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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 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_roll_controller.cpp
+ * Implementation of a simple orthogonal roll PID controller.
+ *
+ * Authors and acknowledgements in header.
+ */
+
+#include "../ecl.h"
+#include "ecl_roll_controller.h"
+#include <stdint.h>
+#include <float.h>
+#include <geo/geo.h>
+#include <ecl/ecl.h>
+#include <mathlib/mathlib.h>
+
+ECL_RollController::ECL_RollController() :
+ _last_run(0),
+ _tc(0.1f),
+ _last_output(0.0f),
+ _integrator(0.0f),
+ _rate_error(0.0f),
+ _rate_setpoint(0.0f),
+ _max_deflection_rad(math::radians(45.0f))
+{
+
+}
+
+float ECL_RollController::control(float roll_setpoint, float roll, float roll_rate,
+ float scaler, bool lock_integrator, float airspeed_min, float airspeed_max, float airspeed)
+{
+ /* get the usual dt estimate */
+ uint64_t dt_micros = ecl_elapsed_time(&_last_run);
+ _last_run = ecl_absolute_time();
+ float dt = (float)dt_micros * 1e-6f;
+
+ /* lock integral for long intervals */
+ if (dt_micros > 500000)
+ lock_integrator = true;
+
+ float k_ff = math::max((_k_p - _k_i * _tc) * _tc - _k_d, 0.0f);
+ float k_i_rate = _k_i * _tc;
+
+ /* input conditioning */
+ if (!isfinite(airspeed)) {
+ /* airspeed is NaN, +- INF or not available, pick center of band */
+ airspeed = 0.5f * (airspeed_min + airspeed_max);
+ } else if (airspeed < airspeed_min) {
+ airspeed = airspeed_min;
+ }
+
+ float roll_error = roll_setpoint - roll;
+ _rate_setpoint = roll_error / _tc;
+
+ /* limit the rate */
+ if (_max_rate > 0.01f) {
+ _rate_setpoint = (_rate_setpoint > _max_rate) ? _max_rate : _rate_setpoint;
+ _rate_setpoint = (_rate_setpoint < -_max_rate) ? -_max_rate : _rate_setpoint;
+ }
+
+ _rate_error = _rate_setpoint - roll_rate;
+
+
+ float ilimit_scaled = _integrator_max * scaler;
+
+ if (!lock_integrator && k_i_rate > 0.0f && airspeed > 0.5f * airspeed_min) {
+
+ float id = _rate_error * k_i_rate * dt * scaler;
+
+ /*
+ * anti-windup: do not allow integrator to increase into the
+ * wrong direction if actuator is at limit
+ */
+ if (_last_output < -_max_deflection_rad) {
+ /* only allow motion to center: increase value */
+ id = math::max(id, 0.0f);
+ } else if (_last_output > _max_deflection_rad) {
+ /* only allow motion to center: decrease value */
+ id = math::min(id, 0.0f);
+ }
+
+ _integrator += id;
+ }
+
+ /* integrator limit */
+ _integrator = math::constrain(_integrator, -ilimit_scaled, ilimit_scaled);
+ /* store non-limited output */
+ _last_output = ((_rate_error * _k_d * scaler) + _integrator + (_rate_setpoint * k_ff)) * scaler;
+
+ return math::constrain(_last_output, -_max_deflection_rad, _max_deflection_rad);
+}
+
+void ECL_RollController::reset_integrator()
+{
+ _integrator = 0.0f;
+}
+