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diff --git a/src/examples/flow_position_control/flow_position_control_params.c b/src/examples/flow_position_control/flow_position_control_params.c
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-/****************************************************************************
- *
- * Copyright (C) 2008-2013 PX4 Development Team. All rights reserved.
- * Author: Samuel Zihlmann <samuezih@ee.ethz.ch>
- * Lorenz Meier <lm@inf.ethz.ch>
- *
- * 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 flow_position_control_params.c
- */
-
-#include "flow_position_control_params.h"
-
-/* controller parameters */
-
-// Position control P gain
-PARAM_DEFINE_FLOAT(FPC_POS_P, 3.0f);
-// Position control D / damping gain
-PARAM_DEFINE_FLOAT(FPC_POS_D, 0.0f);
-// Altitude control P gain
-PARAM_DEFINE_FLOAT(FPC_H_P, 0.15f);
-// Altitude control I (integrator) gain
-PARAM_DEFINE_FLOAT(FPC_H_I, 0.00001f);
-// Altitude control D gain
-PARAM_DEFINE_FLOAT(FPC_H_D, 0.8f);
-// Altitude control rate limiter
-PARAM_DEFINE_FLOAT(FPC_H_RATE, 0.1f);
-// Altitude control minimum altitude
-PARAM_DEFINE_FLOAT(FPC_H_MIN, 0.5f);
-// Altitude control maximum altitude (higher than 1.5m is untested)
-PARAM_DEFINE_FLOAT(FPC_H_MAX, 1.5f);
-// Altitude control feed forward throttle - adjust to the
-// throttle position (0..1) where the copter hovers in manual flight
-PARAM_DEFINE_FLOAT(FPC_T_FFWD, 0.7f); // adjust this before flight
-PARAM_DEFINE_FLOAT(FPC_L_S_X, 1.2f);
-PARAM_DEFINE_FLOAT(FPC_L_S_Y, 1.2f);
-PARAM_DEFINE_FLOAT(FPC_L_H_ERR, 0.1f);
-PARAM_DEFINE_FLOAT(FPC_L_TH_I, 0.05f);
-PARAM_DEFINE_FLOAT(FPC_L_TH_U, 0.8f);
-PARAM_DEFINE_FLOAT(FPC_L_TH_L, 0.6f);
-PARAM_DEFINE_FLOAT(FPC_L_YAW_STEP, 0.03f);
-PARAM_DEFINE_FLOAT(FPC_MAN_THR, 0.1f);
-
-
-int parameters_init(struct flow_position_control_param_handles *h)
-{
- /* PID parameters */
- h->pos_p = param_find("FPC_POS_P");
- h->pos_d = param_find("FPC_POS_D");
- h->height_p = param_find("FPC_H_P");
- h->height_i = param_find("FPC_H_I");
- h->height_d = param_find("FPC_H_D");
- h->height_rate = param_find("FPC_H_RATE");
- h->height_min = param_find("FPC_H_MIN");
- h->height_max = param_find("FPC_H_MAX");
- h->thrust_feedforward = param_find("FPC_T_FFWD");
- h->limit_speed_x = param_find("FPC_L_S_X");
- h->limit_speed_y = param_find("FPC_L_S_Y");
- h->limit_height_error = param_find("FPC_L_H_ERR");
- h->limit_thrust_int = param_find("FPC_L_TH_I");
- h->limit_thrust_upper = param_find("FPC_L_TH_U");
- h->limit_thrust_lower = param_find("FPC_L_TH_L");
- h->limit_yaw_step = param_find("FPC_L_YAW_STEP");
- h->manual_threshold = param_find("FPC_MAN_THR");
- h->rc_scale_pitch = param_find("RC_SCALE_PITCH");
- h->rc_scale_roll = param_find("RC_SCALE_ROLL");
- h->rc_scale_yaw = param_find("RC_SCALE_YAW");
-
- return OK;
-}
-
-int parameters_update(const struct flow_position_control_param_handles *h, struct flow_position_control_params *p)
-{
- param_get(h->pos_p, &(p->pos_p));
- param_get(h->pos_d, &(p->pos_d));
- param_get(h->height_p, &(p->height_p));
- param_get(h->height_i, &(p->height_i));
- param_get(h->height_d, &(p->height_d));
- param_get(h->height_rate, &(p->height_rate));
- param_get(h->height_min, &(p->height_min));
- param_get(h->height_max, &(p->height_max));
- param_get(h->thrust_feedforward, &(p->thrust_feedforward));
- param_get(h->limit_speed_x, &(p->limit_speed_x));
- param_get(h->limit_speed_y, &(p->limit_speed_y));
- param_get(h->limit_height_error, &(p->limit_height_error));
- param_get(h->limit_thrust_int, &(p->limit_thrust_int));
- param_get(h->limit_thrust_upper, &(p->limit_thrust_upper));
- param_get(h->limit_thrust_lower, &(p->limit_thrust_lower));
- param_get(h->limit_yaw_step, &(p->limit_yaw_step));
- param_get(h->manual_threshold, &(p->manual_threshold));
- param_get(h->rc_scale_pitch, &(p->rc_scale_pitch));
- param_get(h->rc_scale_roll, &(p->rc_scale_roll));
- param_get(h->rc_scale_yaw, &(p->rc_scale_yaw));
-
- return OK;
-}