mirror of
https://gitee.com/mirrors_PX4/PX4-Autopilot.git
synced 2026-10-31 02:21:36 +08:00
fw_att_control: move ecl/attitude_fw into fw_att_control module
- ecl/attitude_fw was never maintained as a standalone library - moving ecl/attitude_fw library into the fw_att_control module to ease further development
This commit is contained in:
@@ -0,0 +1,117 @@
|
||||
/****************************************************************************
|
||||
*
|
||||
* Copyright (c) 2013 Estimation and Control Library (ECL). 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 ECL 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 ecl_controller.h
|
||||
* Definition of base class for other controllers
|
||||
*
|
||||
* @author Lorenz Meier <lm@inf.ethz.ch>
|
||||
* @author Thomas Gubler <thomasgubler@gmail.com>
|
||||
*
|
||||
* Acknowledgements:
|
||||
*
|
||||
* The control design is based on a design
|
||||
* by Paul Riseborough and Andrew Tridgell, 2013,
|
||||
* which in turn is based on initial work of
|
||||
* Jonathan Challinger, 2012.
|
||||
*/
|
||||
|
||||
#pragma once
|
||||
|
||||
#include <drivers/drv_hrt.h>
|
||||
#include <px4_log.h>
|
||||
|
||||
struct ECL_ControlData {
|
||||
float roll;
|
||||
float pitch;
|
||||
float yaw;
|
||||
float body_x_rate;
|
||||
float body_y_rate;
|
||||
float body_z_rate;
|
||||
float roll_setpoint;
|
||||
float pitch_setpoint;
|
||||
float yaw_setpoint;
|
||||
float roll_rate_setpoint;
|
||||
float pitch_rate_setpoint;
|
||||
float yaw_rate_setpoint;
|
||||
float airspeed_min;
|
||||
float airspeed_max;
|
||||
float airspeed;
|
||||
float scaler;
|
||||
float groundspeed;
|
||||
float groundspeed_scaler;
|
||||
bool lock_integrator;
|
||||
};
|
||||
|
||||
class ECL_Controller
|
||||
{
|
||||
public:
|
||||
ECL_Controller();
|
||||
virtual ~ECL_Controller() = default;
|
||||
|
||||
virtual float control_attitude(const struct ECL_ControlData &ctl_data) = 0;
|
||||
virtual float control_euler_rate(const struct ECL_ControlData &ctl_data) = 0;
|
||||
virtual float control_bodyrate(const struct ECL_ControlData &ctl_data) = 0;
|
||||
|
||||
/* Setters */
|
||||
void set_time_constant(float time_constant);
|
||||
void set_k_p(float k_p);
|
||||
void set_k_i(float k_i);
|
||||
void set_k_ff(float k_ff);
|
||||
void set_integrator_max(float max);
|
||||
void set_max_rate(float max_rate);
|
||||
void set_bodyrate_setpoint(float rate);
|
||||
|
||||
/* Getters */
|
||||
float get_rate_error();
|
||||
float get_desired_rate();
|
||||
float get_desired_bodyrate();
|
||||
float get_integrator();
|
||||
|
||||
void reset_integrator();
|
||||
|
||||
protected:
|
||||
uint64_t _last_run;
|
||||
float _tc;
|
||||
float _k_p;
|
||||
float _k_i;
|
||||
float _k_ff;
|
||||
float _integrator_max;
|
||||
float _max_rate;
|
||||
float _last_output;
|
||||
float _integrator;
|
||||
float _rate_error;
|
||||
float _rate_setpoint;
|
||||
float _bodyrate_setpoint;
|
||||
float constrain_airspeed(float airspeed, float minspeed, float maxspeed);
|
||||
};
|
||||
Reference in New Issue
Block a user