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FlightTasks: added FlightTaskManual as replacement for the current stick based position controlled flight
it's a draft and only works for velocity setpoints oriented in NED frame yet # Conflicts: # src/lib/FlightTasks/tasks/FlightTaskOrbit.cpp
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@ -34,6 +34,7 @@ px4_add_module(
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MODULE lib__flight_tasks
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SRCS
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FlightTask.h
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tasks/FlightTaskManual.cpp
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tasks/FlightTaskOrbit.cpp
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DEPENDS
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platforms__common
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@ -42,6 +42,7 @@
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#pragma once
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#include "tasks/FlightTask.hpp"
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#include "tasks/FlightTaskManual.hpp"
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#include "tasks/FlightTaskOrbit.hpp"
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class FlightTasks
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@ -114,7 +115,12 @@ public:
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* Get result of the task execution
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* @return pointer to the setpoint for the position controller
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*/
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const vehicle_local_position_setpoint_s *get_position_setpoint() const { return Orbit.get_position_setpoint(); };
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const vehicle_local_position_setpoint_s *get_position_setpoint() const
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{
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//if (is_any_task_active()) {
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return _tasks[_current_task]->get_position_setpoint();
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//}
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};
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/**
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* Check if any task is active
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@ -123,10 +129,11 @@ public:
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bool is_any_task_active() const { return _current_task > -1 && _current_task < _task_count; };
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private:
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static const int _task_count = 1;
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int _current_task = -1;
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FlightTaskManual Manual;
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FlightTaskOrbit Orbit;
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FlightTask *_tasks[_task_count] = {&Orbit};
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static const int _task_count = 2;
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FlightTask *_tasks[_task_count] = {&Manual, &Orbit};
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};
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@ -32,7 +32,7 @@
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****************************************************************************/
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/**
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* @file FlightTask.h
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* @file FlightTask.hpp
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*
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* Abstract base class for different advanced flight tasks like orbit, follow me, ...
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*
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@ -67,7 +67,7 @@ public:
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* Call once on the event of switching away from the task
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* @return 0 on success, >0 on error
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*/
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virtual int disable() = 0;
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virtual int disable() { return 0; };
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/**
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* To be called regularly in the control loop cycle to execute the task
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@ -167,10 +167,10 @@ private:
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void _evaluate_sticks()
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{
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if (_manual_control_setpoint != NULL && hrt_elapsed_time(&_manual_control_setpoint->timestamp) < _timeout) {
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_sticks(0) = _manual_control_setpoint->y; /* "roll" [-1,1] */
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_sticks(1) = _manual_control_setpoint->x; /* "pitch" [-1,1] */
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_sticks(2) = _manual_control_setpoint->r; /* "yaw" [-1,1] */
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_sticks(3) = (_manual_control_setpoint->z - 0.5f) * 2.f; /* "thrust" resacaled from [0,1] to [-1,1] */
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_sticks(0) = _manual_control_setpoint->x; /* NED x, "pitch" [-1,1] */
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_sticks(1) = _manual_control_setpoint->y; /* NED y, "roll" [-1,1] */
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_sticks(2) = (_manual_control_setpoint->z - 0.5f) * 2.f; /* NED z, "thrust" resacaled from [0,1] to [-1,1] */
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_sticks(3) = _manual_control_setpoint->r; /* "yaw" [-1,1] */
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} else {
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_sticks = matrix::Vector<float, 4>(); /* default is all zero */
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127
src/lib/FlightTasks/tasks/FlightTaskManual.hpp
Normal file
127
src/lib/FlightTasks/tasks/FlightTaskManual.hpp
Normal file
@ -0,0 +1,127 @@
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/****************************************************************************
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*
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* Copyright (c) 2017 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 FlightTaskManual.hpp
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*
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* Flight task for the normal, legacy, manual position controlled flight
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* where stick inputs map basically to the velocity setpoint
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*
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* @author Matthias Grob <maetugr@gmail.com>
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*/
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#pragma once
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#include "FlightTask.hpp"
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class FlightTaskManual : public FlightTask
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{
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public:
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FlightTaskManual() :
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_xy_vel_man_expo(nullptr, "MPC_XY_MAN_EXPO"),
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_z_vel_man_expo(nullptr, "MPC_Z_MAN_EXPO"),
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_hold_dz(nullptr, "MPC_HOLD_DZ"),
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_velocity_hor_manual(nullptr, "MPC_VEL_MANUAL"),
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_z_vel_max_up(nullptr, "MPC_Z_VEL_MAX_UP"),
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_z_vel_max_down(nullptr, "MPC_Z_VEL_MAX_DN")
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{};
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virtual ~FlightTaskManual() {};
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/**
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* Call once on the event where you switch to the task
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* @return 0 on success, >0 on error otherwise
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*/
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virtual int activate()
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{
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FlightTask::activate();
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return 0;
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};
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/**
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* Call once on the event of switching away from the task
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* @return 0 on success, >0 on error otherwise
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*/
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virtual int disable()
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{
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FlightTask::disable();
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return 0;
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};
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/**
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* Call regularly in the control loop cycle to execute the task
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* @return 0 on success, >0 on error otherwise
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*/
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virtual int update()
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{
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FlightTask::update();
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matrix::Vector3f man_vel_sp;
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man_vel_sp(0) = math::expo_deadzone(_sticks(0), _xy_vel_man_expo.get(), _hold_dz.get());
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man_vel_sp(1) = math::expo_deadzone(_sticks(1), _xy_vel_man_expo.get(), _hold_dz.get());
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man_vel_sp(2) = -math::expo_deadzone(_sticks(2), _z_vel_man_expo.get(), _hold_dz.get());
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const float man_vel_hor_length = matrix::Vector2f(man_vel_sp.data()).length();
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/* saturate such that magnitude is never larger than 1 */
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if (man_vel_hor_length > 1.0f) {
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man_vel_sp(0) /= man_vel_hor_length;
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man_vel_sp(1) /= man_vel_hor_length;
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}
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/* prepare yaw to rotate into NED frame */
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float yaw_input_fame = 0;
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//float yaw_input_fame = _yaw;
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/* setpoint in NED frame */
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man_vel_sp = matrix::Dcmf(matrix::Eulerf(0.0f, 0.0f, yaw_input_fame)) * man_vel_sp;
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/* scale smaller than unit length vector to maximal manual speed (m/s) */
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matrix::Vector3f vel_scale(_velocity_hor_manual.get(),
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_velocity_hor_manual.get(),
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(man_vel_sp(2) > 0.0f) ? _z_vel_max_down.get() : _z_vel_max_up.get());
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man_vel_sp = man_vel_sp.emult(vel_scale);
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_set_position_setpoint(matrix::Vector3f(NAN, NAN, NAN));
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_set_velocity_setpoint(man_vel_sp);
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return 0;
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};
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private:
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control::BlockParamFloat _xy_vel_man_expo; /**< ratio of exponential curve for stick input in xy direction pos mode */
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control::BlockParamFloat _z_vel_man_expo; /**< ratio of exponential curve for stick input in xy direction pos mode */
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control::BlockParamFloat _hold_dz; /**< deadzone around the center for the sticks when flying in position mode */
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control::BlockParamFloat _velocity_hor_manual; /**< target velocity in manual controlled mode at full speed */
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control::BlockParamFloat _z_vel_max_up; /**< maximal vertical velocity when flying upwards with the stick */
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control::BlockParamFloat _z_vel_max_down; /**< maximal vertical velocity when flying downwards with the stick */
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};
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@ -32,7 +32,7 @@
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****************************************************************************/
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/**
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* @file FlightTaskOrbit.h
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* @file FlightTaskOrbit.hpp
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*
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* Flight task for orbiting in a circle around a target position
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*
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@ -63,7 +63,11 @@ public:
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* Call once on the event of switching away from the task
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* @return 0 on success, >0 on error otherwise
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*/
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virtual int disable() { return 0; };
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virtual int disable()
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{
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FlightTask::disable();
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return 0;
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};
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/**
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* Call regularly in the control loop cycle to execute the task
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@ -73,11 +77,11 @@ public:
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{
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FlightTask::update();
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r += _sticks(1) * _deltatime;
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r += _sticks(0) * _deltatime;
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r = math::constrain(r, 0.5f, 4.f);
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v -= _sticks(0) * _deltatime;
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v -= _sticks(1) * _deltatime;
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v = math::constrain(v, -7.f, 7.f);
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altitude += _sticks(3) * _deltatime;
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altitude += _sticks(2) * _deltatime;
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altitude = math::constrain(altitude, 2.f, 5.f);
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matrix::Vector2<float> target_to_position = matrix::Vector2f(_position.data()) - matrix::Vector2f();
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