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
This commit is contained in:
Matthias Grob 2017-08-14 15:16:05 +02:00 committed by Beat Küng
parent a9d0990bb8
commit 28f4d18062
5 changed files with 153 additions and 14 deletions

View File

@ -34,6 +34,7 @@ px4_add_module(
MODULE lib__flight_tasks
SRCS
FlightTask.h
tasks/FlightTaskManual.cpp
tasks/FlightTaskOrbit.cpp
DEPENDS
platforms__common

View File

@ -42,6 +42,7 @@
#pragma once
#include "tasks/FlightTask.hpp"
#include "tasks/FlightTaskManual.hpp"
#include "tasks/FlightTaskOrbit.hpp"
class FlightTasks
@ -114,7 +115,12 @@ public:
* Get result of the task execution
* @return pointer to the setpoint for the position controller
*/
const vehicle_local_position_setpoint_s *get_position_setpoint() const { return Orbit.get_position_setpoint(); };
const vehicle_local_position_setpoint_s *get_position_setpoint() const
{
//if (is_any_task_active()) {
return _tasks[_current_task]->get_position_setpoint();
//}
};
/**
* Check if any task is active
@ -123,10 +129,11 @@ public:
bool is_any_task_active() const { return _current_task > -1 && _current_task < _task_count; };
private:
static const int _task_count = 1;
int _current_task = -1;
FlightTaskManual Manual;
FlightTaskOrbit Orbit;
FlightTask *_tasks[_task_count] = {&Orbit};
static const int _task_count = 2;
FlightTask *_tasks[_task_count] = {&Manual, &Orbit};
};

View File

@ -32,7 +32,7 @@
****************************************************************************/
/**
* @file FlightTask.h
* @file FlightTask.hpp
*
* Abstract base class for different advanced flight tasks like orbit, follow me, ...
*
@ -67,7 +67,7 @@ public:
* Call once on the event of switching away from the task
* @return 0 on success, >0 on error
*/
virtual int disable() = 0;
virtual int disable() { return 0; };
/**
* To be called regularly in the control loop cycle to execute the task
@ -167,10 +167,10 @@ private:
void _evaluate_sticks()
{
if (_manual_control_setpoint != NULL && hrt_elapsed_time(&_manual_control_setpoint->timestamp) < _timeout) {
_sticks(0) = _manual_control_setpoint->y; /* "roll" [-1,1] */
_sticks(1) = _manual_control_setpoint->x; /* "pitch" [-1,1] */
_sticks(2) = _manual_control_setpoint->r; /* "yaw" [-1,1] */
_sticks(3) = (_manual_control_setpoint->z - 0.5f) * 2.f; /* "thrust" resacaled from [0,1] to [-1,1] */
_sticks(0) = _manual_control_setpoint->x; /* NED x, "pitch" [-1,1] */
_sticks(1) = _manual_control_setpoint->y; /* NED y, "roll" [-1,1] */
_sticks(2) = (_manual_control_setpoint->z - 0.5f) * 2.f; /* NED z, "thrust" resacaled from [0,1] to [-1,1] */
_sticks(3) = _manual_control_setpoint->r; /* "yaw" [-1,1] */
} else {
_sticks = matrix::Vector<float, 4>(); /* default is all zero */

View File

@ -0,0 +1,127 @@
/****************************************************************************
*
* Copyright (c) 2017 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 FlightTaskManual.hpp
*
* Flight task for the normal, legacy, manual position controlled flight
* where stick inputs map basically to the velocity setpoint
*
* @author Matthias Grob <maetugr@gmail.com>
*/
#pragma once
#include "FlightTask.hpp"
class FlightTaskManual : public FlightTask
{
public:
FlightTaskManual() :
_xy_vel_man_expo(nullptr, "MPC_XY_MAN_EXPO"),
_z_vel_man_expo(nullptr, "MPC_Z_MAN_EXPO"),
_hold_dz(nullptr, "MPC_HOLD_DZ"),
_velocity_hor_manual(nullptr, "MPC_VEL_MANUAL"),
_z_vel_max_up(nullptr, "MPC_Z_VEL_MAX_UP"),
_z_vel_max_down(nullptr, "MPC_Z_VEL_MAX_DN")
{};
virtual ~FlightTaskManual() {};
/**
* Call once on the event where you switch to the task
* @return 0 on success, >0 on error otherwise
*/
virtual int activate()
{
FlightTask::activate();
return 0;
};
/**
* Call once on the event of switching away from the task
* @return 0 on success, >0 on error otherwise
*/
virtual int disable()
{
FlightTask::disable();
return 0;
};
/**
* Call regularly in the control loop cycle to execute the task
* @return 0 on success, >0 on error otherwise
*/
virtual int update()
{
FlightTask::update();
matrix::Vector3f man_vel_sp;
man_vel_sp(0) = math::expo_deadzone(_sticks(0), _xy_vel_man_expo.get(), _hold_dz.get());
man_vel_sp(1) = math::expo_deadzone(_sticks(1), _xy_vel_man_expo.get(), _hold_dz.get());
man_vel_sp(2) = -math::expo_deadzone(_sticks(2), _z_vel_man_expo.get(), _hold_dz.get());
const float man_vel_hor_length = matrix::Vector2f(man_vel_sp.data()).length();
/* saturate such that magnitude is never larger than 1 */
if (man_vel_hor_length > 1.0f) {
man_vel_sp(0) /= man_vel_hor_length;
man_vel_sp(1) /= man_vel_hor_length;
}
/* prepare yaw to rotate into NED frame */
float yaw_input_fame = 0;
//float yaw_input_fame = _yaw;
/* setpoint in NED frame */
man_vel_sp = matrix::Dcmf(matrix::Eulerf(0.0f, 0.0f, yaw_input_fame)) * man_vel_sp;
/* scale smaller than unit length vector to maximal manual speed (m/s) */
matrix::Vector3f vel_scale(_velocity_hor_manual.get(),
_velocity_hor_manual.get(),
(man_vel_sp(2) > 0.0f) ? _z_vel_max_down.get() : _z_vel_max_up.get());
man_vel_sp = man_vel_sp.emult(vel_scale);
_set_position_setpoint(matrix::Vector3f(NAN, NAN, NAN));
_set_velocity_setpoint(man_vel_sp);
return 0;
};
private:
control::BlockParamFloat _xy_vel_man_expo; /**< ratio of exponential curve for stick input in xy direction pos mode */
control::BlockParamFloat _z_vel_man_expo; /**< ratio of exponential curve for stick input in xy direction pos mode */
control::BlockParamFloat _hold_dz; /**< deadzone around the center for the sticks when flying in position mode */
control::BlockParamFloat _velocity_hor_manual; /**< target velocity in manual controlled mode at full speed */
control::BlockParamFloat _z_vel_max_up; /**< maximal vertical velocity when flying upwards with the stick */
control::BlockParamFloat _z_vel_max_down; /**< maximal vertical velocity when flying downwards with the stick */
};

View File

@ -32,7 +32,7 @@
****************************************************************************/
/**
* @file FlightTaskOrbit.h
* @file FlightTaskOrbit.hpp
*
* Flight task for orbiting in a circle around a target position
*
@ -63,7 +63,11 @@ public:
* Call once on the event of switching away from the task
* @return 0 on success, >0 on error otherwise
*/
virtual int disable() { return 0; };
virtual int disable()
{
FlightTask::disable();
return 0;
};
/**
* Call regularly in the control loop cycle to execute the task
@ -73,11 +77,11 @@ public:
{
FlightTask::update();
r += _sticks(1) * _deltatime;
r += _sticks(0) * _deltatime;
r = math::constrain(r, 0.5f, 4.f);
v -= _sticks(0) * _deltatime;
v -= _sticks(1) * _deltatime;
v = math::constrain(v, -7.f, 7.f);
altitude += _sticks(3) * _deltatime;
altitude += _sticks(2) * _deltatime;
altitude = math::constrain(altitude, 2.f, 5.f);
matrix::Vector2<float> target_to_position = matrix::Vector2f(_position.data()) - matrix::Vector2f();