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flight_task: added dead-reckon rtl flight task implementation
This commit is contained in:
@@ -48,6 +48,7 @@ list(APPEND flight_tasks_all
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ManualAltitudeSmoothVel
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ManualPosition
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Transition
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ReturnDeadReckoning
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)
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if(NOT px4_constrained_flash_build)
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@@ -255,8 +255,12 @@ void FlightModeManager::start_flight_task()
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// Dead-Reckoning Return
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if (nav_state_rtl_dr) {
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found_some_task = true;
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PX4_INFO("Going into Dead-Reckoning Return mode");
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task_failure = false;
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FlightTaskError error = switchTask(FlightTaskIndex::ReturnDeadReckoning);
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task_failure = (error != FlightTaskError::NoError);
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matching_task_running = matching_task_running && !task_failure;
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}
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// Emergency descend
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@@ -0,0 +1,39 @@
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############################################################################
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#
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# Copyright (c) 2024 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.
|
||||
# 2. Redistributions in binary form must reproduce the above copyright
|
||||
# notice, this list of conditions and the following disclaimer in
|
||||
# the documentation and/or other materials provided with the
|
||||
# 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
|
||||
# without specific prior written permission.
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||||
#
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||||
# THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
|
||||
# "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
|
||||
# LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
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||||
# FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
|
||||
# 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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px4_add_library(FlightTaskReturnDeadReckoning
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FlightTaskReturnDeadReckoning.cpp
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)
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target_link_libraries(FlightTaskReturnDeadReckoning PUBLIC FlightTask)
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target_include_directories(FlightTaskReturnDeadReckoning PUBLIC ${CMAKE_CURRENT_SOURCE_DIR})
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+289
@@ -0,0 +1,289 @@
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/****************************************************************************
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*
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* Copyright (c) 2019-2025 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
|
||||
* are met:
|
||||
*
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||||
* 1. Redistributions of source code must retain the above copyright
|
||||
* notice, this list of conditions and the following disclaimer.
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||||
* 2. Redistributions in binary form must reproduce the above copyright
|
||||
* notice, this list of conditions and the following disclaimer in
|
||||
* 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
|
||||
* 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,
|
||||
* 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 FlightTaskReturnDeadReckoning.cpp
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*/
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#include "FlightTaskReturnDeadReckoning.hpp"
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bool FlightTaskReturnDeadReckoning::activate(const trajectory_setpoint_s &last_setpoint)
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{
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PX4_INFO("FlightTaskReturnDeadReckoning::activate");
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if (!FlightTask::activate(last_setpoint)) {
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PX4_ERR("Failed to activate task");
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return false;
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}
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_updateSubscriptions();
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_state = State::INIT;
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if (!_updateBearingToHome()) {
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PX4_ERR("Failed to compute bearing to home");
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return false;
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}
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if (!_computeReturnParameters()) {
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PX4_ERR("Failed to compute return parameters");
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return false;
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}
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if (!_initializeSmoothers()) {
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PX4_ERR("Failed to initialize smoothers");
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return false;
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}
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return true;
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}
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bool FlightTaskReturnDeadReckoning::update()
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{
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if (!FlightTask::update()) {
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return false;
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}
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_updateSubscriptions();
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if (_isGlobalPositionValid()) {
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// Update the bearing to home
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if (!_updateBearingToHome()) {
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PX4_ERR("Failed to compute bearing to home");
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return false;
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}
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}
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_updateState();
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_updateSetpoints();
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return true;
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}
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void FlightTaskReturnDeadReckoning::_updateState()
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{
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switch (_state) {
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case State::INIT:
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if (_isAboveReturnAltitude()) {
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_state = State::RETURN;
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PX4_INFO("Returning to home position at %.2fm (MSL) with bearing %.2f deg",
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(double) _rtl_alt, (double) math::degrees(_bearing_to_home));
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} else {
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_state = State::ASCENT;
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PX4_INFO("Ascending to return altitude %.2fm (MSL) with bearing %.2f deg",
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(double) _rtl_alt, (double) math::degrees(_bearing_to_home));
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}
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break;
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case State::ASCENT:
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if (_isAboveReturnAltitude()) {
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_state = State::RETURN;
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PX4_INFO("Returning to home position at %.2fm (MSL) with bearing %.2f deg",
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(double) _rtl_alt, (double) math::degrees(_bearing_to_home));
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}
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break;
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case State::RETURN:
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if (_isWithinHomePositionRadius()) {
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_state = State::HOLD;
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PX4_INFO("Holding altitude at %.2fm (MSL) over home position", (double) _rtl_alt);
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}
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break;
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case State::HOLD:
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break;
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default:
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PX4_ERR("Unknown state");
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return;
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}
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}
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void FlightTaskReturnDeadReckoning::_updateSetpoints()
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{
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switch (_state) {
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case State::INIT:
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_slew_rate_acceleration_x.update(0.0f, _deltatime);
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_slew_rate_acceleration_y.update(0.0f, _deltatime);
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_slew_rate_velocity_z.update(0.0f, _deltatime);
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// Hold current altitude
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_velocity_setpoint(2) = _slew_rate_velocity_z.getState();
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break;
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case State::ASCENT:
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_slew_rate_acceleration_x.update(0.0f, _deltatime);
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_slew_rate_acceleration_y.update(0.0f, _deltatime);
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_slew_rate_velocity_z.update(-_param_mpc_z_v_auto_up.get(), _deltatime);
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// Ascent until reaching the return altitude
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_velocity_setpoint(2) = _slew_rate_velocity_z.getState();
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break;
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case State::RETURN:
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_slew_rate_acceleration_x.update(_rtl_acc*cosf(_bearing_to_home), _deltatime);
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_slew_rate_acceleration_y.update(_rtl_acc*sinf(_bearing_to_home), _deltatime);
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_slew_rate_velocity_z.update(0.0f, _deltatime);
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// Stay at the return altitude
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_position_setpoint(2) = -(_rtl_alt - (float) _home_position(2));
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break;
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case State::HOLD:
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_slew_rate_acceleration_x.update(0.0f, _deltatime);
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_slew_rate_acceleration_y.update(0.0f, _deltatime);
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_slew_rate_velocity_z.update(0.0f, _deltatime);
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// Stay at the return altitude
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_position_setpoint(2) = -(_rtl_alt - (float) _home_position(2));
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break;
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default:
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PX4_ERR("Unknown state");
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return;
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};
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// Heading setpoint
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_heading_smoothing.update(_bearing_to_home, _deltatime);
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_yaw_setpoint = _heading_smoothing.getSmoothedHeading();
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_yawspeed_setpoint = _heading_smoothing.getSmoothedHeadingRate();
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// Acceleration setpoint
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_acceleration_setpoint.xy() = matrix::Vector2f(
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_slew_rate_acceleration_x.getState(),
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_slew_rate_acceleration_y.getState()
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);
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return;
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}
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void FlightTaskReturnDeadReckoning::_updateSubscriptions()
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{
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_sub_vehicle_global_position.update();
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}
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bool FlightTaskReturnDeadReckoning::_readHomePosition(matrix::Vector3d &home_position)
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{
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home_position.setNaN();
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if (_sub_home_position.get().valid_hpos && _sub_home_position.get().valid_alt) {
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home_position(0) = _sub_home_position.get().lat;
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home_position(1) = _sub_home_position.get().lon;
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home_position(2) = (double) _sub_home_position.get().alt;
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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 FlightTaskReturnDeadReckoning::_readGlobalPosition(matrix::Vector3d &global_position)
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{
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global_position.setNaN();
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global_position(0) = _sub_vehicle_global_position.get().lat;
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global_position(1) = _sub_vehicle_global_position.get().lon;
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global_position(2) = (double) _sub_vehicle_global_position.get().alt;
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return true;
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}
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bool FlightTaskReturnDeadReckoning::_updateBearingToHome()
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{
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if (_readGlobalPosition(_start_vehicle_global_position) && _readHomePosition(_home_position)) {
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_bearing_to_home = _computeBearing(_start_vehicle_global_position, _home_position);
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}
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return !isnanf(_bearing_to_home);
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}
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float FlightTaskReturnDeadReckoning::_computeBearing(const matrix::Vector3d &_global_position_start, const matrix::Vector3d &_global_position_end)
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{
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float bearing = NAN;
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if (_global_position_start.isAllFinite() && _global_position_end.isAllFinite()) {
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bearing = get_bearing_to_next_waypoint(_global_position_start(0), _global_position_start(1),
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_global_position_end(0), _global_position_end(1));
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}
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return bearing;
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}
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bool FlightTaskReturnDeadReckoning::_computeReturnParameters()
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{
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_rtl_alt = _param_rtl_return_alt.get();
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_rtl_alt = math::max((float) _start_vehicle_global_position(2), (float) _home_position(2) + _rtl_alt);
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_rtl_acc = _param_mpc_acc_hor_max.get();
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return true;
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}
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bool FlightTaskReturnDeadReckoning::_initializeSmoothers()
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{
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// Initialize the heading smoother
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_heading_smoothing.setMaxHeadingRate(_param_mpc_yawrauto_max.get());
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_heading_smoothing.setMaxHeadingAccel(_param_mpc_yawrauto_acc.get());
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_heading_smoothing.reset(_sub_vehicle_local_position.get().heading, 0.0f);
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// Initialize the position smoother
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_slew_rate_velocity_z.setSlewRate(_param_mpc_acc_up_max.get());
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_slew_rate_velocity_z.setForcedValue((float) _sub_vehicle_local_position.get().vz);
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// Initialize the acceleration smoothers
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_slew_rate_acceleration_x.setSlewRate(_param_mpc_jerk_auto.get());
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_slew_rate_acceleration_x.setForcedValue(_sub_vehicle_local_position.get().ax);
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_slew_rate_acceleration_y.setSlewRate(_param_mpc_jerk_auto.get());
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_slew_rate_acceleration_y.setForcedValue(_sub_vehicle_local_position.get().ay);
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return true;
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}
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bool FlightTaskReturnDeadReckoning::_isAboveReturnAltitude() const
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{
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float current_alt =_sub_vehicle_global_position.get().alt;
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float target_alt = _rtl_alt - _param_nav_mc_alt_rad.get();
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return current_alt > target_alt;
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}
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bool FlightTaskReturnDeadReckoning::_isWithinHomePositionRadius()
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{
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if (_isGlobalPositionValid()) {
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_readGlobalPosition(_start_vehicle_global_position);
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return get_distance_to_next_waypoint(
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_start_vehicle_global_position(0), _start_vehicle_global_position(1),
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_home_position(0), _home_position(1)) < _param_nav_acc_rad.get();
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}
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return false;
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}
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+144
@@ -0,0 +1,144 @@
|
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/****************************************************************************
|
||||
*
|
||||
* Copyright (c) 2019-2025 PX4 Development Team. All rights reserved.
|
||||
*
|
||||
* Redistribution and use in source and binary forms, with or without
|
||||
* modification, are permitted provided that the following conditions
|
||||
* are met:
|
||||
*
|
||||
* 1. Redistributions of source code must retain the above copyright
|
||||
* notice, this list of conditions and the following disclaimer.
|
||||
* 2. Redistributions in binary form must reproduce the above copyright
|
||||
* notice, this list of conditions and the following disclaimer in
|
||||
* the documentation and/or other materials provided with the
|
||||
* distribution.
|
||||
* 3. Neither the name PX4 nor the names of its contributors may be
|
||||
* used to endorse or promote products derived from this software
|
||||
* without specific prior written permission.
|
||||
*
|
||||
* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
|
||||
* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
|
||||
* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
|
||||
* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
|
||||
* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
|
||||
* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
|
||||
* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
|
||||
* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
|
||||
* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
|
||||
* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
|
||||
* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
|
||||
* POSSIBILITY OF SUCH DAMAGE.
|
||||
*
|
||||
****************************************************************************/
|
||||
|
||||
/**
|
||||
* @file FlightTaskReturnDeadReckoning.hpp
|
||||
*/
|
||||
|
||||
#pragma once
|
||||
|
||||
#include "FlightTask.hpp"
|
||||
#include <uORB/Subscription.hpp>
|
||||
#include <uORB/topics/vehicle_global_position.h>
|
||||
#include <lib/motion_planning/HeadingSmoothing.hpp>
|
||||
#include <lib/motion_planning/PositionSmoothing.hpp>
|
||||
#include <lib/slew_rate/SlewRate.hpp>
|
||||
|
||||
class FlightTaskReturnDeadReckoning : public FlightTask
|
||||
{
|
||||
public:
|
||||
FlightTaskReturnDeadReckoning() = default;
|
||||
virtual ~FlightTaskReturnDeadReckoning() = default;
|
||||
|
||||
bool update() override;
|
||||
bool activate(const trajectory_setpoint_s &last_setpoint) override;
|
||||
|
||||
private:
|
||||
uORB::SubscriptionData<vehicle_global_position_s> _sub_vehicle_global_position{ORB_ID(vehicle_global_position)};
|
||||
|
||||
void _updateState();
|
||||
|
||||
void _updateSetpoints();
|
||||
|
||||
|
||||
/**
|
||||
* Initialize home position
|
||||
* @return true on success, false on error
|
||||
*/
|
||||
bool _readHomePosition(matrix::Vector3d &home_position);
|
||||
|
||||
/**
|
||||
* Reads current GNSS position
|
||||
* @return true on success, false on error
|
||||
*/
|
||||
bool _readGlobalPosition(matrix::Vector3d &global_position);
|
||||
|
||||
|
||||
bool _updateBearingToHome();
|
||||
|
||||
/**
|
||||
* Compute bearing to home position
|
||||
* @return true on success, false on error
|
||||
*/
|
||||
float _computeBearing(const matrix::Vector3d &_global_position_start,
|
||||
const matrix::Vector3d &_global_position_end);
|
||||
|
||||
/**
|
||||
* Computes return altitude velocity
|
||||
* @return true on success, false on error
|
||||
*/
|
||||
bool _computeReturnParameters();
|
||||
|
||||
/**
|
||||
* Initialize the trajectory setpoint smoothers
|
||||
* @return true on success, false on error
|
||||
*/
|
||||
bool _initializeSmoothers();
|
||||
|
||||
void _updateSubscriptions();
|
||||
|
||||
bool _isGlobalPositionValid() const
|
||||
{
|
||||
return _sub_vehicle_global_position.get().lat_lon_valid && _sub_vehicle_global_position.get().alt_valid;
|
||||
}
|
||||
|
||||
bool _isAboveReturnAltitude() const;
|
||||
|
||||
bool _isWithinHomePositionRadius();
|
||||
|
||||
|
||||
// Variable storing the home position
|
||||
matrix::Vector3d _home_position; /**< Stores home position */
|
||||
matrix::Vector3d _start_vehicle_global_position; /**< Stores vehicle last known GNSS position */
|
||||
float _bearing_to_home{0.0f}; /**< Stores bearing between home and last GNSS position */
|
||||
|
||||
HeadingSmoothing _heading_smoothing; /**< Smoother for heading */
|
||||
SlewRate<float> _slew_rate_acceleration_x{0.0f}; /**< Slew rate for x-acceleration setpoint */
|
||||
SlewRate<float> _slew_rate_acceleration_y{0.0f}; /**< Slew rate for y-acceleration setpoint */
|
||||
SlewRate<float> _slew_rate_velocity_z{0.0f}; /**< Smoother for vertical velocity */
|
||||
|
||||
|
||||
float _rtl_alt{0.0f}; /**< Return altitude */
|
||||
float _rtl_acc{0.0f}; /**< Return acceleration */
|
||||
|
||||
enum class State {
|
||||
UNKNOWN = 0,
|
||||
INIT,
|
||||
ASCENT,
|
||||
RETURN,
|
||||
HOLD
|
||||
};
|
||||
State _state{State::UNKNOWN}; /**< State machine for flight task */
|
||||
|
||||
DEFINE_PARAMETERS_CUSTOM_PARENT(FlightTask,
|
||||
(ParamFloat<px4::params::MPC_ACC_HOR_MAX>) _param_mpc_acc_hor_max,
|
||||
(ParamFloat<px4::params::RTL_RETURN_ALT>) _param_rtl_return_alt, //< RTL altitude
|
||||
(ParamFloat<px4::params::MPC_YAWRAUTO_MAX>) _param_mpc_yawrauto_max, //< max yaw rate in auto modes
|
||||
(ParamFloat<px4::params::MPC_YAWRAUTO_ACC>) _param_mpc_yawrauto_acc, //< max yaw acceleration in auto modes
|
||||
(ParamFloat<px4::params::MPC_JERK_AUTO>) _param_mpc_jerk_auto, //< maximum jerk in auto modes
|
||||
(ParamFloat<px4::params::MPC_Z_V_AUTO_UP>) _param_mpc_z_v_auto_up, //< max vertical velocity up
|
||||
(ParamFloat<px4::params::MPC_ACC_UP_MAX>) _param_mpc_acc_up_max, //< max vertical acceleration up
|
||||
(ParamFloat<px4::params::NAV_MC_ALT_RAD>) _param_nav_mc_alt_rad, //< max vertical error
|
||||
(ParamFloat<px4::params::NAV_ACC_RAD>) _param_nav_acc_rad //< max horizontal error
|
||||
);
|
||||
};
|
||||
Reference in New Issue
Block a user