mirror of
https://gitee.com/mirrors_PX4/PX4-Autopilot.git
synced 2026-06-26 07:10:35 +08:00
Initial import
This commit is contained in:
@@ -0,0 +1,140 @@
|
||||
/****************************************************************************
|
||||
*
|
||||
* 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.cpp
|
||||
* 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.
|
||||
*/
|
||||
|
||||
#include "ecl_controller.h"
|
||||
|
||||
#include <stdio.h>
|
||||
#include <mathlib/mathlib.h>
|
||||
|
||||
ECL_Controller::ECL_Controller(const char *name) :
|
||||
_last_run(0),
|
||||
_tc(0.1f),
|
||||
_k_p(0.0f),
|
||||
_k_i(0.0f),
|
||||
_k_ff(0.0f),
|
||||
_integrator_max(0.0f),
|
||||
_max_rate(0.0f),
|
||||
_last_output(0.0f),
|
||||
_integrator(0.0f),
|
||||
_rate_error(0.0f),
|
||||
_rate_setpoint(0.0f),
|
||||
_bodyrate_setpoint(0.0f),
|
||||
_perf_name()
|
||||
{
|
||||
/* Init performance counter */
|
||||
snprintf(_perf_name, sizeof(_perf_name), "fw att control %s nonfinite input", name);
|
||||
_nonfinite_input_perf = perf_alloc(PC_COUNT, _perf_name);
|
||||
}
|
||||
|
||||
ECL_Controller::~ECL_Controller()
|
||||
{
|
||||
perf_free(_nonfinite_input_perf);
|
||||
}
|
||||
|
||||
void ECL_Controller::reset_integrator()
|
||||
{
|
||||
_integrator = 0.0f;
|
||||
}
|
||||
|
||||
void ECL_Controller::set_time_constant(float time_constant)
|
||||
{
|
||||
if (time_constant > 0.1f && time_constant < 3.0f) {
|
||||
_tc = time_constant;
|
||||
}
|
||||
}
|
||||
|
||||
void ECL_Controller::set_k_p(float k_p)
|
||||
{
|
||||
_k_p = k_p;
|
||||
}
|
||||
|
||||
void ECL_Controller::set_k_i(float k_i)
|
||||
{
|
||||
_k_i = k_i;
|
||||
}
|
||||
|
||||
void ECL_Controller::set_k_ff(float k_ff)
|
||||
{
|
||||
_k_ff = k_ff;
|
||||
}
|
||||
|
||||
void ECL_Controller::set_integrator_max(float max)
|
||||
{
|
||||
_integrator_max = max;
|
||||
}
|
||||
|
||||
void ECL_Controller::set_max_rate(float max_rate)
|
||||
{
|
||||
_max_rate = max_rate;
|
||||
}
|
||||
|
||||
float ECL_Controller::get_rate_error()
|
||||
{
|
||||
return _rate_error;
|
||||
}
|
||||
|
||||
float ECL_Controller::get_desired_rate()
|
||||
{
|
||||
return _rate_setpoint;
|
||||
}
|
||||
|
||||
float ECL_Controller::get_desired_bodyrate()
|
||||
{
|
||||
return _bodyrate_setpoint;
|
||||
}
|
||||
|
||||
float ECL_Controller::constrain_airspeed(float airspeed, float minspeed, float maxspeed) {
|
||||
float airspeed_result = airspeed;
|
||||
if (!PX4_ISFINITE(airspeed)) {
|
||||
/* airspeed is NaN, +- INF or not available, pick center of band */
|
||||
airspeed_result = 0.5f * (minspeed + maxspeed);
|
||||
} else if (airspeed < minspeed) {
|
||||
airspeed_result = minspeed;
|
||||
}
|
||||
return airspeed_result;
|
||||
}
|
||||
Reference in New Issue
Block a user