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https://github.com/ArduPilot/ardupilot
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AP_ADSB: cleanup
non-functional change
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5adbf9b232
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@ -462,8 +462,6 @@ void AP_ADSB::send_adsb_vehicle(const mavlink_channel_t chan)
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void AP_ADSB::send_dynamic_out(const mavlink_channel_t chan)
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void AP_ADSB::send_dynamic_out(const mavlink_channel_t chan)
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{
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{
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// --------------
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// Knowns
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AP_GPS gps = _ahrs.get_gps();
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AP_GPS gps = _ahrs.get_gps();
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Vector3f gps_velocity = gps.velocity();
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Vector3f gps_velocity = gps.velocity();
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@ -504,20 +502,10 @@ void AP_ADSB::send_dynamic_out(const mavlink_channel_t chan)
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state |= UAVIONIX_ADSB_OUT_DYNAMIC_STATE_ON_GROUND;
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state |= UAVIONIX_ADSB_OUT_DYNAMIC_STATE_ON_GROUND;
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}
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}
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// --------------
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// Not Sure
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uint32_t utcTime = UINT_MAX; // uint32_t utcTime,
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// TODO: confirm this sets utcTime correctly
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// TODO: confirm this sets utcTime correctly
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const uint64_t gps_time = gps.time_epoch_usec();
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const uint64_t gps_time = gps.time_epoch_usec();
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utcTime = gps_time / 1000000ULL;
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const uint32_t utcTime = gps_time / 1000000ULL;
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// --------------
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// Unknowns
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// TODO: implement http://www.srh.noaa.gov/images/epz/wxcalc/pressureAltitude.pdf
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AP_Baro baro = _ahrs.get_baro();
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AP_Baro baro = _ahrs.get_baro();
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int32_t altPres = INT_MAX;
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int32_t altPres = INT_MAX;
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if (baro.healthy()) {
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if (baro.healthy()) {
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