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* PositionSetpoint: remove yaw_valid field * Navigator: set yaw setpoint to NAN for Takeoff Don't set a yaw setpoint for takeoff, as Navigator doesn't handle the yaw reset. The yaw setpoint generation is handled by FlightTaskAuto. * PositionSetpoint.msg: remove disable_weather_vane and instead only use the yaw field Strictly follow the concept that if the position_setpoint.yaw is set, then follow it the controller, and otherwise let the controller set it as it thinks it's best. * Navigator: remove logic that sets yaw to be accepted in TAKEOFF No longer needed as during Takeoff we anyway don't set a yaw setpoint. * PositionSetpoint.msg: remove yawspeed_valid * PositionSetpoint.msg: remove yawspeed * Navigator: set yaw setpoint to NAN instead of current In set_takeoff and set_land_item, as well as for VTOL transition. The flight tasks then set the yaw corresponding to the current yaw. * Navigator: change get_yaw_acceptance into a bool * PositionSetpoint.msg: improve comment for yaw * MissionBlock: remove unnecessary code from set_vtol_transition_item * Navigator: clean up calculate_breaking_stop(), set yaw to NAN * Navigator: set yaw to NAN in variouls places where not specifc setpoint is desired * Navigator: set yaw to NAN in reset_position_setpoint() --------- Signed-off-by: Silvan Fuhrer <silvan@auterion.com> Co-authored-by: Matthias Grob <maetugr@gmail.com>
498 lines
18 KiB
C++
498 lines
18 KiB
C++
/****************************************************************************
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*
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* Copyright (c) 2013-2021 PX4 Development Team. 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
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* are met:
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*
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* 1. 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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* 2. Redistributions in binary form must reproduce the above copyright
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* notice, this list of conditions and the following disclaimer in
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* the documentation and/or other materials provided with the
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* distribution.
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* 3. Neither the name PX4 nor the names of its contributors may be
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* used to endorse or promote products derived from this software
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* without specific prior written permission.
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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
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* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
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* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
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* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
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* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
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* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
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* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
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* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
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* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
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* POSSIBILITY OF SUCH DAMAGE.
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*
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****************************************************************************/
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/**
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* @file navigator_mission.cpp
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*
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* Helper class to access missions
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*
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* @author Julian Oes <julian@oes.ch>
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* @author Thomas Gubler <thomasgubler@gmail.com>
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* @author Anton Babushkin <anton.babushkin@me.com>
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* @author Ban Siesta <bansiesta@gmail.com>
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* @author Simon Wilks <simon@uaventure.com>
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* @author Andreas Antener <andreas@uaventure.com>
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* @author Sander Smeets <sander@droneslab.com>
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* @author Lorenz Meier <lorenz@px4.io>
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*/
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#include "mission.h"
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#include "navigator.h"
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#include <string.h>
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#include <drivers/drv_hrt.h>
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#include <systemlib/mavlink_log.h>
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#include <systemlib/err.h>
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#include <lib/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/mission_result.h>
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#include <drivers/drv_hrt.h>
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#include <px4_platform_common/events.h>
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using namespace time_literals;
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static constexpr int32_t DEFAULT_MISSION_CACHE_SIZE = 10;
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Mission::Mission(Navigator *navigator) :
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MissionBase(navigator, DEFAULT_MISSION_CACHE_SIZE)
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{
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}
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void
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Mission::on_inactive()
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{
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_vehicle_status_sub.update();
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if (_need_mission_save && _vehicle_status_sub.get().arming_state != vehicle_status_s::ARMING_STATE_ARMED) {
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save_mission_state();
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}
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MissionBase::on_inactive();
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}
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void
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Mission::on_activation()
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{
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_need_mission_save = true;
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MissionBase::on_activation();
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}
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bool
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Mission::isLanding()
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{
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if (get_land_start_available()) {
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static constexpr size_t max_num_next_items{1u};
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int32_t next_mission_items_index[max_num_next_items];
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size_t num_found_items;
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getNextPositionItems(_mission.land_start_index + 1, next_mission_items_index, num_found_items, max_num_next_items);
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// vehicle is currently landing if
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// mission valid, still flying, and in the landing portion of mission (past land start marker)
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bool on_landing_stage = (num_found_items > 0U) && _mission.current_seq > next_mission_items_index[0U];
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// special case: if the land start index is at a LOITER_TO_ALT WP, then we're in the landing sequence already when the
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// distance to the WP is below the loiter radius + acceptance.
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if ((num_found_items > 0U) && _mission.current_seq == next_mission_items_index[0U]
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&& _mission_item.nav_cmd == NAV_CMD_LOITER_TO_ALT) {
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const float d_current = get_distance_to_next_waypoint(_mission_item.lat, _mission_item.lon,
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_navigator->get_global_position()->lat, _navigator->get_global_position()->lon);
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// consider mission_item.loiter_radius invalid if NAN or 0, use default value in this case.
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const float mission_item_loiter_radius_abs = (PX4_ISFINITE(_mission_item.loiter_radius)
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&& fabsf(_mission_item.loiter_radius) > FLT_EPSILON) ? fabsf(_mission_item.loiter_radius) :
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_navigator->get_loiter_radius();
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on_landing_stage = d_current <= (_navigator->get_acceptance_radius() + mission_item_loiter_radius_abs);
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}
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return _navigator->get_mission_result()->valid && on_landing_stage;
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} else {
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return false;
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}
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}
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bool
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Mission::set_current_mission_index(uint16_t index)
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{
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if (index == _mission.current_seq) {
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return true;
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}
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if (_navigator->get_mission_result()->valid && (index < _mission.count)) {
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if (goToItem(index, true) != PX4_OK) {
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// Keep the old mission index (it was not updated by the interface) and report back.
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return false;
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}
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_is_current_planned_mission_item_valid = true;
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// we start from the first item so can reset the cache
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if (_mission.current_seq == 0) {
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resetItemCache();
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}
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// update mission items if already in active mission
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if (isActive()) {
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// prevent following "previous - current" line
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_navigator->reset_triplets();
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update_mission();
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set_mission_items();
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}
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// User has actively set new index, reset.
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_inactivation_index = -1;
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return true;
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}
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return false;
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}
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bool Mission::setNextMissionItem()
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{
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return (goToNextItem(true) == PX4_OK);
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}
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bool
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Mission::do_need_move_to_takeoff()
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{
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if (_vehicle_status_sub.get().vehicle_type == vehicle_status_s::VEHICLE_TYPE_ROTARY_WING
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&& _mission_item.nav_cmd == NAV_CMD_VTOL_TAKEOFF) {
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float d_current = get_distance_to_next_waypoint(_mission_item.lat, _mission_item.lon,
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_global_pos_sub.get().lat, _global_pos_sub.get().lon);
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return d_current > _navigator->get_acceptance_radius();
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}
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return false;
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}
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void Mission::setActiveMissionItems()
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{
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/* Get mission item that comes after current if available */
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static constexpr size_t max_num_next_items{2u};
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int32_t next_mission_items_index[max_num_next_items];
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size_t num_found_items;
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getNextPositionItems(_mission.current_seq + 1, next_mission_items_index, num_found_items, max_num_next_items);
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mission_item_s next_mission_items[max_num_next_items];
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const dm_item_t dataman_id = static_cast<dm_item_t>(_mission.dataman_id);
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for (size_t i = 0U; i < num_found_items; i++) {
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mission_item_s next_mission_item;
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bool success = _dataman_cache.loadWait(dataman_id, next_mission_items_index[i],
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reinterpret_cast<uint8_t *>(&next_mission_item), sizeof(next_mission_item), MAX_DATAMAN_LOAD_WAIT);
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if (success) {
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next_mission_items[i] = next_mission_item;
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} else {
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num_found_items = i;
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break;
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}
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}
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/*********************************** handle mission item *********************************************/
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WorkItemType new_work_item_type = WorkItemType::WORK_ITEM_TYPE_DEFAULT;
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position_setpoint_triplet_s *pos_sp_triplet = _navigator->get_position_setpoint_triplet();
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const position_setpoint_s current_setpoint_copy = pos_sp_triplet->current;
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if (item_contains_position(_mission_item)) {
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handleTakeoff(new_work_item_type, next_mission_items, num_found_items);
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handleLanding(new_work_item_type, next_mission_items, num_found_items);
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// TODO Precision land needs to be refactored: https://github.com/PX4/Firmware/issues/14320
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if (new_work_item_type != WorkItemType::WORK_ITEM_TYPE_PRECISION_LAND) {
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mission_item_to_position_setpoint(_mission_item, &pos_sp_triplet->current);
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}
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// Allow a rotary wing vehicle to decelerate before reaching a wp with a hold time or a timeout
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// This is done by setting the position triplet's next position's valid flag to false,
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// which makes the FlightTask disregard the next position
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// TODO: Setting the next waypoint's validity flag to handle braking / correct waypoint behavior
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// seems hacky, handle this more properly.
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const bool brake_for_hold = _vehicle_status_sub.get().vehicle_type == vehicle_status_s::VEHICLE_TYPE_ROTARY_WING
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&& (get_time_inside(_mission_item) > FLT_EPSILON || item_has_timeout(_mission_item));
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if (_mission_item.autocontinue && !brake_for_hold) {
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/* try to process next mission item */
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if (num_found_items >= 1u) {
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/* got next mission item, update setpoint triplet */
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mission_item_to_position_setpoint(next_mission_items[0u], &pos_sp_triplet->next);
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} else {
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/* next mission item is not available */
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pos_sp_triplet->next.valid = false;
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}
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} else {
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/* vehicle will be paused on current waypoint, don't set next item */
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pos_sp_triplet->next.valid = false;
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}
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} else if (item_contains_gate(_mission_item)) {
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// The mission item is a gate, let's check if the next item in the list provides
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// a position to go towards.
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if (num_found_items > 0u) {
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// We have a position, convert it to the setpoint and update setpoint triplet
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mission_item_to_position_setpoint(next_mission_items[0u], &pos_sp_triplet->current);
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}
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if (num_found_items >= 2u) {
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/* got next mission item, update setpoint triplet */
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mission_item_to_position_setpoint(next_mission_items[1u], &pos_sp_triplet->next);
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} else {
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pos_sp_triplet->next.valid = false;
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}
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} else {
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handleVtolTransition(new_work_item_type, next_mission_items, num_found_items);
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}
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// Only set the previous position item if the current one really changed
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if ((_work_item_type != WorkItemType::WORK_ITEM_TYPE_MOVE_TO_LAND) &&
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!position_setpoint_equal(&pos_sp_triplet->current, ¤t_setpoint_copy)) {
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pos_sp_triplet->previous = current_setpoint_copy;
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}
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issue_command(_mission_item);
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/* set current work item type */
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_work_item_type = new_work_item_type;
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reset_mission_item_reached();
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if (_mission_type == MissionType::MISSION_TYPE_MISSION) {
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set_mission_result();
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}
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publish_navigator_mission_item(); // for logging
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_navigator->set_position_setpoint_triplet_updated();
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}
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void Mission::handleTakeoff(WorkItemType &new_work_item_type, mission_item_s next_mission_items[],
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size_t &num_found_items)
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{
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position_setpoint_triplet_s *pos_sp_triplet = _navigator->get_position_setpoint_triplet();
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/* do climb before going to setpoint if needed and not already executing climb */
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/* in fixed-wing this whole block will be ignored and a takeoff item is always propagated */
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if (PX4_ISFINITE(_mission_init_climb_altitude_amsl) &&
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_work_item_type == WorkItemType::WORK_ITEM_TYPE_DEFAULT) {
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new_work_item_type = WorkItemType::WORK_ITEM_TYPE_CLIMB;
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/* use current mission item as next position item */
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num_found_items = 1u;
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next_mission_items[0u] = _mission_item;
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next_mission_items[0u].nav_cmd = NAV_CMD_WAYPOINT;
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mavlink_log_info(_navigator->get_mavlink_log_pub(), "Climb to %.1f meters above home\t",
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(double)(_mission_init_climb_altitude_amsl - _navigator->get_home_position()->alt));
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events::send<float>(events::ID("mission_climb_before_start"), events::Log::Info,
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"Climb to {1:.1m_v} above home", _mission_init_climb_altitude_amsl - _navigator->get_home_position()->alt);
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if (_land_detected_sub.get().landed) {
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_mission_item.nav_cmd = NAV_CMD_TAKEOFF;
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} else {
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_mission_item.nav_cmd = NAV_CMD_LOITER_TO_ALT;
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}
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_mission_item.lat = _global_pos_sub.get().lat;
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_mission_item.lon = _global_pos_sub.get().lon;
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_mission_item.yaw = NAN; // FlightTaskAuto handles yaw directly
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_mission_item.altitude = _mission_init_climb_altitude_amsl;
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_mission_item.altitude_is_relative = false;
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_mission_item.autocontinue = true;
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_mission_item.time_inside = 0.0f;
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_mission_init_climb_altitude_amsl = NAN;
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} else if (_mission_item.nav_cmd == NAV_CMD_TAKEOFF
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&& _work_item_type == WorkItemType::WORK_ITEM_TYPE_DEFAULT
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&& _vehicle_status_sub.get().vehicle_type == vehicle_status_s::VEHICLE_TYPE_ROTARY_WING) {
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/* if there is no need to do a takeoff but we have a takeoff item, treat is as waypoint */
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_mission_item.nav_cmd = NAV_CMD_WAYPOINT;
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/* ignore yaw here, otherwise it might yaw before heading_sp_update takes over */
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_mission_item.yaw = NAN;
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} else if (_mission_item.nav_cmd == NAV_CMD_VTOL_TAKEOFF
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&& _work_item_type == WorkItemType::WORK_ITEM_TYPE_DEFAULT) {
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// if the vehicle is already in fixed wing mode then the current mission item
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// will be accepted immediately and the work items will be skipped
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new_work_item_type = WorkItemType::WORK_ITEM_TYPE_CLIMB;
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/* ignore yaw here, otherwise it might yaw before heading_sp_update takes over */
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_mission_item.yaw = NAN;
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}
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/* if we just did a normal takeoff navigate to the actual waypoint now */
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if (_mission_item.nav_cmd == NAV_CMD_TAKEOFF &&
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_work_item_type == WorkItemType::WORK_ITEM_TYPE_CLIMB) {
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_mission_item.nav_cmd = NAV_CMD_WAYPOINT;
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/* ignore yaw here, otherwise it might yaw before heading_sp_update takes over */
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_mission_item.yaw = NAN;
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}
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/* if we just did a VTOL takeoff, prepare transition */
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if (_mission_item.nav_cmd == NAV_CMD_VTOL_TAKEOFF &&
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_work_item_type == WorkItemType::WORK_ITEM_TYPE_CLIMB &&
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_vehicle_status_sub.get().vehicle_type == vehicle_status_s::VEHICLE_TYPE_ROTARY_WING &&
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!_land_detected_sub.get().landed) {
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/* set yaw setpoint to heading of VTOL_TAKEOFF wp against current position */
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_mission_item.yaw = get_bearing_to_next_waypoint(
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_global_pos_sub.get().lat, _global_pos_sub.get().lon,
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_mission_item.lat, _mission_item.lon);
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_mission_item.force_heading = true;
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new_work_item_type = WorkItemType::WORK_ITEM_TYPE_ALIGN_HEADING;
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/* set position setpoint to current while aligning */
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_mission_item.lat = _global_pos_sub.get().lat;
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_mission_item.lon = _global_pos_sub.get().lon;
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}
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/* heading is aligned now, prepare transition */
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if (_mission_item.nav_cmd == NAV_CMD_VTOL_TAKEOFF &&
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_work_item_type == WorkItemType::WORK_ITEM_TYPE_ALIGN_HEADING &&
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_vehicle_status_sub.get().vehicle_type == vehicle_status_s::VEHICLE_TYPE_ROTARY_WING &&
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!_land_detected_sub.get().landed) {
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/* check if the vtol_takeoff waypoint is on top of us */
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if (do_need_move_to_takeoff()) {
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new_work_item_type = WorkItemType::WORK_ITEM_TYPE_TRANSITION_AFTER_TAKEOFF;
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}
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set_vtol_transition_item(&_mission_item, vtol_vehicle_status_s::VEHICLE_VTOL_STATE_FW);
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_mission_item.yaw = NAN;
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// keep current setpoints (FW position controller generates wp to track during transition)
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pos_sp_triplet->current.type = position_setpoint_s::SETPOINT_TYPE_POSITION;
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}
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/* takeoff completed and transitioned, move to takeoff wp as fixed wing */
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if (_mission_item.nav_cmd == NAV_CMD_VTOL_TAKEOFF
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&& _work_item_type == WorkItemType::WORK_ITEM_TYPE_TRANSITION_AFTER_TAKEOFF) {
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new_work_item_type = WorkItemType::WORK_ITEM_TYPE_DEFAULT;
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_mission_item.nav_cmd = NAV_CMD_WAYPOINT;
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_mission_item.autocontinue = true;
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_mission_item.time_inside = 0.0f;
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}
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}
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void Mission::handleVtolTransition(WorkItemType &new_work_item_type, mission_item_s next_mission_items[],
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size_t &num_found_items)
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{
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position_setpoint_triplet_s *pos_sp_triplet = _navigator->get_position_setpoint_triplet();
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/* turn towards next waypoint before MC to FW transition */
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if (_mission_item.nav_cmd == NAV_CMD_DO_VTOL_TRANSITION
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&& _work_item_type == WorkItemType::WORK_ITEM_TYPE_DEFAULT
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&& new_work_item_type == WorkItemType::WORK_ITEM_TYPE_DEFAULT
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&& _vehicle_status_sub.get().vehicle_type == vehicle_status_s::VEHICLE_TYPE_ROTARY_WING
|
|
&& !_land_detected_sub.get().landed
|
|
&& (num_found_items > 0u)) {
|
|
|
|
new_work_item_type = WorkItemType::WORK_ITEM_TYPE_ALIGN_HEADING;
|
|
|
|
set_align_mission_item(&_mission_item, &next_mission_items[0u]);
|
|
|
|
/* set position setpoint to target during the transition */
|
|
mission_item_to_position_setpoint(next_mission_items[0u], &pos_sp_triplet->current);
|
|
}
|
|
|
|
/* yaw is aligned now */
|
|
if (_work_item_type == WorkItemType::WORK_ITEM_TYPE_ALIGN_HEADING &&
|
|
new_work_item_type == WorkItemType::WORK_ITEM_TYPE_DEFAULT) {
|
|
|
|
new_work_item_type = WorkItemType::WORK_ITEM_TYPE_DEFAULT;
|
|
|
|
pos_sp_triplet->previous = pos_sp_triplet->current;
|
|
// keep current setpoints (FW position controller generates wp to track during transition)
|
|
pos_sp_triplet->current.type = position_setpoint_s::SETPOINT_TYPE_POSITION;
|
|
}
|
|
}
|
|
|
|
void
|
|
Mission::save_mission_state()
|
|
{
|
|
if (_vehicle_status_sub.get().arming_state == vehicle_status_s::ARMING_STATE_ARMED) {
|
|
// Save only while disarmed, as this is a blocking operation
|
|
_need_mission_save = true;
|
|
return;
|
|
}
|
|
|
|
_need_mission_save = false;
|
|
mission_s mission_state = {};
|
|
|
|
/* read current state */
|
|
bool success = _dataman_client.readSync(DM_KEY_MISSION_STATE, 0, reinterpret_cast<uint8_t *>(&mission_state),
|
|
sizeof(mission_s));
|
|
|
|
if (success) {
|
|
/* data read successfully, check dataman ID and items count */
|
|
if (mission_state.dataman_id == _mission.dataman_id && mission_state.count == _mission.count
|
|
&& mission_state.mission_id == _mission.mission_id) {
|
|
/* navigator may modify only sequence, write modified state only if it changed */
|
|
if (mission_state.current_seq != _mission.current_seq) {
|
|
mission_state = _mission;
|
|
|
|
success = _dataman_client.writeSync(DM_KEY_MISSION_STATE, 0, reinterpret_cast<uint8_t *>(&mission_state),
|
|
sizeof(mission_s));
|
|
|
|
if (!success) {
|
|
|
|
PX4_ERR("Can't save mission state");
|
|
}
|
|
}
|
|
}
|
|
|
|
} else {
|
|
/* invalid data, this must not happen and indicates error in mission publisher */
|
|
mission_state = _mission;
|
|
|
|
mavlink_log_critical(_navigator->get_mavlink_log_pub(), "Invalid mission state.\t");
|
|
/* EVENT
|
|
* @description No mission or storage failure
|
|
*/
|
|
events::send(events::ID("mission_invalid_mission_state"), events::Log::Error, "Invalid mission state");
|
|
|
|
/* write modified state only if changed */
|
|
success = _dataman_client.writeSync(DM_KEY_MISSION_STATE, 0, reinterpret_cast<uint8_t *>(&mission_state),
|
|
sizeof(mission_s));
|
|
|
|
if (!success) {
|
|
|
|
PX4_ERR("Can't save mission state");
|
|
}
|
|
}
|
|
}
|