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commander: centralise home position publication
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@ -1237,49 +1237,54 @@ static void commander_set_home_position(orb_advert_t &homePub, home_position_s &
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const vehicle_local_position_s &localPosition, const vehicle_global_position_s &globalPosition,
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const vehicle_attitude_s &attitude)
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{
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//Need global and local position fix to be able to set home
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if (!status_flags.condition_global_position_valid || !status_flags.condition_local_position_valid) {
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// Need global and local position fix to be able to set home
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// Ensure that the GPS accuracy is good enough
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if (status_flags.condition_global_position_valid
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&& status_flags.condition_local_position_valid
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&& (globalPosition.eph > eph_threshold || globalPosition.epv > epv_threshold)) {
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//Set home position
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home.timestamp = hrt_absolute_time();
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home.lat = globalPosition.lat;
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home.lon = globalPosition.lon;
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home.valid_hpos = true;
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home.alt = globalPosition.alt;
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home.valid_alt = true;
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home.x = localPosition.x;
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home.y = localPosition.y;
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home.z = localPosition.z;
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matrix::Eulerf euler = matrix::Quatf(attitude.q);
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home.yaw = euler.psi();
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PX4_INFO("home: %.7f, %.7f, %.2f", home.lat, home.lon, (double)home.alt);
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//Play tune first time we initialize HOME
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if (!status_flags.condition_home_position_valid) {
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tune_home_set(true);
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}
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/* mark home position as set */
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status_flags.condition_home_position_valid = true;
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} else if (!home.valid_alt && localPosition.z_global) {
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// Handle case where we have started global height estimation after takeoff and can only set the home altitude
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home.timestamp = hrt_absolute_time();
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home.alt = localPosition.ref_alt;
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home.valid_alt = true;
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PX4_INFO("home alt: %.2f", (double)home.alt);
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} else {
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return;
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}
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//Ensure that the GPS accuracy is good enough for intializing home
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if (globalPosition.eph > eph_threshold || globalPosition.epv > epv_threshold) {
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return;
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}
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//Set home position
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home.timestamp = hrt_absolute_time();
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home.lat = globalPosition.lat;
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home.lon = globalPosition.lon;
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home.valid_hpos = true;
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home.alt = globalPosition.alt;
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home.valid_alt = true;
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home.x = localPosition.x;
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home.y = localPosition.y;
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home.z = localPosition.z;
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matrix::Eulerf euler = matrix::Quatf(attitude.q);
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home.yaw = euler.psi();
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PX4_INFO("home: %.7f, %.7f, %.2f", home.lat, home.lon, (double)home.alt);
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/* announce new home position */
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if (homePub != nullptr) {
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orb_publish(ORB_ID(home_position), homePub, &home);
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} else {
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homePub = orb_advertise(ORB_ID(home_position), &home);
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}
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//Play tune first time we initialize HOME
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if (!status_flags.condition_home_position_valid) {
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tune_home_set(true);
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}
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/* mark home position as set */
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status_flags.condition_home_position_valid = true;
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}
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int commander_thread_main(int argc, char *argv[])
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@ -3120,20 +3125,9 @@ int commander_thread_main(int argc, char *argv[])
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/* Set home position altitude to EKF origin height if home is not set and the EKF has a global origin.
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* This allows home atitude to be used in the calculation of height above takeoff location when GPS
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* use has commenced after takeoff. */
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if (!_home.valid_alt && local_position.z_global) {
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_home.timestamp = hrt_absolute_time();
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_home.alt = local_position.ref_alt;
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_home.valid_alt = true;
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else if (!_home.valid_alt && local_position.z_global) {
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commander_set_home_position(home_pub, _home, local_position, global_position, attitude);
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/* publish new home altitude */
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if (home_pub != nullptr) {
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orb_publish(ORB_ID(home_position), home_pub, &_home);
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} else {
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home_pub = orb_advertise(ORB_ID(home_position), &_home);
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}
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PX4_INFO("home alt: %.2f", (double)_home.alt);
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}
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// check for arming state change
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