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https://github.com/PX4/PX4-Autopilot.git
synced 2026-05-22 06:14:14 +08:00
fix: allow altitude changes in course mode
This commit is contained in:
@@ -876,11 +876,19 @@ Commander::handle_command(const vehicle_command_s &cmd)
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answer_command(cmd, vehicle_command_ack_s::VEHICLE_CMD_RESULT_UNSUPPORTED);
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} else {
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if (_user_mode_intention.change(vehicle_status_s::NAVIGATION_STATE_AUTO_LOITER, getSourceFromCommand(cmd))) {
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// If already in course mode, stay in course mode (navigator handles any altitude update)
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// Only switch to loiter if a specific lat/lon target is given, or we are not in course mode.
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const bool has_position_target = PX4_ISFINITE(cmd.param5) && PX4_ISFINITE(cmd.param6);
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const bool in_course_mode = _vehicle_status.nav_state == vehicle_status_s::NAVIGATION_STATE_AUTO_COURSE;
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const uint8_t target_state = (in_course_mode && !has_position_target)
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? vehicle_status_s::NAVIGATION_STATE_AUTO_COURSE
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: vehicle_status_s::NAVIGATION_STATE_AUTO_LOITER;
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if (_user_mode_intention.change(target_state, getSourceFromCommand(cmd))) {
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cmd_result = vehicle_command_ack_s::VEHICLE_CMD_RESULT_ACCEPTED;
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} else {
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printRejectMode(vehicle_status_s::NAVIGATION_STATE_AUTO_LOITER);
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printRejectMode(target_state);
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cmd_result = vehicle_command_ack_s::VEHICLE_CMD_RESULT_TEMPORARILY_REJECTED;
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}
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}
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@@ -570,6 +570,19 @@ FixedWingModeManager::control_auto(const float control_interval, const Vector2d
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position_setpoint_s current_sp = pos_sp_curr;
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move_position_setpoint_for_vtol_transition(current_sp);
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// Course and heading setpoints are handled directly before setpoint-type resolution.
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// Dispatching here avoids handle_setpoint_type() misidentifying these as stationary
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// position setpoints (dist_xy ≈ 0) and incorrectly downgrading them to LOITER.
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if (PX4_ISFINITE(current_sp.course) || PX4_ISFINITE(current_sp.yaw)) {
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control_auto_position(control_interval, curr_pos, ground_speed, pos_sp_prev, current_sp);
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if (!_vehicle_status.in_transition_to_fw) {
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publishLocalPositionSetpoint(current_sp);
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}
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return;
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}
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const uint8_t position_sp_type = handle_setpoint_type(current_sp, pos_sp_next);
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_position_sp_type = position_sp_type;
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@@ -280,153 +280,165 @@ void Navigator::run()
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// only update the reposition setpoint if armed, as it otherwise won't get executed until the vehicle switches to loiter,
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// which can lead to dangerous and unexpected behaviors (see loiter.cpp, there is an if(armed) in there too)
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// Wait for vehicle_status before handling the next command, otherwise the setpoint could be overwritten
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_wait_for_vehicle_status_timestamp = hrt_absolute_time();
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vehicle_global_position_s position_setpoint{};
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if (PX4_ISFINITE(cmd.param5) && PX4_ISFINITE(cmd.param6)) {
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position_setpoint.lat = cmd.param5;
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position_setpoint.lon = cmd.param6;
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// In course mode with only an altitude change (no lat/lon target), update the course altitude directly.
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// The reposition triplet is not used in course mode — the course mode publishes its own setpoint each tick.
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if (_navigation_mode == &_course
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&& !PX4_ISFINITE(cmd.param5) && !PX4_ISFINITE(cmd.param6)
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&& PX4_ISFINITE(cmd.param7)) {
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_course.set_altitude(cmd.param7);
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// DO_REPOSITION is acknowledged by commander
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} else {
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position_setpoint.lat = get_global_position()->lat;
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position_setpoint.lon = get_global_position()->lon;
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}
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position_setpoint.alt = PX4_ISFINITE(cmd.param7) ? cmd.param7 : get_global_position()->alt;
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// Wait for vehicle_status before handling the next command, otherwise the setpoint could be overwritten
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_wait_for_vehicle_status_timestamp = hrt_absolute_time();
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if (geofence_allows_position(position_setpoint)) {
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position_setpoint_triplet_s *rep = get_reposition_triplet();
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position_setpoint_triplet_s *curr = get_position_setpoint_triplet();
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// store current position as previous position and goal as next
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rep->previous.yaw = get_local_position()->heading;
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rep->previous.lat = get_global_position()->lat;
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rep->previous.lon = get_global_position()->lon;
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rep->previous.alt = get_global_position()->alt;
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rep->current.type = position_setpoint_s::SETPOINT_TYPE_LOITER;
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bool only_alt_change_requested = false;
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// If no argument for ground speed, use default value.
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if (cmd.param1 <= 0 || !PX4_ISFINITE(cmd.param1)) {
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// on entering Loiter mode, reset speed setpoint to default
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if (_navigation_mode != &_loiter) {
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rep->current.cruising_speed = -1.f;
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} else {
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rep->current.cruising_speed = get_cruising_speed();
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}
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} else {
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rep->current.cruising_speed = cmd.param1;
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}
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rep->current.cruising_throttle = get_cruising_throttle();
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rep->current.acceptance_radius = get_acceptance_radius();
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// Go on and check which changes had been requested
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if (PX4_ISFINITE(cmd.param4)) {
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rep->current.yaw = cmd.param4;
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} else {
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rep->current.yaw = NAN;
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}
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vehicle_global_position_s position_setpoint{};
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if (PX4_ISFINITE(cmd.param5) && PX4_ISFINITE(cmd.param6)) {
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// Position change with optional altitude change
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rep->current.lat = cmd.param5;
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rep->current.lon = cmd.param6;
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if (PX4_ISFINITE(cmd.param7)) {
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rep->current.alt = cmd.param7;
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} else {
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rep->current.alt = get_global_position()->alt;
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}
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} else if (PX4_ISFINITE(cmd.param7) || PX4_ISFINITE(cmd.param4)) {
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// Position is not changing, thus we keep the setpoint
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rep->current.lat = PX4_ISFINITE(curr->current.lat) ? curr->current.lat : get_global_position()->lat;
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rep->current.lon = PX4_ISFINITE(curr->current.lon) ? curr->current.lon : get_global_position()->lon;
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if (PX4_ISFINITE(cmd.param7)) {
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rep->current.alt = cmd.param7;
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only_alt_change_requested = true;
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} else {
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rep->current.alt = get_global_position()->alt;
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}
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position_setpoint.lat = cmd.param5;
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position_setpoint.lon = cmd.param6;
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} else {
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// All three set to NaN - pause vehicle
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rep->current.alt = get_global_position()->alt;
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if (_vstatus.vehicle_type == vehicle_status_s::VEHICLE_TYPE_ROTARY_WING
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&& (get_position_setpoint_triplet()->current.type != position_setpoint_s::SETPOINT_TYPE_TAKEOFF)) {
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preproject_stop_point(rep->current.lat, rep->current.lon);
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} else {
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// For fixedwings we can use the current vehicle's position to define the loiter point
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rep->current.lat = get_global_position()->lat;
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rep->current.lon = get_global_position()->lon;
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}
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position_setpoint.lat = get_global_position()->lat;
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position_setpoint.lon = get_global_position()->lon;
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}
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if (only_alt_change_requested) {
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if (PX4_ISFINITE(curr->current.loiter_radius) && curr->current.loiter_radius > FLT_EPSILON) {
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rep->current.loiter_radius = curr->current.loiter_radius;
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position_setpoint.alt = PX4_ISFINITE(cmd.param7) ? cmd.param7 : get_global_position()->alt;
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if (geofence_allows_position(position_setpoint)) {
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position_setpoint_triplet_s *rep = get_reposition_triplet();
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position_setpoint_triplet_s *curr = get_position_setpoint_triplet();
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// store current position as previous position and goal as next
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rep->previous.yaw = get_local_position()->heading;
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rep->previous.lat = get_global_position()->lat;
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rep->previous.lon = get_global_position()->lon;
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rep->previous.alt = get_global_position()->alt;
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rep->current.type = position_setpoint_s::SETPOINT_TYPE_LOITER;
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bool only_alt_change_requested = false;
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// If no argument for ground speed, use default value.
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if (cmd.param1 <= 0 || !PX4_ISFINITE(cmd.param1)) {
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// on entering Loiter mode, reset speed setpoint to default
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if (_navigation_mode != &_loiter) {
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rep->current.cruising_speed = -1.f;
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} else {
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rep->current.cruising_speed = get_cruising_speed();
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}
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} else {
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rep->current.loiter_radius = get_default_loiter_rad();
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rep->current.cruising_speed = cmd.param1;
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}
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if (PX4_ISFINITE(curr->current.loiter_minor_radius) && fabsf(curr->current.loiter_minor_radius) > FLT_EPSILON) {
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rep->current.loiter_minor_radius = curr->current.loiter_minor_radius;
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rep->current.cruising_throttle = get_cruising_throttle();
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rep->current.acceptance_radius = get_acceptance_radius();
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// Go on and check which changes had been requested
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if (PX4_ISFINITE(cmd.param4)) {
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rep->current.yaw = cmd.param4;
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} else {
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rep->current.loiter_minor_radius = NAN;
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rep->current.yaw = NAN;
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}
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if (PX4_ISFINITE(curr->current.loiter_orientation) && fabsf(curr->current.loiter_minor_radius) > FLT_EPSILON) {
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rep->current.loiter_orientation = curr->current.loiter_orientation;
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if (PX4_ISFINITE(cmd.param5) && PX4_ISFINITE(cmd.param6)) {
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// Position change with optional altitude change
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rep->current.lat = cmd.param5;
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rep->current.lon = cmd.param6;
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if (PX4_ISFINITE(cmd.param7)) {
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rep->current.alt = cmd.param7;
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} else {
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rep->current.alt = get_global_position()->alt;
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}
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} else if (PX4_ISFINITE(cmd.param7) || PX4_ISFINITE(cmd.param4)) {
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// Position is not changing, thus we keep the setpoint
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rep->current.lat = PX4_ISFINITE(curr->current.lat) ? curr->current.lat : get_global_position()->lat;
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rep->current.lon = PX4_ISFINITE(curr->current.lon) ? curr->current.lon : get_global_position()->lon;
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if (PX4_ISFINITE(cmd.param7)) {
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rep->current.alt = cmd.param7;
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only_alt_change_requested = true;
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} else {
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rep->current.alt = get_global_position()->alt;
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}
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} else {
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rep->current.loiter_orientation = 0.0f;
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// All three set to NaN - pause vehicle
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rep->current.alt = get_global_position()->alt;
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if (_vstatus.vehicle_type == vehicle_status_s::VEHICLE_TYPE_ROTARY_WING
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&& (get_position_setpoint_triplet()->current.type != position_setpoint_s::SETPOINT_TYPE_TAKEOFF)) {
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preproject_stop_point(rep->current.lat, rep->current.lon);
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} else {
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// For fixedwings we can use the current vehicle's position to define the loiter point
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rep->current.lat = get_global_position()->lat;
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rep->current.lon = get_global_position()->lon;
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}
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}
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if (curr->current.loiter_pattern > 0) {
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rep->current.loiter_pattern = curr->current.loiter_pattern;
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if (only_alt_change_requested) {
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if (PX4_ISFINITE(curr->current.loiter_radius) && curr->current.loiter_radius > FLT_EPSILON) {
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rep->current.loiter_radius = curr->current.loiter_radius;
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} else {
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rep->current.loiter_pattern = position_setpoint_s::LOITER_TYPE_ORBIT;
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} else {
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rep->current.loiter_radius = get_default_loiter_rad();
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}
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if (PX4_ISFINITE(curr->current.loiter_minor_radius) && fabsf(curr->current.loiter_minor_radius) > FLT_EPSILON) {
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rep->current.loiter_minor_radius = curr->current.loiter_minor_radius;
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} else {
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rep->current.loiter_minor_radius = NAN;
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}
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if (PX4_ISFINITE(curr->current.loiter_orientation) && fabsf(curr->current.loiter_minor_radius) > FLT_EPSILON) {
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rep->current.loiter_orientation = curr->current.loiter_orientation;
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} else {
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rep->current.loiter_orientation = 0.0f;
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}
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if (curr->current.loiter_pattern > 0) {
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rep->current.loiter_pattern = curr->current.loiter_pattern;
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} else {
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rep->current.loiter_pattern = position_setpoint_s::LOITER_TYPE_ORBIT;
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}
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rep->current.loiter_direction_counter_clockwise = curr->current.loiter_direction_counter_clockwise;
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}
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rep->current.loiter_direction_counter_clockwise = curr->current.loiter_direction_counter_clockwise;
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rep->previous.timestamp = hrt_absolute_time();
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rep->current.valid = true;
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rep->current.timestamp = hrt_absolute_time();
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rep->next.valid = false;
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_time_loitering_after_gf_breach = 0; // have to manually reset this in all LOITER cases
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} else {
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mavlink_log_critical(&_mavlink_log_pub, "Reposition is outside geofence\t");
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events::send(events::ID("navigator_reposition_outside_geofence"), {events::Log::Error, events::LogInternal::Info},
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"Reposition is outside geofence");
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}
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rep->previous.timestamp = hrt_absolute_time();
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// CMD_DO_REPOSITION is acknowledged by commander
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rep->current.valid = true;
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rep->current.timestamp = hrt_absolute_time();
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rep->next.valid = false;
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_time_loitering_after_gf_breach = 0; // have to manually reset this in all LOITER cases
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} else {
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mavlink_log_critical(&_mavlink_log_pub, "Reposition is outside geofence\t");
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events::send(events::ID("navigator_reposition_outside_geofence"), {events::Log::Error, events::LogInternal::Info},
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"Reposition is outside geofence");
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}
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// CMD_DO_REPOSITION is acknowledged by commander
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} else if (cmd.command == vehicle_command_s::VEHICLE_CMD_DO_CHANGE_ALTITUDE
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&& _vstatus.arming_state == vehicle_status_s::ARMING_STATE_ARMED) {
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// only update the setpoint if armed, as it otherwise won't get executed until the vehicle switches to loiter,
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@@ -1272,6 +1284,7 @@ void Navigator::reset_position_setpoint(position_setpoint_s &sp)
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sp.lat = static_cast<double>(NAN);
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sp.lon = static_cast<double>(NAN);
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sp.yaw = NAN;
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sp.course = NAN;
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sp.loiter_radius = get_default_loiter_rad();
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sp.acceptance_radius = get_default_acceptance_radius();
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sp.cruising_speed = get_cruising_speed();
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