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authorThomas Gubler <thomasgubler@gmail.com>2012-10-21 21:36:29 +0200
committerThomas Gubler <thomasgubler@gmail.com>2012-10-21 21:36:29 +0200
commitab447ac713b010c090d6e2de85fa5d0d0af5cbbe (patch)
treef813e61089b3e27c7eee4b5a99a30322be50a5b2 /apps/fixedwing_att_control/fixedwing_att_control_att.c
parent5616f5c4b1a40bab6a48ec95775ed74a03c73273 (diff)
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[work in progess]roll attitude and roll rate loop works
Diffstat (limited to 'apps/fixedwing_att_control/fixedwing_att_control_att.c')
-rw-r--r--apps/fixedwing_att_control/fixedwing_att_control_att.c131
1 files changed, 131 insertions, 0 deletions
diff --git a/apps/fixedwing_att_control/fixedwing_att_control_att.c b/apps/fixedwing_att_control/fixedwing_att_control_att.c
new file mode 100644
index 000000000..7d648ccfa
--- /dev/null
+++ b/apps/fixedwing_att_control/fixedwing_att_control_att.c
@@ -0,0 +1,131 @@
+/****************************************************************************
+ *
+ * Copyright (C) 2012 PX4 Development Team. All rights reserved.
+ * Author: @author Thomas Gubler <thomasgubler@student.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 fixedwing_att_control_rate.c
+ * Implementation of a fixed wing attitude controller.
+ */
+#include <fixedwing_att_control_rate.h>
+
+#include <nuttx/config.h>
+#include <stdio.h>
+#include <stdlib.h>
+#include <string.h>
+#include <unistd.h>
+#include <fcntl.h>
+#include <errno.h>
+#include <math.h>
+#include <poll.h>
+#include <time.h>
+#include <arch/board/up_hrt.h>
+#include <arch/board/board.h>
+#include <uORB/uORB.h>
+
+#include <uORB/topics/vehicle_attitude.h>
+#include <uORB/topics/vehicle_attitude_setpoint.h>
+#include <uORB/topics/manual_control_setpoint.h>
+#include <systemlib/param/param.h>
+#include <systemlib/pid/pid.h>
+#include <systemlib/geo/geo.h>
+#include <systemlib/systemlib.h>
+
+
+
+
+struct fw_att_control_params {
+ param_t roll_p;
+};
+
+
+
+/* Internal Prototypes */
+static int parameters_init(struct fw_att_control_params *h);
+static int parameters_update(const struct fw_att_control_params *h, struct fw_att_control_params *p);
+
+static int parameters_init(struct fw_att_control_params *h)
+{
+ /* PID parameters */
+ h->roll_p = param_find("FW_ROLL_POS_P"); //TODO define rate params for fixed wing
+
+
+// if(h->attrate_i == PARAM_INVALID)
+// printf("FATAL MC_ATTRATE_I does not exist\n");
+
+ return OK;
+}
+
+static int parameters_update(const struct fw_att_control_params *h, struct fw_att_control_params *p)
+{
+ param_get(h->roll_p, &(p->roll_p));
+
+ return OK;
+}
+
+int fixedwing_att_control_attitude(const struct vehicle_attitude_setpoint_s *att_sp,
+ const struct vehicle_attitude_s *att,
+ struct vehicle_rates_setpoint_s *rates_sp)
+{
+ static int counter = 0;
+ static bool initialized = false;
+
+ static struct fw_att_control_params p;
+ static struct fw_att_control_params h;
+
+ static uint64_t last_run = 0;
+ const float deltaT = (hrt_absolute_time() - last_run) / 1000000.0f;
+ last_run = hrt_absolute_time();
+
+ if(!initialized)
+ {
+ parameters_init(&h);
+ parameters_update(&h, &p);
+ initialized = true;
+ }
+
+ /* load new parameters with lower rate */
+ if (counter % 2500 == 0) {
+ /* update parameters from storage */
+ parameters_update(&h, &p);
+ }
+
+ /* Roll (P) */
+ float roll_error = att_sp->roll_tait_bryan - att->roll;
+ rates_sp->roll = p.roll_p * roll_error;
+
+ counter++;
+
+ return 0;
+}
+
+
+