucket = round(range / Modes.maxRange * RANGE_BUCKET_COUNT);
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if (bucket < 0)
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bucket = 0;
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else if (bucket >= RANGE_BUCKET_COUNT)
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bucket = RANGE_BUCKET_COUNT-1;
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++Modes.stats_current.range_histogram[bucket];
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}
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}
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// return true if it's OK for the aircraft to have travelled from its last known position
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// to a new position at (lat,lon,surface) at a time of now.
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static int speed_check(struct aircraft *a, double lat, double lon, int surface)
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{
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uint64_t elapsed;
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double distance;
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double range;
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int speed;
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int inrange;
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if (!trackDataValid(&a->position_valid))
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return 1; // no reference, assume OK
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elapsed = trackDataAge(&a->position_valid);
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if (trackDataValid(&a->gs_valid))
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speed = a->gs;
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else if (trackDataValid(&a->tas_valid))
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speed = a->tas * 4 / 3;
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else if (trackDataValid(&a->ias_valid))
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speed = a->ias * 2;
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else
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speed = surface ? 100 : 600; // guess
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// Work out a reasonable speed to use:
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// current speed + 1/3
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// surface speed min 20kt, max 150kt
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// airborne speed min 200kt, no max
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speed = speed * 4 / 3;
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if (surface) {
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if (speed < 20)
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speed = 20;
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if (speed > 150)
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speed = 150;
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} else {
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if (speed < 200)
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speed = 200;
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}
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// 100m (surface) or 500m (airborne) base distance to allow for minor errors,
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// plus distance covered at the given speed for the elapsed time + 1 second.
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range = (surface ? 0.1e3 : 0.5e3) + ((elapsed + 1000.0) / 1000.0) * (speed * 1852.0 / 3600.0);
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// find actual distance
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distance = greatcircle(a->lat, a->lon, lat, lon);
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inrange = (distance <= range);
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#ifdef DEBUG_CPR_CHECKS
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if (!inrange) {
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fprintf(stderr, "Speed check failed: %06x: %.3f,%.3f -> %.3f,%.3f in %.1f seconds, max speed %d kt, range %.1fkm, actual %.1fkm\n",
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a->addr, a->lat, a->lon, lat, lon, elapsed/1000.0, speed, range/1000.0, distance/1000.0);
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}
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#endif
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return inrange;
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}
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// return 1 if left_rc is worse (less accurate) than right_rc
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static int rcIsWorse(int left_rc, int right_rc)
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{
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if (left_rc == 0 && right_rc == 0) // both unknown
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return 0;
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if (left_rc == 0)
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return 1; // left unknown < right known
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if (right_rc == 0)
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return 0; // left known > right unknown
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return (left_rc > right_rc);
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}
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static int doGlobalCPR(struct aircraft *a, struct modesMessage *mm, double *lat, double *lon, unsigned *nic, unsigned *rc)
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{
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int result;
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int fflag = mm->cpr_odd;
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int surface = (mm->cpr_type == CPR_SURFACE);
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// derive NIC, Rc from the worse of the two position
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// smaller NIC is worse
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*nic = (a->cpr_even_nic < a->cpr_odd_nic ? a->cpr_even_nic : a->cpr_odd_nic);
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*rc = (rcIsWorse(a->cpr_even_rc, a->cpr_odd_rc) ? a->cpr_even_rc : a->cpr_odd_rc);
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if (surface) {
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// surface global CPR
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// find reference location
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double reflat, reflon;
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if (trackDataValid(&a->position_valid)) { // Ok to try aircraft relative first
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reflat = a->lat;
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reflon = a->lon;
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} else if (Modes.bUserFlags & MODES_USER_LATLON_VALID) {
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reflat = Modes.fUserLat;
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reflon = Modes.fUserLon;
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} else {
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// No local reference, give up
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return (-1);
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}
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result = decodeCPRsurface(reflat, reflon,
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a->cpr_even_lat, a->cpr_even_lon,
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a->cpr_odd_lat, a->cpr_odd_lon,
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fflag,
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lat, lon);
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} else {
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// airborne global CPR
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result = decodeCPRairborne(a->cpr_even_lat, a->cpr_even_lon,
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a->cpr_odd_lat, a->cpr_odd_lon,
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fflag,
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lat, lon);
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}
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if (result < 0) {
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#ifdef DEBUG_CPR_CHECKS
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fprintf(stderr, "CPR: decode failure for %06X (%d).\n", a->addr, result);
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fprintf(stderr, " even: %d %d odd: %d %d fflag: %s\n",
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a->cpr_even_lat, a->cpr_even_lon,
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a->cpr_odd_lat, a->cpr_odd_lon,
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fflag ? "odd" : "even");
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#endif
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return result;
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}
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// check max range
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if (Modes.maxRange > 0 && (Modes.bUserFlags & MODES_USER_LATLON_VALID)) {
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double range = greatcircle(Modes.fUserLat, Modes.fUserLon, *lat, *lon);
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if (range > Modes.maxRange) {
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#ifdef DEBUG_CPR_CHECKS
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fprintf(stderr, "Global range check failed: %06x: %.3f,%.3f, max range %.1fkm, actual %.1fkm\n",
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a->addr, *lat, *lon, Modes.maxRange/1000.0, range/1000.0);
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#endif
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Modes.stats_current.cpr_global_range_checks++;
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return (-2); // we consider an out-of-range value to be bad data
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}
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}
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// for mlat results, skip the speed check
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if (mm->source == SOURCE_MLAT)
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return result;
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// check speed limit
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if (trackDataValid(&a->position_valid) && a->pos_nic >= *nic && !rcIsWorse(a->pos_rc, *rc) && !speed_check(a, *lat, *lon, surface)) {
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Modes.stats_current.cpr_global_speed_checks++;
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return -2;
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}
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return result;
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}
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static int doLocalCPR(struct aircraft *a, struct modesMessage *mm, double *lat, double *lon, unsigned *nic, unsigned *rc)
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{
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// relative CPR
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// find reference location
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double reflat, reflon;
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double range_limit = 0;
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int result;
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int fflag = mm->cpr_odd;
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int surface = (mm->cpr_type == CPR_SURFACE);
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if (fflag) {
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*nic = a->cpr_odd_nic;
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*rc = a->cpr_odd_rc;
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} else {
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*nic = a->cpr_even_nic;
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*rc = a->cpr_even_rc;
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}
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if (trackDataValid(&a->position_valid)) {
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reflat = a->lat;
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reflon = a->lon;
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if (a->pos_nic < *nic)
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*nic = a->pos_nic;
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if (rcIsWorse(a->pos_rc, *rc))
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*rc = a->pos_rc;
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range_limit = 50e3;
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} else if (!surface && (Modes.bUserFlags & MODES_USER_LATLON_VALID)) {
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reflat = Modes.fUserLat;
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reflon = Modes.fUserLon;
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// The cell size is at least 360NM, giving a nominal
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// max range of 180NM (half a cell).
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//
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// If the receiver range is more than half a cell
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// then we must limit this range further to avoid
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// ambiguity. (e.g. if we receive a position report
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// at 200NM distance, this may resolve to a position
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// at (200-360) = 160NM in the wrong direction)
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if (Modes.maxRange == 0) {
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return (-1); // Can't do receiver-centered checks at all
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} else if (Modes.maxRange <= 1852*180) {
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range_limit = Modes.maxRange;
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} else if (Modes.maxRange < 1852*360) {
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range_limit = (1852*360) - Modes.maxRange;
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} else {
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return (-1); // Can't do receiver-centered checks at all
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}
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} else {
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// No local reference, give up
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return (-1);
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}
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result = decodeCPRrelative(reflat, reflon,
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mm->cpr_lat,
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mm->cpr_lon,
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fflag, surface,
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lat, lon);
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if (result < 0) {
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return result;
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}
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// check range limit
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if (range_limit > 0) {
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double range = greatcircle(reflat, reflon, *lat, *lon);
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if (range > range_limit) {
|
|
Modes.stats_current.cpr_local_range_checks++;
|
|
return (-1);
|
|
}
|
|
}
|
|
|
|
// check speed limit
|
|
if (trackDataValid(&a->position_valid) && a->pos_nic >= *nic && !rcIsWorse(a->pos_rc, *rc) && !speed_check(a, *lat, *lon, surface)) {
|
|
#ifdef DEBUG_CPR_CHECKS
|
|
fprintf(stderr, "Speed check for %06X with local decoding failed\n", a->addr);
|
|
#endif
|
|
Modes.stats_current.cpr_local_speed_checks++;
|
|
return -1;
|
|
}
|
|
|
|
return 0;
|
|
}
|
|
|
|
static uint64_t time_between(uint64_t t1, uint64_t t2)
|
|
{
|
|
if (t1 >= t2)
|
|
return t1 - t2;
|
|
else
|
|
return t2 - t1;
|
|
}
|
|
|
|
static void updatePosition(struct aircraft *a, struct modesMessage *mm)
|
|
{
|
|
int location_result = -1;
|
|
uint64_t max_elapsed;
|
|
double new_lat = 0, new_lon = 0;
|
|
unsigned new_nic = 0;
|
|
unsigned new_rc = 0;
|
|
int surface;
|
|
|
|
surface = (mm->cpr_type == CPR_SURFACE);
|
|
|
|
if (surface) {
|
|
++Modes.stats_current.cpr_surface;
|
|
|
|
// Surface: 25 seconds if >25kt or speed unknown, 50 seconds otherwise
|
|
if (mm->gs_valid && mm->gs.selected <= 25)
|
|
max_elapsed = 50000;
|
|
else
|
|
max_elapsed = 25000;
|
|
} else {
|
|
++Modes.stats_current.cpr_airborne;
|
|
|
|
// Airborne: 10 seconds
|
|
max_elapsed = 10000;
|
|
}
|
|
|
|
// If we have enough recent data, try global CPR
|
|
if (trackDataValid(&a->cpr_odd_valid) && trackDataValid(&a->cpr_even_valid) &&
|
|
a->cpr_odd_valid.source == a->cpr_even_valid.source &&
|
|
a->cpr_odd_type == a->cpr_even_type &&
|
|
time_between(a->cpr_odd_valid.updated, a->cpr_even_valid.updated) <= max_elapsed) {
|
|
|
|
location_result = doGlobalCPR(a, mm, &new_lat, &new_lon, &new_nic, &new_rc);
|
|
|
|
if (location_result == -2) {
|
|
#ifdef DEBUG_CPR_CHECKS
|
|
fprintf(stderr, "global CPR failure (invalid) for (%06X).\n", a->addr);
|
|
#endif
|
|
// Global CPR failed because the position produced implausible results.
|
|
// This is bad data. Discard both odd and even messages and wait for a fresh pair.
|
|
// Also disable aircraft-relative positions until we have a new good position (but don't discard the
|
|
// recorded position itself)
|
|
Modes.stats_current.cpr_global_bad++;
|
|
a->cpr_odd_valid.source = a->cpr_even_valid.source = a->position_valid.source = SOURCE_INVALID;
|
|
|
|
return;
|
|
} else if (location_result == -1) {
|
|
#ifdef DEBUG_CPR_CHECKS
|
|
if (mm->source == SOURCE_MLAT) {
|
|
fprintf(stderr, "CPR skipped from MLAT (%06X).\n", a->addr);
|
|
}
|
|
#endif
|
|
// No local reference for surface position available, or the two messages crossed a zone.
|
|
// Nonfatal, try again later.
|
|
Modes.stats_current.cpr_global_skipped++;
|
|
} else {
|
|
Modes.stats_current.cpr_global_ok++;
|
|
combine_validity(&a->position_valid, &a->cpr_even_valid, &a->cpr_odd_valid);
|
|
}
|
|
}
|
|
|
|
// Otherwise try relative CPR.
|
|
if (location_result == -1) {
|
|
location_result = doLocalCPR(a, mm, &new_lat, &new_lon, &new_nic, &new_rc);
|
|
|
|
if (location_result < 0) {
|
|
Modes.stats_current.cpr_local_skipped++;
|
|
} else {
|
|
Modes.stats_current.cpr_local_ok++;
|
|
mm->cpr_relative = 1;
|
|
|
|
if (mm->cpr_odd) {
|
|
a->position_valid = a->cpr_odd_valid;
|
|
} else {
|
|
a->position_valid = a->cpr_even_valid;
|
|
}
|
|
}
|
|
}
|
|
|
|
if (location_result == 0) {
|
|
// If we sucessfully decoded, back copy the results to mm so that we can print them in list output
|
|
mm->cpr_decoded = 1;
|
|
mm->decoded_lat = new_lat;
|
|
mm->decoded_lon = new_lon;
|
|
mm->decoded_nic = new_nic;
|
|
mm->decoded_rc = new_rc;
|
|
|
|
// Update aircraft state
|
|
a->lat = new_lat;
|
|
a->lon = new_lon;
|
|
a->pos_nic = new_nic;
|
|
a->pos_rc = new_rc;
|
|
|
|
update_range_histogram(new_lat, new_lon);
|
|
}
|
|
}
|
|
|
|
static unsigned compute_nic(unsigned metype, unsigned version, unsigned nic_a, unsigned nic_b, unsigned nic_c)
|
|
{
|
|
switch (metype) {
|
|
case 5: // surface
|
|
case 9: // airborne
|
|
case 20: // airborne, GNSS altitude
|
|
return 11;
|
|
|
|
case 6: // surface
|
|
case 10: // airborne
|
|
case 21: // airborne, GNSS altitude
|
|
return 10;
|
|
|
|
case 7: // surface
|
|
if (version == 2) {
|
|
if (nic_a && !nic_c) {
|
|
return 9;
|
|
} else {
|
|
return 8;
|
|
}
|
|
} else if (version == 1) {
|
|
if (nic_a) {
|
|
return 9;
|
|
} else {
|
|
return 8;
|
|
}
|
|
} else {
|
|
return 8;
|
|
}
|
|
|
|
case 8: // surface
|
|
if (version == 2) {
|
|
if (nic_a && nic_c) {
|
|
return 7;
|
|
} else if (nic_a && !nic_c) {
|
|
return 6;
|
|
} else if (!nic_a && nic_c) {
|
|
return 6;
|
|
} else {
|
|
return 0;
|
|
}
|
|
} else {
|
|
return 0;
|
|
}
|
|
|
|
case 11: // airborne
|
|
if (version == 2) {
|
|
if (nic_a && nic_b) {
|
|
return 9;
|
|
} else {
|
|
return 8;
|
|
}
|
|
} else if (version == 1) {
|
|
if (nic_a) {
|
|
return 9;
|
|
} else {
|
|
return 8;
|
|
}
|
|
} else {
|
|
return 8;
|
|
}
|
|
|
|
case 12: // airborne
|
|
return 7;
|
|
|
|
case 13: // airborne
|
|
return 6;
|
|
|
|
case 14: // airborne
|
|
return 5;
|
|
|
|
case 15: // airborne
|
|
return 4;
|
|
|
|
case 16: // airborne
|
|
if (nic_a && nic_b) {
|
|
return 3;
|
|
} else {
|
|
return 2;
|
|
}
|
|
|
|
case 17: // airborne
|
|
return 1;
|
|
|
|
default:
|
|
return 0;
|
|
}
|
|
}
|
|
|
|
static unsigned compute_rc(unsigned metype, unsigned version, unsigned nic_a, unsigned nic_b, unsigned nic_c)
|
|
{
|
|
// ED-102 Table 2-14, Table N-4, Table N-11
|
|
|
|
switch (metype) {
|
|
case 5: // surface
|
|
case 9: // airborne
|
|
case 20: // airborne, GNSS altitude
|
|
return 8; // 7.5m
|
|
|
|
case 6: // surface
|
|
case 10: // airborne
|
|
case 21: // airborne, GNSS altitude
|
|
return 25;
|
|
|
|
case 7: // surface
|
|
if (version == 2) {
|
|
if (nic_a && !nic_c) {
|
|
return 75;
|
|
} else {
|
|
return 186; // 185.2m, 0.1NM
|
|
}
|
|
} else if (version == 1) {
|
|
if (nic_a) {
|
|
return 75;
|
|
} else {
|
|
return 186; // 185.2m, 0.1NM
|
|
}
|
|
} else {
|
|
return 186; // 185.2m, 0.1NM
|
|
}
|
|
|
|
case 8: // surface
|
|
if (version == 2) {
|
|
if (nic_a && nic_c) {
|
|
return 371; // 370.4m, 0.2NM
|
|
} else if (nic_a && !nic_c) {
|
|
return 556; // 555.6m, 0.3NM
|
|
} else if (!nic_a && nic_c) {
|
|
return 1111; // 1111m, 0.6NM
|
|
} else {
|
|
return RC_UNKNOWN;
|
|
}
|
|
} else {
|
|
return RC_UNKNOWN;
|
|
}
|
|
|
|
case 11: // airborne
|
|
if (version == 2) {
|
|
if (nic_a && nic_b) {
|
|
return 75;
|
|
} else {
|
|
return 186; // 185.2m, 0.1NM
|
|
}
|
|
} else if (version == 1) {
|
|
if (nic_a) {
|
|
return 75;
|
|
} else {
|
|
return 186; // 185.2m, 0.1NM
|
|
}
|
|
} else {
|
|
return 186; // 185.2m, 0.1NM
|
|
}
|
|
|
|
case 12: // airborne
|
|
return 371; // 370.4m, 0.2NM
|
|
|
|
case 13: // airborne
|
|
if (version == 2) {
|
|
if (!nic_a && nic_b) {
|
|
return 556; // 555.6m, 0.3NM
|
|
} else if (!nic_a && !nic_b) {
|
|
return 926; // 926m, 0.5NM
|
|
} else if (nic_a && nic_b) {
|
|
return 1112; // 1111.2m, 0.6NM
|
|
} else {
|
|
return RC_UNKNOWN; // bad combination
|
|
}
|
|
} else if (version == 1) {
|
|
if (nic_a) {
|
|
return 1112; // 1111.2m, 0.6NM
|
|
} else {
|
|
return 926; // 926m, 0.5NM
|
|
}
|
|
} else {
|
|
return 926; // 926m, 0.5NM
|
|
}
|
|
|
|
case 14: // airborne
|
|
return 1852; // 1.0NM
|
|
|
|
case 15: // airborne
|
|
return 3704; // 2NM
|
|
|
|
case 16: // airborne
|
|
if (version == 2) {
|
|
if (nic_a && nic_b) {
|
|
return 7408; // 4NM
|
|
} else {
|
|
return 14816; // 8NM
|
|
}
|
|
} else if (version == 1) {
|
|
if (nic_a) {
|
|
return 7408; // 4NM
|
|
} else {
|
|
return 14816; // 8NM
|
|
}
|
|
} else {
|
|
return 18520; // 10NM
|
|
}
|
|
|
|
case 17: // airborne
|
|
return 37040; // 20NM
|
|
|
|
default:
|
|
return RC_UNKNOWN;
|
|
}
|
|
}
|
|
|
|
// Map ADS-B v0 position message type to NACp value
|
|
// returned computed NACp, or -1 if not a suitable message type
|
|
static int compute_v0_nacp(struct modesMessage *mm)
|
|
{
|
|
if (mm->msgtype != 17 && mm->msgtype != 18) {
|
|
return -1;
|
|
}
|
|
|
|
// ED-102A Table N-7
|
|
switch (mm->metype) {
|
|
case 0: return 0;
|
|
case 5: return 11;
|
|
case 6: return 10;
|
|
case 7: return 8;
|
|
case 8: return 0;
|
|
case 9: return 11;
|
|
case 10: return 10;
|
|
case 11: return 8;
|
|
case 12: return 7;
|
|
case 13: return 6;
|
|
case 14: return 5;
|
|
case 15: return 4;
|
|
case 16: return 1;
|
|
case 17: return 1;
|
|
case 18: return 0;
|
|
case 20: return 11;
|
|
case 21: return 10;
|
|
case 22: return 0;
|
|
default: return -1;
|
|
}
|
|
}
|
|
|
|
// Map ADS-B v0 position message type to SIL value
|
|
// returned computed SIL, or -1 if not a suitable message type
|
|
static int compute_v0_sil(struct modesMessage *mm)
|
|
{
|
|
if (mm->msgtype != 17 && mm->msgtype != 18) {
|
|
return -1;
|
|
}
|
|
|
|
// ED-102A Table N-8
|
|
switch (mm->metype) {
|
|
case 0:
|
|
return 0;
|
|
|
|
case 5:
|
|
case 6:
|
|
case 7:
|
|
case 8:
|
|
case 9:
|
|
case 10:
|
|
case 11:
|
|
case 12:
|
|
case 13:
|
|
case 14:
|
|
case 15:
|
|
case 16:
|
|
case 17:
|
|
return 2;
|
|
|
|
case 18:
|
|
return 0;
|
|
|
|
case 20:
|
|
case 21:
|
|
return 2;
|
|
|
|
case 22:
|
|
return 0;
|
|
|
|
default:
|
|
return -1;
|
|
}
|
|
}
|
|
|
|
static void compute_nic_rc_from_message(struct modesMessage *mm, struct aircraft *a, unsigned *nic, unsigned *rc)
|
|
{
|
|
int nic_a = (trackDataValid(&a->nic_a_valid) && a->nic_a);
|
|
int nic_b = (mm->accuracy.nic_b_valid && mm->accuracy.nic_b);
|
|
int nic_c = (trackDataValid(&a->nic_c_valid) && a->nic_c);
|
|
|
|
*nic = compute_nic(mm->metype, a->adsb_version, nic_a, nic_b, nic_c);
|
|
*rc = compute_rc(mm->metype, a->adsb_version, nic_a, nic_b, nic_c);
|
|
}
|
|
|
|
static int altitude_to_feet(int raw, altitude_unit_t unit)
|
|
{
|
|
switch (unit) {
|
|
case UNIT_METERS:
|
|
return raw / 0.3048;
|
|
case UNIT_FEET:
|
|
return raw;
|
|
default:
|
|
return 0;
|
|
}
|
|
}
|
|
|
|
//
|
|
//=========================================================================
|
|
//
|
|
// Receive new messages and update tracked aircraft state
|
|
//
|
|
|
|
struct aircraft *trackUpdateFromMessage(struct modesMessage *mm)
|
|
{
|
|
struct aircraft *a;
|
|
|
|
if (mm->msgtype == 32) {
|
|
// Mode A/C, just count it (we ignore SPI)
|
|
modeAC_count[modeAToIndex(mm->squawk)]++;
|
|
return NULL;
|
|
}
|
|
|
|
if (mm->addr == 0) {
|
|
// junk address, don't track it
|
|
return NULL;
|
|
}
|
|
|
|
_messageNow = mm->sysTimestampMsg;
|
|
|
|
// Lookup our aircraft or create a new one
|
|
a = trackFindAircraft(mm->addr);
|
|
if (!a) { // If it's a currently unknown aircraft....
|
|
a = trackCreateAircraft(mm); // ., create a new record for it,
|
|
a->next = Modes.aircrafts; // .. and put it at the head of the list
|
|
Modes.aircrafts = a;
|
|
}
|
|
|
|
if (mm->signalLevel > 0) {
|
|
a->signalLevel[a->signalNext] = mm->signalLevel;
|
|
a->signalNext = (a->signalNext + 1) & 7;
|
|
}
|
|
a->seen = messageNow();
|
|
a->messages++;
|
|
|
|
// update addrtype, we only ever go towards "more direct" types
|
|
if (mm->addrtype < a->addrtype)
|
|
a->addrtype = mm->addrtype;
|
|
|
|
// if we saw some direct ADS-B for the first time, assume version 0
|
|
if (mm->source == SOURCE_ADSB && a->adsb_version < 0)
|
|
a->adsb_version = 0;
|
|
|
|
// category shouldn't change over time, don't bother with metadata
|
|
if (mm->category_valid) {
|
|
a->category = mm->category;
|
|
}
|
|
|
|
// operational status message
|
|
// done early to update version / HRD / TAH
|
|
if (mm->opstatus.valid) {
|
|
a->adsb_version = mm->opstatus.version;
|
|
if (mm->opstatus.hrd != HEADING_INVALID) {
|
|
a->adsb_hrd = mm->opstatus.hrd;
|
|
}
|
|
if (mm->opstatus.tah != HEADING_INVALID) {
|
|
a->adsb_tah = mm->opstatus.tah;
|
|
}
|
|
}
|
|
|
|
// fill in ADS-B v0 NACp, SIL from position message type
|
|
if (a->adsb_version == 0 && !mm->accuracy.nac_p_valid) {
|
|
int computed_nacp = compute_v0_nacp(mm);
|
|
if (computed_nacp != -1) {
|
|
mm->accuracy.nac_p_valid = 1;
|
|
mm->accuracy.nac_p = computed_nacp;
|
|
}
|
|
}
|
|
|
|
if (a->adsb_version == 0 && mm->accuracy.sil_type == SIL_INVALID) {
|
|
int computed_sil = compute_v0_sil(mm);
|
|
if (computed_sil != -1) {
|
|
mm->accuracy.sil_type = SIL_UNKNOWN;
|
|
mm->accuracy.sil = computed_sil;
|
|
}
|
|
}
|
|
|
|
if (mm->altitude_baro_valid && accept_data(&a->altitude_baro_valid, mm->source)) {
|
|
int alt = altitude_to_feet(mm->altitude_baro, mm->altitude_baro_unit);
|
|
if (a->modeC_hit) {
|
|
int new_modeC = (a->altitude_baro + 49) / 100;
|
|
int old_modeC = (alt + 49) / 100;
|
|
if (new_modeC != old_modeC) {
|
|
a->modeC_hit = 0;
|
|
}
|
|
}
|
|
|
|
a->altitude_baro = alt;
|
|
}
|
|
|
|
if (mm->squawk_valid && accept_data(&a->squawk_valid, mm->source)) {
|
|
if (mm->squawk != a->squawk) {
|
|
a->modeA_hit = 0;
|
|
}
|
|
a->squawk = mm->squawk;
|
|
|
|
#if 0 // Disabled for now as it obscures the origin of the data
|
|
// Handle 7x00 without a corresponding emergency status
|
|
if (!mm->emergency_valid) {
|
|
emergency_t squawk_emergency;
|
|
switch (mm->squawk) {
|
|
case 0x7500:
|
|
squawk_emergency = EMERGENCY_UNLAWFUL;
|
|
break;
|
|
case 0x7600:
|
|
squawk_emergency = EMERGENCY_NORDO;
|
|
break;
|
|
case 0x7700:
|
|
squawk_emergency = EMERGENCY_GENERAL;
|
|
break;
|
|
default:
|
|
squawk_emergency = EMERGENCY_NONE;
|
|
break;
|
|
}
|
|
|
|
if (squawk_emergency != EMERGENCY_NONE && accept_data(&a->emergency_valid, mm->source)) {
|
|
a->emergency = squawk_emergency;
|
|
}
|
|
}
|
|
#endif
|
|
}
|
|
|
|
if (mm->emergency_valid && accept_data(&a->emergency_valid, mm->source)) {
|
|
a->emergency = mm->emergency;
|
|
}
|
|
|
|
if (mm->altitude_geom_valid && accept_data(&a->altitude_geom_valid, mm->source)) {
|
|
a->altitude_geom = altitude_to_feet(mm->altitude_geom, mm->altitude_geom_unit);
|
|
}
|
|
|
|
if (mm->geom_delta_valid && accept_data(&a->geom_delta_valid, mm->source)) {
|
|
a->geom_delta = mm->geom_delta;
|
|
}
|
|
|
|
if (mm->heading_valid) {
|
|
heading_type_t htype = mm->heading_type;
|
|
if (htype == HEADING_MAGNETIC_OR_TRUE) {
|
|
htype = a->adsb_hrd;
|
|
} else if (htype == HEADING_TRACK_OR_HEADING) {
|
|
htype = a->adsb_tah;
|
|
}
|
|
|
|
if (htype == HEADING_GROUND_TRACK && accept_data(&a->track_valid, mm->source)) {
|
|
a->track = mm->heading;
|
|
} else if (htype == HEADING_MAGNETIC && accept_data(&a->mag_heading_valid, mm->source)) {
|
|
a->mag_heading = mm->heading;
|
|
} else if (htype == HEADING_TRUE && accept_data(&a->true_heading_valid, mm->source)) {
|
|
a->true_heading = mm->heading;
|
|
}
|
|
}
|
|
|
|
if (mm->track_rate_valid && accept_data(&a->track_rate_valid, mm->source)) {
|
|
a->track_rate = mm->track_rate;
|
|
}
|
|
|
|
if (mm->roll_valid && accept_data(&a->roll_valid, mm->source)) {
|
|
a->roll = mm->roll;
|
|
}
|
|
|
|
if (mm->gs_valid) {
|
|
mm->gs.selected = (a->adsb_version == 2 ? mm->gs.v2 : mm->gs.v0);
|
|
if (accept_data(&a->gs_valid, mm->source)) {
|
|
a->gs = mm->gs.selected;
|
|
}
|
|
}
|
|
|
|
if (mm->ias_valid && accept_data(&a->ias_valid, mm->source)) {
|
|
a->ias = mm->ias;
|
|
}
|
|
|
|
if (mm->tas_valid && accept_data(&a->tas_valid, mm->source)) {
|
|
a->tas = mm->tas;
|
|
}
|
|
|
|
if (mm->mach_valid && accept_data(&a->mach_valid, mm->source)) {
|
|
a->mach = mm->mach;
|
|
}
|
|
|
|
if (mm->baro_rate_valid && accept_data(&a->baro_rate_valid, mm->source)) {
|
|
a->baro_rate = mm->baro_rate;
|
|
}
|
|
|
|
if (mm->geom_rate_valid && accept_data(&a->geom_rate_valid, mm->source)) {
|
|
a->geom_rate = mm->geom_rate;
|
|
}
|
|
|
|
if (mm->airground != AG_INVALID) {
|
|
// If our current state is UNCERTAIN, accept new data as normal
|
|
// If our current state is certain but new data is not, only accept the uncertain state if the certain data has gone stale
|
|
if (mm->airground != AG_UNCERTAIN ||
|
|
(mm->airground == AG_UNCERTAIN && !trackDataFresh(&a->airground_valid))) {
|
|
if (accept_data(&a->airground_valid, mm->source)) {
|
|
a->airground = mm->airground;
|
|
}
|
|
}
|
|
}
|
|
|
|
if (mm->callsign_valid && accept_data(&a->callsign_valid, mm->source)) {
|
|
memcpy(a->callsign, mm->callsign, sizeof(a->callsign));
|
|
}
|
|
|
|
// prefer MCP over FMS
|
|
// unless the source says otherwise
|
|
if (mm->nav.mcp_altitude_valid && mm->nav.altitude_source != NAV_ALT_FMS && accept_data(&a->nav_altitude_valid, mm->source)) {
|
|
a->nav_altitude = mm->nav.mcp_altitude;
|
|
} else if (mm->nav.fms_altitude_valid && accept_data(&a->nav_altitude_valid, mm->source)) {
|
|
a->nav_altitude = mm->nav.fms_altitude;
|
|
}
|
|
|
|
if (mm->nav.heading_valid && accept_data(&a->nav_heading_valid, mm->source)) {
|
|
a->nav_heading = mm->nav.heading;
|
|
}
|
|
|
|
if (mm->nav.modes_valid && accept_data(&a->nav_modes_valid, mm->source)) {
|
|
a->nav_modes = mm->nav.modes;
|
|
}
|
|
|
|
if (mm->nav.qnh_valid && accept_data(&a->nav_qnh_valid, mm->source)) {
|
|
a->nav_qnh = mm->nav.qnh;
|
|
}
|
|
|
|
// CPR, even
|
|
if (mm->cpr_valid && !mm->cpr_odd && accept_data(&a->cpr_even_valid, mm->source)) {
|
|
a->cpr_even_type = mm->cpr_type;
|
|
a->cpr_even_lat = mm->cpr_lat;
|
|
a->cpr_even_lon = mm->cpr_lon;
|
|
compute_nic_rc_from_message(mm, a, &a->cpr_even_nic, &a->cpr_even_rc);
|
|
}
|
|
|
|
// CPR, odd
|
|
if (mm->cpr_valid && mm->cpr_odd && accept_data(&a->cpr_odd_valid, mm->source)) {
|
|
a->cpr_odd_type = mm->cpr_type;
|
|
a->cpr_odd_lat = mm->cpr_lat;
|
|
a->cpr_odd_lon = mm->cpr_lon;
|
|
compute_nic_rc_from_message(mm, a, &a->cpr_odd_nic, &a->cpr_odd_rc);
|
|
}
|
|
|
|
if (mm->accuracy.sda_valid && accept_data(&a->sda_valid, mm->source)) {
|
|
a->sda = mm->accuracy.sda;
|
|
}
|
|
|
|
if (mm->accuracy.nic_a_valid && accept_data(&a->nic_a_valid, mm->source)) {
|
|
a->nic_a = mm->accuracy.nic_a;
|
|
}
|
|
|
|
if (mm->accuracy.nic_c_valid && accept_data(&a->nic_c_valid, mm->source)) {
|
|
a->nic_c = mm->accuracy.nic_c;
|
|
}
|
|
|
|
if (mm->accuracy.nic_baro_valid && accept_data(&a->nic_baro_valid, mm->source)) {
|
|
a->nic_baro = mm->accuracy.nic_baro;
|
|
}
|
|
|
|
if (mm->accuracy.nac_p_valid && accept_data(&a->nac_p_valid, mm->source)) {
|
|
a->nac_p = mm->accuracy.nac_p;
|
|
}
|
|
|
|
if (mm->accuracy.nac_v_valid && accept_data(&a->nac_v_valid, mm->source)) {
|
|
a->nac_v = mm->accuracy.nac_v;
|
|
}
|
|
|
|
if (mm->accuracy.sil_type != SIL_INVALID && accept_data(&a->sil_valid, mm->source)) {
|
|
a->sil = mm->accuracy.sil;
|
|
if (a->sil_type == SIL_INVALID || mm->accuracy.sil_type != SIL_UNKNOWN) {
|
|
a->sil_type = mm->accuracy.sil_type;
|
|
}
|
|
}
|
|
|
|
if (mm->accuracy.gva_valid && accept_data(&a->gva_valid, mm->source)) {
|
|
a->gva = mm->accuracy.gva;
|
|
}
|
|
|
|
if (mm->accuracy.sda_valid && accept_data(&a->sda_valid, mm->source)) {
|
|
a->sda = mm->accuracy.sda;
|
|
}
|
|
|
|
// Now handle derived data
|
|
|
|
// derive geometric altitude if we have baro + delta
|
|
if (compare_validity(&a->altitude_baro_valid, &a->altitude_geom_valid) > 0 &&
|
|
compare_validity(&a->geom_delta_valid, &a->altitude_geom_valid) > 0) {
|
|
// Baro and delta are both more recent than geometric, derive geometric from baro + delta
|
|
a->altitude_geom = a->altitude_baro + a->geom_delta;
|
|
combine_validity(&a->altitude_geom_valid, &a->altitude_baro_valid, &a->geom_delta_valid);
|
|
}
|
|
|
|
// If we've got a new cprlat or cprlon
|
|
if (mm->cpr_valid) {
|
|
updatePosition(a, mm);
|
|
}
|
|
|
|
return (a);
|
|
}
|
|
|
|
//
|
|
// Periodic updates of tracking state
|
|
//
|
|
|
|
// Periodically match up mode A/C results with mode S results
|
|
static void trackMatchAC(uint64_t now)
|
|
{
|
|
// clear match flags
|
|
for (unsigned i = 0; i < 4096; ++i) {
|
|
modeAC_match[i] = 0;
|
|
}
|
|
|
|
// scan aircraft list, look for matches
|
|
for (struct aircraft *a = Modes.aircrafts; a; a = a->next) {
|
|
if ((now - a->seen) > 5000) {
|
|
continue;
|
|
}
|
|
|
|
// match on Mode A
|
|
if (trackDataValid(&a->squawk_valid)) {
|
|
unsigned i = modeAToIndex(a->squawk);
|
|
if ((modeAC_count[i] - modeAC_lastcount[i]) >= TRACK_MODEAC_MIN_MESSAGES) {
|
|
a->modeA_hit = 1;
|
|
modeAC_match[i] = (modeAC_match[i] ? 0xFFFFFFFF : a->addr);
|
|
}
|
|
}
|
|
|
|
// match on Mode C (+/- 100ft)
|
|
if (trackDataValid(&a->altitude_baro_valid)) {
|
|
int modeC = (a->altitude_baro + 49) / 100;
|
|
|
|
unsigned modeA = modeCToModeA(modeC);
|
|
unsigned i = modeAToIndex(modeA);
|
|
if (modeA && (modeAC_count[i] - modeAC_lastcount[i]) >= TRACK_MODEAC_MIN_MESSAGES) {
|
|
a->modeC_hit = 1;
|
|
modeAC_match[i] = (modeAC_match[i] ? 0xFFFFFFFF : a->addr);
|
|
}
|
|
|
|
modeA = modeCToModeA(modeC + 1);
|
|
i = modeAToIndex(modeA);
|
|
if (modeA && (modeAC_count[i] - modeAC_lastcount[i]) >= TRACK_MODEAC_MIN_MESSAGES) {
|
|
a->modeC_hit = 1;
|
|
modeAC_match[i] = (modeAC_match[i] ? 0xFFFFFFFF : a->addr);
|
|
}
|
|
|
|
modeA = modeCToModeA(modeC - 1);
|
|
i = modeAToIndex(modeA);
|
|
if (modeA && (modeAC_count[i] - modeAC_lastcount[i]) >= TRACK_MODEAC_MIN_MESSAGES) {
|
|
a->modeC_hit = 1;
|
|
modeAC_match[i] = (modeAC_match[i] ? 0xFFFFFFFF : a->addr);
|
|
}
|
|
}
|
|
}
|
|
|
|
// reset counts for next time
|
|
for (unsigned i = 0; i < 4096; ++i) {
|
|
if (!modeAC_count[i])
|
|
continue;
|
|
|
|
if ((modeAC_count[i] - modeAC_lastcount[i]) < TRACK_MODEAC_MIN_MESSAGES) {
|
|
if (++modeAC_age[i] > 15) {
|
|
// not heard from for a while, clear it out
|
|
modeAC_lastcount[i] = modeAC_count[i] = modeAC_age[i] = 0;
|
|
}
|
|
} else {
|
|
// this one is live
|
|
// set a high initial age for matches, so they age out rapidly
|
|
// and don't show up on the interactive display when the matching
|
|
// mode S data goes away or changes
|
|
if (modeAC_match[i]) {
|
|
modeAC_age[i] = 10;
|
|
} else {
|
|
modeAC_age[i] = 0;
|
|
}
|
|
}
|
|
|
|
modeAC_lastcount[i] = modeAC_count[i];
|
|
}
|
|
}
|
|
|
|
//
|
|
//=========================================================================
|
|
//
|
|
// If we don't receive new nessages within TRACK_AIRCRAFT_TTL
|
|
// we remove the aircraft from the list.
|
|
//
|
|
static void trackRemoveStaleAircraft(uint64_t now)
|
|
{
|
|
struct aircraft *a = Modes.aircrafts;
|
|
struct aircraft *prev = NULL;
|
|
|
|
while(a) {
|
|
if ((now - a->seen) > TRACK_AIRCRAFT_TTL ||
|
|
(a->messages == 1 && (now - a->seen) > TRACK_AIRCRAFT_ONEHIT_TTL)) {
|
|
// Count aircraft where we saw only one message before reaping them.
|
|
// These are likely to be due to messages with bad addresses.
|
|
if (a->messages == 1)
|
|
Modes.stats_current.single_message_aircraft++;
|
|
|
|
// Remove the element from the linked list, with care
|
|
// if we are removing the first element
|
|
if (!prev) {
|
|
Modes.aircrafts = a->next; free(a); a = Modes.aircrafts;
|
|
} else {
|
|
prev->next = a->next; free(a); a = prev->next;
|
|
}
|
|
} else {
|
|
|
|
#define EXPIRE(_f) do { if (a->_f##_valid.source != SOURCE_INVALID && now >= a->_f##_valid.expires) { a->_f##_valid.source = SOURCE_INVALID; } } while (0)
|
|
EXPIRE(callsign);
|
|
EXPIRE(altitude_baro);
|
|
EXPIRE(altitude_geom);
|
|
EXPIRE(geom_delta);
|
|
EXPIRE(gs);
|
|
EXPIRE(ias);
|
|
EXPIRE(tas);
|
|
EXPIRE(mach);
|
|
EXPIRE(track);
|
|
EXPIRE(track_rate);
|
|
EXPIRE(roll);
|
|
EXPIRE(mag_heading);
|
|
EXPIRE(true_heading);
|
|
EXPIRE(baro_rate);
|
|
EXPIRE(geom_rate);
|
|
EXPIRE(squawk);
|
|
EXPIRE(airground);
|
|
EXPIRE(nav_qnh);
|
|
EXPIRE(nav_altitude);
|
|
EXPIRE(nav_heading);
|
|
EXPIRE(nav_modes);
|
|
EXPIRE(cpr_odd);
|
|
EXPIRE(cpr_even);
|
|
EXPIRE(position);
|
|
EXPIRE(nic_a);
|
|
EXPIRE(nic_c);
|
|
EXPIRE(nic_baro);
|
|
EXPIRE(nac_p);
|
|
EXPIRE(sil);
|
|
EXPIRE(gva);
|
|
EXPIRE(sda);
|
|
#undef EXPIRE
|
|
prev = a; a = a->next;
|
|
}
|
|
}
|
|
}
|
|
|
|
|
|
//
|
|
// Entry point for periodic updates
|
|
//
|
|
|
|
void trackPeriodicUpdate()
|
|
{
|
|
static uint64_t next_update;
|
|
uint64_t now = mstime();
|
|
|
|
// Only do updates once per second
|
|
if (now >= next_update) {
|
|
next_update = now + 1000;
|
|
trackRemoveStaleAircraft(now);
|
|
trackMatchAC(now);
|
|
}
|
|
}
|