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diff --git a/src/modules/commander/state_machine_helper.c b/src/modules/commander/state_machine_helper.c
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+/****************************************************************************
+ *
+ * Copyright (C) 2012 PX4 Development Team. All rights reserved.
+ * Author: Thomas Gubler <thomasgubler@student.ethz.ch>
+ * Julian Oes <joes@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 state_machine_helper.c
+ * State machine helper functions implementations
+ */
+
+#include <stdio.h>
+#include <unistd.h>
+
+#include <uORB/uORB.h>
+#include <uORB/topics/vehicle_status.h>
+#include <uORB/topics/actuator_controls.h>
+#include <systemlib/systemlib.h>
+#include <drivers/drv_hrt.h>
+#include <mavlink/mavlink_log.h>
+
+#include "state_machine_helper.h"
+
+static const char *system_state_txt[] = {
+ "SYSTEM_STATE_PREFLIGHT",
+ "SYSTEM_STATE_STANDBY",
+ "SYSTEM_STATE_GROUND_READY",
+ "SYSTEM_STATE_MANUAL",
+ "SYSTEM_STATE_STABILIZED",
+ "SYSTEM_STATE_AUTO",
+ "SYSTEM_STATE_MISSION_ABORT",
+ "SYSTEM_STATE_EMCY_LANDING",
+ "SYSTEM_STATE_EMCY_CUTOFF",
+ "SYSTEM_STATE_GROUND_ERROR",
+ "SYSTEM_STATE_REBOOT",
+
+};
+
+/**
+ * Transition from one state to another
+ */
+int do_state_update(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd, commander_state_machine_t new_state)
+{
+ int invalid_state = false;
+ int ret = ERROR;
+
+ commander_state_machine_t old_state = current_status->state_machine;
+
+ switch (new_state) {
+ case SYSTEM_STATE_MISSION_ABORT: {
+ /* Indoor or outdoor */
+ // if (flight_environment_parameter == PX4_FLIGHT_ENVIRONMENT_OUTDOOR) {
+ ret = do_state_update(status_pub, current_status, mavlink_fd, (commander_state_machine_t)SYSTEM_STATE_EMCY_LANDING);
+
+ // } else {
+ // ret = do_state_update(status_pub, current_status, mavlink_fd, (commander_state_machine_t)SYSTEM_STATE_EMCY_CUTOFF);
+ // }
+ }
+ break;
+
+ case SYSTEM_STATE_EMCY_LANDING:
+ /* Tell the controller to land */
+
+ /* set system flags according to state */
+ current_status->flag_system_armed = true;
+
+ warnx("EMERGENCY LANDING!\n");
+ mavlink_log_critical(mavlink_fd, "EMERGENCY LANDING!");
+ break;
+
+ case SYSTEM_STATE_EMCY_CUTOFF:
+ /* Tell the controller to cutoff the motors (thrust = 0) */
+
+ /* set system flags according to state */
+ current_status->flag_system_armed = false;
+
+ warnx("EMERGENCY MOTOR CUTOFF!\n");
+ mavlink_log_critical(mavlink_fd, "EMERGENCY MOTOR CUTOFF!");
+ break;
+
+ case SYSTEM_STATE_GROUND_ERROR:
+
+ /* set system flags according to state */
+
+ /* prevent actuators from arming */
+ current_status->flag_system_armed = false;
+
+ warnx("GROUND ERROR, locking down propulsion system\n");
+ mavlink_log_critical(mavlink_fd, "GROUND ERROR, locking down system");
+ break;
+
+ case SYSTEM_STATE_PREFLIGHT:
+ if (current_status->state_machine == SYSTEM_STATE_STANDBY
+ || current_status->state_machine == SYSTEM_STATE_PREFLIGHT) {
+ /* set system flags according to state */
+ current_status->flag_system_armed = false;
+ mavlink_log_critical(mavlink_fd, "Switched to PREFLIGHT state");
+
+ } else {
+ invalid_state = true;
+ mavlink_log_critical(mavlink_fd, "REFUSED to switch to PREFLIGHT state");
+ }
+
+ break;
+
+ case SYSTEM_STATE_REBOOT:
+ if (current_status->state_machine == SYSTEM_STATE_STANDBY
+ || current_status->state_machine == SYSTEM_STATE_PREFLIGHT
+ || current_status->flag_hil_enabled) {
+ invalid_state = false;
+ /* set system flags according to state */
+ current_status->flag_system_armed = false;
+ mavlink_log_critical(mavlink_fd, "REBOOTING SYSTEM");
+ usleep(500000);
+ up_systemreset();
+ /* SPECIAL CASE: NEVER RETURNS FROM THIS FUNCTION CALL */
+
+ } else {
+ invalid_state = true;
+ mavlink_log_critical(mavlink_fd, "REFUSED to REBOOT");
+ }
+
+ break;
+
+ case SYSTEM_STATE_STANDBY:
+ /* set system flags according to state */
+
+ /* standby enforces disarmed */
+ current_status->flag_system_armed = false;
+
+ mavlink_log_critical(mavlink_fd, "Switched to STANDBY state");
+ break;
+
+ case SYSTEM_STATE_GROUND_READY:
+
+ /* set system flags according to state */
+
+ /* ground ready has motors / actuators armed */
+ current_status->flag_system_armed = true;
+
+ mavlink_log_critical(mavlink_fd, "Switched to GROUND READY state");
+ break;
+
+ case SYSTEM_STATE_AUTO:
+
+ /* set system flags according to state */
+
+ /* auto is airborne and in auto mode, motors armed */
+ current_status->flag_system_armed = true;
+
+ mavlink_log_critical(mavlink_fd, "Switched to FLYING / AUTO mode");
+ break;
+
+ case SYSTEM_STATE_STABILIZED:
+
+ /* set system flags according to state */
+ current_status->flag_system_armed = true;
+
+ mavlink_log_critical(mavlink_fd, "Switched to FLYING / STABILIZED mode");
+ break;
+
+ case SYSTEM_STATE_MANUAL:
+
+ /* set system flags according to state */
+ current_status->flag_system_armed = true;
+
+ mavlink_log_critical(mavlink_fd, "Switched to FLYING / MANUAL mode");
+ break;
+
+ default:
+ invalid_state = true;
+ break;
+ }
+
+ if (invalid_state == false || old_state != new_state) {
+ current_status->state_machine = new_state;
+ state_machine_publish(status_pub, current_status, mavlink_fd);
+ publish_armed_status(current_status);
+ ret = OK;
+ }
+
+ if (invalid_state) {
+ mavlink_log_critical(mavlink_fd, "REJECTING invalid state transition");
+ ret = ERROR;
+ }
+
+ return ret;
+}
+
+void state_machine_publish(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd)
+{
+ /* publish the new state */
+ current_status->counter++;
+ current_status->timestamp = hrt_absolute_time();
+
+ /* assemble state vector based on flag values */
+ if (current_status->flag_control_rates_enabled) {
+ current_status->onboard_control_sensors_present |= 0x400;
+
+ } else {
+ current_status->onboard_control_sensors_present &= ~0x400;
+ }
+
+ current_status->onboard_control_sensors_present |= (current_status->flag_control_attitude_enabled) ? 0x800 : 0;
+ current_status->onboard_control_sensors_present |= (current_status->flag_control_attitude_enabled) ? 0x1000 : 0;
+ current_status->onboard_control_sensors_present |= (current_status->flag_control_velocity_enabled || current_status->flag_control_position_enabled) ? 0x2000 : 0;
+ current_status->onboard_control_sensors_present |= (current_status->flag_control_velocity_enabled || current_status->flag_control_position_enabled) ? 0x4000 : 0;
+
+ current_status->onboard_control_sensors_enabled |= (current_status->flag_control_rates_enabled) ? 0x400 : 0;
+ current_status->onboard_control_sensors_enabled |= (current_status->flag_control_attitude_enabled) ? 0x800 : 0;
+ current_status->onboard_control_sensors_enabled |= (current_status->flag_control_attitude_enabled) ? 0x1000 : 0;
+ current_status->onboard_control_sensors_enabled |= (current_status->flag_control_velocity_enabled || current_status->flag_control_position_enabled) ? 0x2000 : 0;
+ current_status->onboard_control_sensors_enabled |= (current_status->flag_control_velocity_enabled || current_status->flag_control_position_enabled) ? 0x4000 : 0;
+
+ orb_publish(ORB_ID(vehicle_status), status_pub, current_status);
+ printf("[cmd] new state: %s\n", system_state_txt[current_status->state_machine]);
+}
+
+void publish_armed_status(const struct vehicle_status_s *current_status)
+{
+ struct actuator_armed_s armed;
+ armed.armed = current_status->flag_system_armed;
+ /* lock down actuators if required, only in HIL */
+ armed.lockdown = (current_status->flag_hil_enabled) ? true : false;
+ orb_advert_t armed_pub = orb_advertise(ORB_ID(actuator_armed), &armed);
+ orb_publish(ORB_ID(actuator_armed), armed_pub, &armed);
+}
+
+
+/*
+ * Private functions, update the state machine
+ */
+void state_machine_emergency_always_critical(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd)
+{
+ warnx("EMERGENCY HANDLER\n");
+ /* Depending on the current state go to one of the error states */
+
+ if (current_status->state_machine == SYSTEM_STATE_PREFLIGHT || current_status->state_machine == SYSTEM_STATE_STANDBY || current_status->state_machine == SYSTEM_STATE_GROUND_READY) {
+ do_state_update(status_pub, current_status, mavlink_fd, (commander_state_machine_t)SYSTEM_STATE_GROUND_ERROR);
+
+ } else if (current_status->state_machine == SYSTEM_STATE_AUTO || current_status->state_machine == SYSTEM_STATE_MANUAL) {
+
+ // DO NOT abort mission
+ //do_state_update(status_pub, current_status, mavlink_fd, (commander_state_machine_t)SYSTEM_STATE_MISSION_ABORT);
+
+ } else {
+ warnx("Unknown system state: #%d\n", current_status->state_machine);
+ }
+}
+
+void state_machine_emergency(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd) //do not call state_machine_emergency_always_critical if we are in manual mode for these errors
+{
+ if (current_status->state_machine != SYSTEM_STATE_MANUAL) { //if we are in manual: user can react to errors themself
+ state_machine_emergency_always_critical(status_pub, current_status, mavlink_fd);
+
+ } else {
+ //global_data_send_mavlink_statustext_message_out("[cmd] ERROR: take action immediately! (did not switch to error state because the system is in manual mode)", MAV_SEVERITY_CRITICAL);
+ }
+
+}
+
+
+
+// /*
+// * Wrapper functions (to be used in the commander), all functions assume lock on current_status
+// */
+
+// /* These functions decide if an emergency exits and then switch to SYSTEM_STATE_MISSION_ABORT or SYSTEM_STATE_GROUND_ERROR
+// *
+// * START SUBSYSTEM/EMERGENCY FUNCTIONS
+// * */
+
+// void update_state_machine_subsystem_present(int status_pub, struct vehicle_status_s *current_status, subsystem_type_t *subsystem_type)
+// {
+// current_status->onboard_control_sensors_present |= 1 << *subsystem_type;
+// current_status->counter++;
+// current_status->timestamp = hrt_absolute_time();
+// orb_publish(ORB_ID(vehicle_status), status_pub, current_status);
+// }
+
+// void update_state_machine_subsystem_notpresent(int status_pub, struct vehicle_status_s *current_status, subsystem_type_t *subsystem_type)
+// {
+// current_status->onboard_control_sensors_present &= ~(1 << *subsystem_type);
+// current_status->counter++;
+// current_status->timestamp = hrt_absolute_time();
+// orb_publish(ORB_ID(vehicle_status), status_pub, current_status);
+
+// /* if a subsystem was removed something went completely wrong */
+
+// switch (*subsystem_type) {
+// case SUBSYSTEM_TYPE_GYRO:
+// //global_data_send_mavlink_statustext_message_out("Commander: gyro not present", MAV_SEVERITY_EMERGENCY);
+// state_machine_emergency_always_critical(status_pub, current_status);
+// break;
+
+// case SUBSYSTEM_TYPE_ACC:
+// //global_data_send_mavlink_statustext_message_out("Commander: accelerometer not present", MAV_SEVERITY_EMERGENCY);
+// state_machine_emergency_always_critical(status_pub, current_status);
+// break;
+
+// case SUBSYSTEM_TYPE_MAG:
+// //global_data_send_mavlink_statustext_message_out("Commander: magnetometer not present", MAV_SEVERITY_EMERGENCY);
+// state_machine_emergency_always_critical(status_pub, current_status);
+// break;
+
+// case SUBSYSTEM_TYPE_GPS:
+// {
+// uint8_t flight_env = global_data_parameter_storage->pm.param_values[PARAM_FLIGHT_ENV];
+
+// if (flight_env == PX4_FLIGHT_ENVIRONMENT_OUTDOOR) {
+// //global_data_send_mavlink_statustext_message_out("Commander: GPS not present", MAV_SEVERITY_EMERGENCY);
+// state_machine_emergency(status_pub, current_status);
+// }
+// }
+// break;
+
+// default:
+// break;
+// }
+
+// }
+
+// void update_state_machine_subsystem_enabled(int status_pub, struct vehicle_status_s *current_status, subsystem_type_t *subsystem_type)
+// {
+// current_status->onboard_control_sensors_enabled |= 1 << *subsystem_type;
+// current_status->counter++;
+// current_status->timestamp = hrt_absolute_time();
+// orb_publish(ORB_ID(vehicle_status), status_pub, current_status);
+// }
+
+// void update_state_machine_subsystem_disabled(int status_pub, struct vehicle_status_s *current_status, subsystem_type_t *subsystem_type)
+// {
+// current_status->onboard_control_sensors_enabled &= ~(1 << *subsystem_type);
+// current_status->counter++;
+// current_status->timestamp = hrt_absolute_time();
+// orb_publish(ORB_ID(vehicle_status), status_pub, current_status);
+
+// /* if a subsystem was disabled something went completely wrong */
+
+// switch (*subsystem_type) {
+// case SUBSYSTEM_TYPE_GYRO:
+// //global_data_send_mavlink_statustext_message_out("Commander: EMERGENCY - gyro disabled", MAV_SEVERITY_EMERGENCY);
+// state_machine_emergency_always_critical(status_pub, current_status);
+// break;
+
+// case SUBSYSTEM_TYPE_ACC:
+// //global_data_send_mavlink_statustext_message_out("Commander: EMERGENCY - accelerometer disabled", MAV_SEVERITY_EMERGENCY);
+// state_machine_emergency_always_critical(status_pub, current_status);
+// break;
+
+// case SUBSYSTEM_TYPE_MAG:
+// //global_data_send_mavlink_statustext_message_out("Commander: EMERGENCY - magnetometer disabled", MAV_SEVERITY_EMERGENCY);
+// state_machine_emergency_always_critical(status_pub, current_status);
+// break;
+
+// case SUBSYSTEM_TYPE_GPS:
+// {
+// uint8_t flight_env = (uint8_t)(global_data_parameter_storage->pm.param_values[PARAM_FLIGHT_ENV]);
+
+// if (flight_env == PX4_FLIGHT_ENVIRONMENT_OUTDOOR) {
+// //global_data_send_mavlink_statustext_message_out("Commander: EMERGENCY - GPS disabled", MAV_SEVERITY_EMERGENCY);
+// state_machine_emergency(status_pub, current_status);
+// }
+// }
+// break;
+
+// default:
+// break;
+// }
+
+// }
+
+
+// void update_state_machine_subsystem_healthy(int status_pub, struct vehicle_status_s *current_status, subsystem_type_t *subsystem_type)
+// {
+// current_status->onboard_control_sensors_health |= 1 << *subsystem_type;
+// current_status->counter++;
+// current_status->timestamp = hrt_absolute_time();
+// orb_publish(ORB_ID(vehicle_status), status_pub, current_status);
+
+// switch (*subsystem_type) {
+// case SUBSYSTEM_TYPE_GYRO:
+// //TODO state machine change (recovering)
+// break;
+
+// case SUBSYSTEM_TYPE_ACC:
+// //TODO state machine change
+// break;
+
+// case SUBSYSTEM_TYPE_MAG:
+// //TODO state machine change
+// break;
+
+// case SUBSYSTEM_TYPE_GPS:
+// //TODO state machine change
+// break;
+
+// default:
+// break;
+// }
+
+
+// }
+
+
+// void update_state_machine_subsystem_unhealthy(int status_pub, struct vehicle_status_s *current_status, subsystem_type_t *subsystem_type)
+// {
+// bool previosly_healthy = (bool)(current_status->onboard_control_sensors_health & 1 << *subsystem_type);
+// current_status->onboard_control_sensors_health &= ~(1 << *subsystem_type);
+// current_status->counter++;
+// current_status->timestamp = hrt_absolute_time();
+// orb_publish(ORB_ID(vehicle_status), status_pub, current_status);
+
+// /* if we received unhealthy message more than *_HEALTH_COUNTER_LIMIT, switch to error state */
+
+// switch (*subsystem_type) {
+// case SUBSYSTEM_TYPE_GYRO:
+// //global_data_send_mavlink_statustext_message_out("Commander: gyro unhealthy", MAV_SEVERITY_CRITICAL);
+
+// if (previosly_healthy) //only throw emergency if previously healthy
+// state_machine_emergency_always_critical(status_pub, current_status);
+
+// break;
+
+// case SUBSYSTEM_TYPE_ACC:
+// //global_data_send_mavlink_statustext_message_out("Commander: accelerometer unhealthy", MAV_SEVERITY_CRITICAL);
+
+// if (previosly_healthy) //only throw emergency if previously healthy
+// state_machine_emergency_always_critical(status_pub, current_status);
+
+// break;
+
+// case SUBSYSTEM_TYPE_MAG:
+// //global_data_send_mavlink_statustext_message_out("Commander: magnetometer unhealthy", MAV_SEVERITY_CRITICAL);
+
+// if (previosly_healthy) //only throw emergency if previously healthy
+// state_machine_emergency_always_critical(status_pub, current_status);
+
+// break;
+
+// case SUBSYSTEM_TYPE_GPS:
+// // //TODO: remove this block
+// // break;
+// // ///////////////////
+// //global_data_send_mavlink_statustext_message_out("Commander: GPS unhealthy", MAV_SEVERITY_CRITICAL);
+
+// // printf("previosly_healthy = %u\n", previosly_healthy);
+// if (previosly_healthy) //only throw emergency if previously healthy
+// state_machine_emergency(status_pub, current_status);
+
+// break;
+
+// default:
+// break;
+// }
+
+// }
+
+
+/* END SUBSYSTEM/EMERGENCY FUNCTIONS*/
+
+
+void update_state_machine_got_position_fix(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd)
+{
+ /* Depending on the current state switch state */
+ if (current_status->state_machine == SYSTEM_STATE_PREFLIGHT) {
+ do_state_update(status_pub, current_status, mavlink_fd, (commander_state_machine_t)SYSTEM_STATE_STANDBY);
+ }
+}
+
+void update_state_machine_no_position_fix(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd)
+{
+ /* Depending on the current state switch state */
+ if (current_status->state_machine == SYSTEM_STATE_STANDBY || current_status->state_machine == SYSTEM_STATE_GROUND_READY || current_status->state_machine == SYSTEM_STATE_AUTO) {
+ state_machine_emergency(status_pub, current_status, mavlink_fd);
+ }
+}
+
+void update_state_machine_arm(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd)
+{
+ if (current_status->state_machine == SYSTEM_STATE_STANDBY) {
+ printf("[cmd] arming\n");
+ do_state_update(status_pub, current_status, mavlink_fd, (commander_state_machine_t)SYSTEM_STATE_GROUND_READY);
+ }
+}
+
+void update_state_machine_disarm(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd)
+{
+ if (current_status->state_machine == SYSTEM_STATE_GROUND_READY || current_status->state_machine == SYSTEM_STATE_MANUAL || current_status->state_machine == SYSTEM_STATE_PREFLIGHT) {
+ printf("[cmd] going standby\n");
+ do_state_update(status_pub, current_status, mavlink_fd, (commander_state_machine_t)SYSTEM_STATE_STANDBY);
+
+ } else if (current_status->state_machine == SYSTEM_STATE_STABILIZED || current_status->state_machine == SYSTEM_STATE_AUTO) {
+ printf("[cmd] MISSION ABORT!\n");
+ do_state_update(status_pub, current_status, mavlink_fd, (commander_state_machine_t)SYSTEM_STATE_STANDBY);
+ }
+}
+
+void update_state_machine_mode_manual(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd)
+{
+ int old_mode = current_status->flight_mode;
+ current_status->flight_mode = VEHICLE_FLIGHT_MODE_MANUAL;
+
+ current_status->flag_control_manual_enabled = true;
+
+ /* set behaviour based on airframe */
+ if ((current_status->system_type == VEHICLE_TYPE_QUADROTOR) ||
+ (current_status->system_type == VEHICLE_TYPE_HEXAROTOR) ||
+ (current_status->system_type == VEHICLE_TYPE_OCTOROTOR)) {
+
+ /* assuming a rotary wing, set to SAS */
+ current_status->manual_control_mode = VEHICLE_MANUAL_CONTROL_MODE_SAS;
+ current_status->flag_control_attitude_enabled = true;
+ current_status->flag_control_rates_enabled = true;
+
+ } else {
+
+ /* assuming a fixed wing, set to direct pass-through */
+ current_status->manual_control_mode = VEHICLE_MANUAL_CONTROL_MODE_DIRECT;
+ current_status->flag_control_attitude_enabled = false;
+ current_status->flag_control_rates_enabled = false;
+ }
+
+ if (old_mode != current_status->flight_mode) state_machine_publish(status_pub, current_status, mavlink_fd);
+
+ if (current_status->state_machine == SYSTEM_STATE_GROUND_READY || current_status->state_machine == SYSTEM_STATE_STABILIZED || current_status->state_machine == SYSTEM_STATE_AUTO) {
+ printf("[cmd] manual mode\n");
+ do_state_update(status_pub, current_status, mavlink_fd, (commander_state_machine_t)SYSTEM_STATE_MANUAL);
+ }
+}
+
+void update_state_machine_mode_stabilized(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd)
+{
+ if (current_status->state_machine == SYSTEM_STATE_GROUND_READY || current_status->state_machine == SYSTEM_STATE_STABILIZED || current_status->state_machine == SYSTEM_STATE_MANUAL || current_status->state_machine == SYSTEM_STATE_AUTO) {
+ int old_mode = current_status->flight_mode;
+ int old_manual_control_mode = current_status->manual_control_mode;
+ current_status->flight_mode = VEHICLE_FLIGHT_MODE_MANUAL;
+ current_status->manual_control_mode = VEHICLE_MANUAL_CONTROL_MODE_SAS;
+ current_status->flag_control_attitude_enabled = true;
+ current_status->flag_control_rates_enabled = true;
+ current_status->flag_control_manual_enabled = true;
+
+ if (old_mode != current_status->flight_mode ||
+ old_manual_control_mode != current_status->manual_control_mode) {
+ printf("[cmd] att stabilized mode\n");
+ do_state_update(status_pub, current_status, mavlink_fd, (commander_state_machine_t)SYSTEM_STATE_MANUAL);
+ state_machine_publish(status_pub, current_status, mavlink_fd);
+ }
+
+ }
+}
+
+void update_state_machine_mode_guided(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd)
+{
+ if (!current_status->flag_vector_flight_mode_ok) {
+ mavlink_log_critical(mavlink_fd, "NO POS LOCK, REJ. GUIDED MODE");
+ tune_error();
+ return;
+ }
+
+ if (current_status->state_machine == SYSTEM_STATE_GROUND_READY || current_status->state_machine == SYSTEM_STATE_MANUAL || current_status->state_machine == SYSTEM_STATE_AUTO) {
+ printf("[cmd] position guided mode\n");
+ int old_mode = current_status->flight_mode;
+ current_status->flight_mode = VEHICLE_FLIGHT_MODE_STAB;
+ current_status->flag_control_manual_enabled = false;
+ current_status->flag_control_attitude_enabled = true;
+ current_status->flag_control_rates_enabled = true;
+ do_state_update(status_pub, current_status, mavlink_fd, (commander_state_machine_t)SYSTEM_STATE_STABILIZED);
+
+ if (old_mode != current_status->flight_mode) state_machine_publish(status_pub, current_status, mavlink_fd);
+
+ }
+}
+
+void update_state_machine_mode_auto(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd)
+{
+ if (!current_status->flag_vector_flight_mode_ok) {
+ mavlink_log_critical(mavlink_fd, "NO POS LOCK, REJ. AUTO MODE");
+ return;
+ }
+
+ if (current_status->state_machine == SYSTEM_STATE_GROUND_READY || current_status->state_machine == SYSTEM_STATE_MANUAL || current_status->state_machine == SYSTEM_STATE_STABILIZED) {
+ printf("[cmd] auto mode\n");
+ int old_mode = current_status->flight_mode;
+ current_status->flight_mode = VEHICLE_FLIGHT_MODE_AUTO;
+ current_status->flag_control_manual_enabled = false;
+ current_status->flag_control_attitude_enabled = true;
+ current_status->flag_control_rates_enabled = true;
+ do_state_update(status_pub, current_status, mavlink_fd, (commander_state_machine_t)SYSTEM_STATE_AUTO);
+
+ if (old_mode != current_status->flight_mode) state_machine_publish(status_pub, current_status, mavlink_fd);
+ }
+}
+
+
+uint8_t update_state_machine_mode_request(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd, uint8_t mode)
+{
+ uint8_t ret = 1;
+
+ /* Switch on HIL if in standby and not already in HIL mode */
+ if ((mode & VEHICLE_MODE_FLAG_HIL_ENABLED)
+ && !current_status->flag_hil_enabled) {
+ if ((current_status->state_machine == SYSTEM_STATE_STANDBY)) {
+ /* Enable HIL on request */
+ current_status->flag_hil_enabled = true;
+ ret = OK;
+ state_machine_publish(status_pub, current_status, mavlink_fd);
+ publish_armed_status(current_status);
+ printf("[cmd] Enabling HIL, locking down all actuators for safety.\n\t(Arming the system will not activate them while in HIL mode)\n");
+
+ } else if (current_status->state_machine != SYSTEM_STATE_STANDBY &&
+ current_status->flag_system_armed) {
+
+ mavlink_log_critical(mavlink_fd, "REJECTING HIL, disarm first!")
+
+ } else {
+
+ mavlink_log_critical(mavlink_fd, "REJECTING HIL, not in standby.")
+ }
+ }
+
+ /* switch manual / auto */
+ if (mode & VEHICLE_MODE_FLAG_AUTO_ENABLED) {
+ update_state_machine_mode_auto(status_pub, current_status, mavlink_fd);
+
+ } else if (mode & VEHICLE_MODE_FLAG_STABILIZED_ENABLED) {
+ update_state_machine_mode_stabilized(status_pub, current_status, mavlink_fd);
+
+ } else if (mode & VEHICLE_MODE_FLAG_GUIDED_ENABLED) {
+ update_state_machine_mode_guided(status_pub, current_status, mavlink_fd);
+
+ } else if (mode & VEHICLE_MODE_FLAG_MANUAL_INPUT_ENABLED) {
+ update_state_machine_mode_manual(status_pub, current_status, mavlink_fd);
+ }
+
+ /* vehicle is disarmed, mode requests arming */
+ if (!(current_status->flag_system_armed) && (mode & VEHICLE_MODE_FLAG_SAFETY_ARMED)) {
+ /* only arm in standby state */
+ // XXX REMOVE
+ if (current_status->state_machine == SYSTEM_STATE_STANDBY || current_status->state_machine == SYSTEM_STATE_PREFLIGHT) {
+ do_state_update(status_pub, current_status, mavlink_fd, (commander_state_machine_t)SYSTEM_STATE_GROUND_READY);
+ ret = OK;
+ printf("[cmd] arming due to command request\n");
+ }
+ }
+
+ /* vehicle is armed, mode requests disarming */
+ if (current_status->flag_system_armed && !(mode & VEHICLE_MODE_FLAG_SAFETY_ARMED)) {
+ /* only disarm in ground ready */
+ if (current_status->state_machine == SYSTEM_STATE_GROUND_READY) {
+ do_state_update(status_pub, current_status, mavlink_fd, (commander_state_machine_t)SYSTEM_STATE_STANDBY);
+ ret = OK;
+ printf("[cmd] disarming due to command request\n");
+ }
+ }
+
+ /* NEVER actually switch off HIL without reboot */
+ if (current_status->flag_hil_enabled && !(mode & VEHICLE_MODE_FLAG_HIL_ENABLED)) {
+ warnx("DENYING request to switch off HIL. Please power cycle (safety reasons)\n");
+ mavlink_log_critical(mavlink_fd, "Power-cycle to exit HIL");
+ ret = ERROR;
+ }
+
+ return ret;
+}
+
+uint8_t update_state_machine_custom_mode_request(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd, uint8_t custom_mode) //TODO: add more checks to avoid state switching in critical situations
+{
+ commander_state_machine_t current_system_state = current_status->state_machine;
+
+ uint8_t ret = 1;
+
+ switch (custom_mode) {
+ case SYSTEM_STATE_GROUND_READY:
+ break;
+
+ case SYSTEM_STATE_STANDBY:
+ break;
+
+ case SYSTEM_STATE_REBOOT:
+ printf("try to reboot\n");
+
+ if (current_system_state == SYSTEM_STATE_STANDBY
+ || current_system_state == SYSTEM_STATE_PREFLIGHT
+ || current_status->flag_hil_enabled) {
+ printf("system will reboot\n");
+ mavlink_log_critical(mavlink_fd, "Rebooting..");
+ usleep(200000);
+ do_state_update(status_pub, current_status, mavlink_fd, (commander_state_machine_t)SYSTEM_STATE_REBOOT);
+ ret = 0;
+ }
+
+ break;
+
+ case SYSTEM_STATE_AUTO:
+ printf("try to switch to auto/takeoff\n");
+
+ if (current_system_state == SYSTEM_STATE_GROUND_READY || current_system_state == SYSTEM_STATE_MANUAL) {
+ do_state_update(status_pub, current_status, mavlink_fd, (commander_state_machine_t)SYSTEM_STATE_AUTO);
+ printf("state: auto\n");
+ ret = 0;
+ }
+
+ break;
+
+ case SYSTEM_STATE_MANUAL:
+ printf("try to switch to manual\n");
+
+ if (current_system_state == SYSTEM_STATE_GROUND_READY || current_system_state == SYSTEM_STATE_AUTO) {
+ do_state_update(status_pub, current_status, mavlink_fd, (commander_state_machine_t)SYSTEM_STATE_MANUAL);
+ printf("state: manual\n");
+ ret = 0;
+ }
+
+ break;
+
+ default:
+ break;
+ }
+
+ return ret;
+}
+