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Navigator resurrect FW GPS failure navigation (#7762)
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@@ -37,24 +37,21 @@
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* @author Thomas Gubler <thomasgubler@gmail.com>
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*/
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#include <string.h>
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#include <stdlib.h>
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#include <math.h>
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#include <fcntl.h>
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#include "gpsfailure.h"
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#include "navigator.h"
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#include <systemlib/mavlink_log.h>
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#include <systemlib/err.h>
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#include <geo/geo.h>
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#include <navigator/navigation.h>
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#include <uORB/uORB.h>
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#include <uORB/topics/mission.h>
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#include <uORB/topics/home_position.h>
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#include <mathlib/mathlib.h>
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#include "navigator.h"
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#include "gpsfailure.h"
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using matrix::Eulerf;
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using matrix::Quatf;
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#define DELAY_SIGMA 0.01f
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static constexpr float DELAY_SIGMA = 0.01f;
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GpsFailure::GpsFailure(Navigator *navigator, const char *name) :
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MissionBlock(navigator, name),
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@@ -67,14 +64,11 @@ GpsFailure::GpsFailure(Navigator *navigator, const char *name) :
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{
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/* load initial params */
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updateParams();
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/* initial reset */
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on_inactive();
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}
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GpsFailure::~GpsFailure()
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{
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}
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void
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GpsFailure::on_inactive()
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{
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@@ -96,24 +90,34 @@ GpsFailure::on_activation()
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void
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GpsFailure::on_active()
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{
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switch (_gpsf_state) {
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case GPSF_STATE_LOITER: {
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/* Position controller does not run in this mode:
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* navigator has to publish an attitude setpoint */
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_navigator->get_att_sp()->roll_body = M_DEG_TO_RAD_F * _param_openlooploiter_roll.get();
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_navigator->get_att_sp()->pitch_body = M_DEG_TO_RAD_F * _param_openlooploiter_pitch.get();
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_navigator->get_att_sp()->thrust = _param_openlooploiter_thrust.get();
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_navigator->publish_att_sp();
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vehicle_attitude_setpoint_s att_sp = {};
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att_sp.timestamp = hrt_absolute_time();
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att_sp.roll_body = math::radians(_param_openlooploiter_roll.get());
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att_sp.pitch_body = math::radians(_param_openlooploiter_pitch.get());
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att_sp.thrust = _param_openlooploiter_thrust.get();
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Quatf q(Eulerf(att_sp.roll_body, att_sp.pitch_body, 0.0f));
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q.copyTo(att_sp.q_d);
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att_sp.q_d_valid = true;
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if (_att_sp_pub != nullptr) {
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/* publish att sp*/
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orb_publish(ORB_ID(vehicle_attitude_setpoint), _att_sp_pub, &att_sp);
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} else {
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/* advertise and publish */
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_att_sp_pub = orb_advertise(ORB_ID(vehicle_attitude_setpoint), &att_sp);
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}
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/* Measure time */
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hrt_abstime elapsed = hrt_elapsed_time(&_timestamp_activation);
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//warnx("open loop loiter, posctl enabled %u, elapsed %.1fs, thrust %.2f",
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//_navigator->get_control_mode()->flag_control_position_enabled, elapsed * 1e-6, (double)_param_openlooploiter_thrust.get());
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if (elapsed > _param_loitertime.get() * 1e6f) {
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/* no recovery, adavance the state machine */
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warnx("gps not recovered, switch to next state");
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if ((_param_loitertime.get() > FLT_EPSILON) &&
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(hrt_elapsed_time(&_timestamp_activation) > _param_loitertime.get() * 1e6f)) {
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/* no recovery, advance the state machine */
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PX4_WARN("GPS not recovered, switching to next failure state");
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advance_gpsf();
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}
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@@ -142,17 +146,17 @@ GpsFailure::set_gpsf_item()
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switch (_gpsf_state) {
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case GPSF_STATE_TERMINATE: {
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/* Request flight termination from the commander */
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/* Request flight termination from commander */
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_navigator->get_mission_result()->flight_termination = true;
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_navigator->set_mission_result_updated();
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warnx("gps fail: request flight termination");
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PX4_WARN("GPS failure: request flight termination");
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}
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break;
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default:
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break;
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}
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reset_mission_item_reached();
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_navigator->set_position_setpoint_triplet_updated();
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}
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@@ -162,20 +166,18 @@ GpsFailure::advance_gpsf()
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switch (_gpsf_state) {
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case GPSF_STATE_NONE:
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_gpsf_state = GPSF_STATE_LOITER;
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warnx("gpsf loiter");
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mavlink_log_critical(_navigator->get_mavlink_log_pub(), "GPS failed: open loop loiter");
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mavlink_log_critical(_navigator->get_mavlink_log_pub(), "Global position failure: fixed bank loiter");
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break;
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case GPSF_STATE_LOITER:
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_gpsf_state = GPSF_STATE_TERMINATE;
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warnx("gpsf terminate");
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mavlink_log_emergency(_navigator->get_mavlink_log_pub(), "no gps recovery, termination");
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warnx("mavlink sent");
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mavlink_log_emergency(_navigator->get_mavlink_log_pub(), "no GPS recovery, terminating flight");
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break;
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case GPSF_STATE_TERMINATE:
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warnx("gpsf end");
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PX4_WARN("terminate");
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_gpsf_state = GPSF_STATE_END;
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break;
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default:
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break;
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