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/****************************************************************************
 *
 *   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 APL 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
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 ****************************************************************************/

/**
 * @file ecl_pitch_controller.h
 * Definition of a simple orthogonal pitch PID controller.
 *
 */

#ifndef ECL_PITCH_CONTROLLER_H
#define ECL_PITCH_CONTROLLER_H

#include <stdbool.h>
#include <stdint.h>

class __EXPORT ECL_PitchController
{
public:
	ECL_PitchController();

	float control(float pitch_setpoint, float pitch, float pitch_rate, float roll, float scaler = 1.0f,
		      bool lock_integrator = false, float airspeed_min = 0.0f, float airspeed_max = 0.0f, float airspeed = (0.0f / 0.0f));

	void reset_integrator();

	void set_time_constant(float time_constant) {
		_tc = time_constant;
	}
	void set_k_p(float k_p) {
		_k_p = k_p;
	}
	void set_k_i(float k_i) {
		_k_i = k_i;
	}
	void set_k_d(float k_d) {
		_k_d = k_d;
	}
	void set_integrator_max(float max) {
		_integrator_max = max;
	}
	void set_max_rate_pos(float max_rate_pos) {
		_max_rate_pos = max_rate_pos;
	}
	void set_max_rate_neg(float max_rate_neg) {
		_max_rate_neg = max_rate_neg;
	}
	void set_roll_ff(float roll_ff) {
		_roll_ff = roll_ff;
	}

	float get_rate_error() {
		return _rate_error;
	}

	float get_desired_rate() {
		return _desired_rate;
	}

private:

	uint64_t _last_run;
	float _tc;
	float _k_p;
	float _k_i;
	float _k_d;
	float _integrator_max;
	float _max_rate_pos;
	float _max_rate_neg;
	float _roll_ff;
	float _last_output;
	float _integrator;
	float _rate_error;
	float _rate_setpoint;
	float _max_deflection_rad;
};

#endif // ECL_PITCH_CONTROLLER_H