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+/****************************************************************************
+ *
+ * Copyright (c) 2013, 2014 PX4 Development Team. 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 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 mc_att_control_main.cpp
+ * Multicopter attitude controller.
+ *
+ * @author Tobias Naegeli <naegelit@student.ethz.ch>
+ * @author Lorenz Meier <lm@inf.ethz.ch>
+ * @author Anton Babushkin <anton.babushkin@me.com>
+ * @author Thomas Gubler <thomasgubler@gmail.com>
+ * @author Julian Oes <julian@oes.ch>
+ * @author Roman Bapst <bapstr@ethz.ch>
+ *
+ * The controller has two loops: P loop for angular error and PD loop for angular rate error.
+ * Desired rotation calculated keeping in mind that yaw response is normally slower than roll/pitch.
+ * For small deviations controller rotates copter to have shortest path of thrust vector and independently rotates around yaw,
+ * so actual rotation axis is not constant. For large deviations controller rotates copter around fixed axis.
+ * These two approaches fused seamlessly with weight depending on angular error.
+ * When thrust vector directed near-horizontally (e.g. roll ~= PI/2) yaw setpoint ignored because of singularity.
+ * Controller doesn't use Euler angles for work, they generated only for more human-friendly control and logging.
+ * If rotation matrix setpoint is invalid it will be generated from Euler angles for compatibility with old position controllers.
+ */
+
+#include <string.h>
+#include <cstdlib>
+#include "mc_att_control.h"
+
+static bool thread_running = false; /**< Deamon status flag */
+static int daemon_task; /**< Handle of deamon task / thread */
+namespace px4
+{
+bool task_should_exit = false;
+}
+
+using namespace px4;
+
+PX4_MAIN_FUNCTION(mc_att_control_multiplatform);
+
+#if !defined(__linux) && !(defined(__APPLE__) && defined(__MACH__))
+/**
+ * Multicopter attitude control app start / stop handling function
+ *
+ * @ingroup apps
+ */
+
+extern "C" __EXPORT int mc_att_control_multiplatform_main(int argc, char *argv[]);
+int mc_att_control_multiplatform_main(int argc, char *argv[])
+{
+ if (argc < 1) {
+ errx(1, "usage: mc_att_control {start|stop|status}");
+ }
+
+ if (!strcmp(argv[1], "start")) {
+
+ if (thread_running) {
+ warnx("already running");
+ /* this is not an error */
+ exit(0);
+ }
+
+ task_should_exit = false;
+
+ daemon_task = task_spawn_cmd("mc_att_control",
+ SCHED_DEFAULT,
+ SCHED_PRIORITY_MAX - 5,
+ 3000,
+ mc_att_control_multiplatform_task_main,
+ (argv) ? (char * const *)&argv[2] : (char * const *)NULL);
+
+ exit(0);
+ }
+
+ if (!strcmp(argv[1], "stop")) {
+ task_should_exit = true;
+ exit(0);
+ }
+
+ if (!strcmp(argv[1], "status")) {
+ if (thread_running) {
+ warnx("is running");
+
+ } else {
+ warnx("not started");
+ }
+
+ exit(0);
+ }
+
+ warnx("unrecognized command");
+ return 1;
+}
+#endif
+
+PX4_MAIN_FUNCTION(mc_att_control_multiplatform)
+{
+ px4::init(argc, argv, "mc_att_control_multiplatform");
+
+ PX4_INFO("starting");
+ MulticopterAttitudeControl attctl;
+ thread_running = true;
+ attctl.spin();
+
+ PX4_INFO("exiting.");
+ thread_running = false;
+ return 0;
+}
+
+