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diff --git a/src/modules/attitude_estimator_ekf/attitude_estimator_ekf_params.c b/src/modules/attitude_estimator_ekf/attitude_estimator_ekf_params.c
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+/****************************************************************************
+ *
+ * Copyright (C) 2012 PX4 Development Team. All rights reserved.
+ * Author: Tobias Naegeli <naegelit@student.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 attitude_estimator_ekf_params.c
+ *
+ * Parameters for EKF filter
+ */
+
+#include "attitude_estimator_ekf_params.h"
+
+/* Extended Kalman Filter covariances */
+
+/* gyro process noise */
+PARAM_DEFINE_FLOAT(EKF_ATT_V2_Q0, 1e-4f);
+PARAM_DEFINE_FLOAT(EKF_ATT_V2_Q1, 0.08f);
+PARAM_DEFINE_FLOAT(EKF_ATT_V2_Q2, 0.009f);
+/* gyro offsets process noise */
+PARAM_DEFINE_FLOAT(EKF_ATT_V2_Q3, 0.005f);
+PARAM_DEFINE_FLOAT(EKF_ATT_V2_Q4, 0.0f);
+
+/* gyro measurement noise */
+PARAM_DEFINE_FLOAT(EKF_ATT_V2_R0, 0.0008f);
+PARAM_DEFINE_FLOAT(EKF_ATT_V2_R1, 0.8f);
+PARAM_DEFINE_FLOAT(EKF_ATT_V2_R2, 1.0f);
+/* accelerometer measurement noise */
+PARAM_DEFINE_FLOAT(EKF_ATT_V2_R3, 0.0f);
+
+/* offsets in roll, pitch and yaw of sensor plane and body */
+PARAM_DEFINE_FLOAT(ATT_ROLL_OFFS, 0.0f);
+PARAM_DEFINE_FLOAT(ATT_PITCH_OFFS, 0.0f);
+PARAM_DEFINE_FLOAT(ATT_YAW_OFFS, 0.0f);
+
+int parameters_init(struct attitude_estimator_ekf_param_handles *h)
+{
+ /* PID parameters */
+ h->q0 = param_find("EKF_ATT_V2_Q0");
+ h->q1 = param_find("EKF_ATT_V2_Q1");
+ h->q2 = param_find("EKF_ATT_V2_Q2");
+ h->q3 = param_find("EKF_ATT_V2_Q3");
+ h->q4 = param_find("EKF_ATT_V2_Q4");
+
+ h->r0 = param_find("EKF_ATT_V2_R0");
+ h->r1 = param_find("EKF_ATT_V2_R1");
+ h->r2 = param_find("EKF_ATT_V2_R2");
+ h->r3 = param_find("EKF_ATT_V2_R3");
+
+ h->roll_off = param_find("ATT_ROLL_OFFS");
+ h->pitch_off = param_find("ATT_PITCH_OFFS");
+ h->yaw_off = param_find("ATT_YAW_OFFS");
+
+ return OK;
+}
+
+int parameters_update(const struct attitude_estimator_ekf_param_handles *h, struct attitude_estimator_ekf_params *p)
+{
+ param_get(h->q0, &(p->q[0]));
+ param_get(h->q1, &(p->q[1]));
+ param_get(h->q2, &(p->q[2]));
+ param_get(h->q3, &(p->q[3]));
+ param_get(h->q4, &(p->q[4]));
+
+ param_get(h->r0, &(p->r[0]));
+ param_get(h->r1, &(p->r[1]));
+ param_get(h->r2, &(p->r[2]));
+ param_get(h->r3, &(p->r[3]));
+
+ param_get(h->roll_off, &(p->roll_off));
+ param_get(h->pitch_off, &(p->pitch_off));
+ param_get(h->yaw_off, &(p->yaw_off));
+
+ return OK;
+}