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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
+ * 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_yaw_controller.h
+ * Definition of a simple orthogonal coordinated turn yaw PID controller.
+ *
+ */
+#ifndef ECL_YAW_CONTROLLER_H
+#define ECL_YAW_CONTROLLER_H
+
+#include <stdbool.h>
+#include <stdint.h>
+
+class __EXPORT ECL_YawController
+{
+public:
+ ECL_YawController();
+
+ float control(float roll, float yaw_rate, float accel_y, float scaler = 1.0f, bool lock_integrator = false,
+ float airspeed_min = 0, float airspeed_max = 0, float aspeed = (0.0f / 0.0f));
+
+ void reset_integrator();
+
+ void set_k_side(float k_a) {
+ _k_side = k_a;
+ }
+ void set_k_i(float k_i) {
+ _k_i = k_i;
+ }
+ void set_k_d(float k_d) {
+ _k_d = k_d;
+ }
+ void set_k_roll_ff(float k_roll_ff) {
+ _k_roll_ff = k_roll_ff;
+ }
+ void set_integrator_max(float max) {
+ _integrator_max = max;
+ }
+
+private:
+ uint64_t _last_run;
+
+ float _k_side;
+ float _k_i;
+ float _k_d;
+ float _k_roll_ff;
+ float _integrator_max;
+
+ float _last_error;
+ float _last_output;
+ float _last_rate_hp_out;
+ float _last_rate_hp_in;
+ float _k_d_last;
+ float _integrator;
+
+};
+
+#endif // ECL_YAW_CONTROLLER_H