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+/****************************************************************************
+ *
+ * Copyright (C) 2013 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.cpp
+ * State machine helper functions implementations
+ */
+
+#include <stdio.h>
+#include <unistd.h>
+#include <stdint.h>
+#include <stdbool.h>
+
+#include <uORB/uORB.h>
+#include <uORB/topics/vehicle_status.h>
+#include <uORB/topics/actuator_controls.h>
+#include <uORB/topics/vehicle_control_mode.h>
+#include <systemlib/systemlib.h>
+#include <systemlib/param/param.h>
+#include <systemlib/err.h>
+#include <drivers/drv_hrt.h>
+#include <mavlink/mavlink_log.h>
+
+#include "state_machine_helper.h"
+#include "commander_helper.h"
+
+/* oddly, ERROR is not defined for c++ */
+#ifdef ERROR
+# undef ERROR
+#endif
+static const int ERROR = -1;
+
+static bool arming_state_changed = true;
+static bool main_state_changed = true;
+static bool navigation_state_changed = true;
+
+transition_result_t
+arming_state_transition(struct vehicle_status_s *status, const struct safety_s *safety, arming_state_t new_arming_state, struct actuator_armed_s *armed)
+{
+ transition_result_t ret = TRANSITION_DENIED;
+
+ /* only check transition if the new state is actually different from the current one */
+ if (new_arming_state == status->arming_state) {
+ ret = TRANSITION_NOT_CHANGED;
+
+ } else {
+
+ switch (new_arming_state) {
+ case ARMING_STATE_INIT:
+
+ /* allow going back from INIT for calibration */
+ if (status->arming_state == ARMING_STATE_STANDBY) {
+ ret = TRANSITION_CHANGED;
+ armed->armed = false;
+ armed->ready_to_arm = false;
+ }
+
+ break;
+
+ case ARMING_STATE_STANDBY:
+
+ /* allow coming from INIT and disarming from ARMED */
+ if (status->arming_state == ARMING_STATE_INIT
+ || status->arming_state == ARMING_STATE_ARMED) {
+
+ /* sensors need to be initialized for STANDBY state */
+ if (status->condition_system_sensors_initialized) {
+ ret = TRANSITION_CHANGED;
+ armed->armed = false;
+ armed->ready_to_arm = true;
+ }
+ }
+
+ break;
+
+ case ARMING_STATE_ARMED:
+
+ /* allow arming from STANDBY and IN-AIR-RESTORE */
+ if ((status->arming_state == ARMING_STATE_STANDBY
+ || status->arming_state == ARMING_STATE_IN_AIR_RESTORE)
+ && (!safety->safety_switch_available || safety->safety_off)) /* only allow arming if safety is off */
+ {
+ ret = TRANSITION_CHANGED;
+ armed->armed = true;
+ armed->ready_to_arm = false;
+ }
+
+ break;
+
+ case ARMING_STATE_ARMED_ERROR:
+
+ /* an armed error happens when ARMED obviously */
+ if (status->arming_state == ARMING_STATE_ARMED) {
+ ret = TRANSITION_CHANGED;
+ armed->armed = true;
+ armed->ready_to_arm = false;
+ }
+
+ break;
+
+ case ARMING_STATE_STANDBY_ERROR:
+
+ /* a disarmed error happens when in STANDBY or in INIT or after ARMED_ERROR */
+ if (status->arming_state == ARMING_STATE_STANDBY
+ || status->arming_state == ARMING_STATE_INIT
+ || status->arming_state == ARMING_STATE_ARMED_ERROR) {
+ ret = TRANSITION_CHANGED;
+ armed->armed = false;
+ armed->ready_to_arm = false;
+ }
+
+ break;
+
+ case ARMING_STATE_REBOOT:
+
+ /* an armed error happens when ARMED obviously */
+ if (status->arming_state == ARMING_STATE_INIT
+ || status->arming_state == ARMING_STATE_STANDBY
+ || status->arming_state == ARMING_STATE_STANDBY_ERROR) {
+ ret = TRANSITION_CHANGED;
+ armed->armed = false;
+ armed->ready_to_arm = false;
+ }
+
+ break;
+
+ case ARMING_STATE_IN_AIR_RESTORE:
+
+ /* XXX implement */
+ break;
+
+ default:
+ break;
+ }
+
+ if (ret == TRANSITION_CHANGED) {
+ status->arming_state = new_arming_state;
+ arming_state_changed = true;
+ }
+ }
+
+ return ret;
+}
+
+bool is_safe(const struct vehicle_status_s *current_state, const struct safety_s *safety, const struct actuator_armed_s *armed)
+{
+ // System is safe if:
+ // 1) Not armed
+ // 2) Armed, but in software lockdown (HIL)
+ // 3) Safety switch is present AND engaged -> actuators locked
+ if (!armed->armed || (armed->armed && armed->lockdown) || (safety->safety_switch_available && !safety->safety_off)) {
+ return true;
+ } else {
+ return false;
+ }
+}
+
+bool
+check_arming_state_changed()
+{
+ if (arming_state_changed) {
+ arming_state_changed = false;
+ return true;
+
+ } else {
+ return false;
+ }
+}
+
+transition_result_t
+main_state_transition(struct vehicle_status_s *current_state, main_state_t new_main_state)
+{
+ transition_result_t ret = TRANSITION_DENIED;
+
+ /* only check transition if the new state is actually different from the current one */
+ if (new_main_state == current_state->main_state) {
+ ret = TRANSITION_NOT_CHANGED;
+
+ } else {
+
+ switch (new_main_state) {
+ case MAIN_STATE_MANUAL:
+ ret = TRANSITION_CHANGED;
+ break;
+
+ case MAIN_STATE_SEATBELT:
+
+ /* need position estimate */
+ // TODO only need altitude estimate really
+ if (current_state->condition_local_position_valid) {
+ ret = TRANSITION_CHANGED;
+ }
+
+ break;
+
+ case MAIN_STATE_EASY:
+
+ /* need position estimate */
+ if (current_state->condition_local_position_valid) {
+ ret = TRANSITION_CHANGED;
+ }
+
+ break;
+
+ case MAIN_STATE_AUTO:
+
+ /* need position estimate */
+ if (current_state->condition_local_position_valid) {
+ ret = TRANSITION_CHANGED;
+ }
+
+ break;
+ }
+
+ if (ret == TRANSITION_CHANGED) {
+ current_state->main_state = new_main_state;
+ main_state_changed = true;
+ }
+ }
+
+ return ret;
+}
+
+bool
+check_main_state_changed()
+{
+ if (main_state_changed) {
+ main_state_changed = false;
+ return true;
+
+ } else {
+ return false;
+ }
+}
+
+transition_result_t
+navigation_state_transition(struct vehicle_status_s *current_status, navigation_state_t new_navigation_state, struct vehicle_control_mode_s *control_mode)
+{
+ transition_result_t ret = TRANSITION_DENIED;
+
+ /* only check transition if the new state is actually different from the current one */
+ if (new_navigation_state == current_status->navigation_state) {
+ ret = TRANSITION_NOT_CHANGED;
+
+ } else {
+
+ switch (new_navigation_state) {
+ case NAVIGATION_STATE_STANDBY:
+ ret = TRANSITION_CHANGED;
+ control_mode->flag_control_rates_enabled = false;
+ control_mode->flag_control_attitude_enabled = false;
+ control_mode->flag_control_velocity_enabled = false;
+ control_mode->flag_control_position_enabled = false;
+ control_mode->flag_control_altitude_enabled = false;
+ control_mode->flag_control_manual_enabled = false;
+ break;
+
+ case NAVIGATION_STATE_DIRECT:
+ ret = TRANSITION_CHANGED;
+ control_mode->flag_control_rates_enabled = true;
+ control_mode->flag_control_attitude_enabled = false;
+ control_mode->flag_control_velocity_enabled = false;
+ control_mode->flag_control_position_enabled = false;
+ control_mode->flag_control_altitude_enabled = false;
+ control_mode->flag_control_manual_enabled = true;
+ break;
+
+ case NAVIGATION_STATE_STABILIZE:
+ ret = TRANSITION_CHANGED;
+ control_mode->flag_control_rates_enabled = true;
+ control_mode->flag_control_attitude_enabled = true;
+ control_mode->flag_control_velocity_enabled = false;
+ control_mode->flag_control_position_enabled = false;
+ control_mode->flag_control_altitude_enabled = false;
+ control_mode->flag_control_manual_enabled = true;
+ break;
+
+ case NAVIGATION_STATE_ALTHOLD:
+ ret = TRANSITION_CHANGED;
+ control_mode->flag_control_rates_enabled = true;
+ control_mode->flag_control_attitude_enabled = true;
+ control_mode->flag_control_velocity_enabled = false;
+ control_mode->flag_control_position_enabled = false;
+ control_mode->flag_control_altitude_enabled = true;
+ control_mode->flag_control_manual_enabled = true;
+ break;
+
+ case NAVIGATION_STATE_VECTOR:
+ ret = TRANSITION_CHANGED;
+ control_mode->flag_control_rates_enabled = true;
+ control_mode->flag_control_attitude_enabled = true;
+ control_mode->flag_control_velocity_enabled = true;
+ control_mode->flag_control_position_enabled = true;
+ control_mode->flag_control_altitude_enabled = true;
+ control_mode->flag_control_manual_enabled = true;
+ break;
+
+ case NAVIGATION_STATE_AUTO_READY:
+ ret = TRANSITION_CHANGED;
+ control_mode->flag_control_rates_enabled = true;
+ control_mode->flag_control_attitude_enabled = true;
+ control_mode->flag_control_velocity_enabled = true;
+ control_mode->flag_control_position_enabled = true;
+ control_mode->flag_control_altitude_enabled = true;
+ control_mode->flag_control_manual_enabled = false;
+ break;
+
+ case NAVIGATION_STATE_AUTO_TAKEOFF:
+
+ /* only transitions from AUTO_READY */
+ if (current_status->navigation_state != NAVIGATION_STATE_AUTO_READY) {
+ ret = TRANSITION_CHANGED;
+ control_mode->flag_control_rates_enabled = true;
+ control_mode->flag_control_attitude_enabled = true;
+ control_mode->flag_control_velocity_enabled = true;
+ control_mode->flag_control_position_enabled = true;
+ control_mode->flag_control_altitude_enabled = true;
+ control_mode->flag_control_manual_enabled = false;
+ }
+
+ break;
+
+ case NAVIGATION_STATE_AUTO_LOITER:
+
+ /* deny transitions from landed states */
+ if (current_status->navigation_state != NAVIGATION_STATE_STANDBY &&
+ current_status->navigation_state != NAVIGATION_STATE_AUTO_READY) {
+ ret = TRANSITION_CHANGED;
+ control_mode->flag_control_rates_enabled = true;
+ control_mode->flag_control_attitude_enabled = true;
+ control_mode->flag_control_velocity_enabled = true;
+ control_mode->flag_control_position_enabled = true;
+ control_mode->flag_control_altitude_enabled = true;
+ control_mode->flag_control_manual_enabled = false;
+ }
+
+ break;
+
+ case NAVIGATION_STATE_AUTO_MISSION:
+
+ /* deny transitions from landed states */
+ if (current_status->navigation_state != NAVIGATION_STATE_STANDBY &&
+ current_status->navigation_state != NAVIGATION_STATE_AUTO_READY) {
+ ret = TRANSITION_CHANGED;
+ control_mode->flag_control_rates_enabled = true;
+ control_mode->flag_control_attitude_enabled = true;
+ control_mode->flag_control_velocity_enabled = true;
+ control_mode->flag_control_position_enabled = true;
+ control_mode->flag_control_altitude_enabled = true;
+ control_mode->flag_control_manual_enabled = false;
+ }
+
+ break;
+
+ case NAVIGATION_STATE_AUTO_RTL:
+
+ /* deny transitions from landed states */
+ if (current_status->navigation_state != NAVIGATION_STATE_STANDBY &&
+ current_status->navigation_state != NAVIGATION_STATE_AUTO_READY) {
+ ret = TRANSITION_CHANGED;
+ control_mode->flag_control_rates_enabled = true;
+ control_mode->flag_control_attitude_enabled = true;
+ control_mode->flag_control_velocity_enabled = true;
+ control_mode->flag_control_position_enabled = true;
+ control_mode->flag_control_altitude_enabled = true;
+ control_mode->flag_control_manual_enabled = false;
+ }
+
+ break;
+
+ case NAVIGATION_STATE_AUTO_LAND:
+
+ /* deny transitions from landed states */
+ if (current_status->navigation_state != NAVIGATION_STATE_STANDBY &&
+ current_status->navigation_state != NAVIGATION_STATE_AUTO_READY) {
+ ret = TRANSITION_CHANGED;
+ control_mode->flag_control_rates_enabled = true;
+ control_mode->flag_control_attitude_enabled = true;
+ control_mode->flag_control_velocity_enabled = true;
+ control_mode->flag_control_position_enabled = true;
+ control_mode->flag_control_altitude_enabled = true;
+ control_mode->flag_control_manual_enabled = false;
+ }
+
+ break;
+
+ default:
+ break;
+ }
+
+ if (ret == TRANSITION_CHANGED) {
+ current_status->navigation_state = new_navigation_state;
+ navigation_state_changed = true;
+ }
+ }
+
+ return ret;
+}
+
+bool
+check_navigation_state_changed()
+{
+ if (navigation_state_changed) {
+ navigation_state_changed = false;
+ return true;
+
+ } else {
+ return false;
+ }
+}
+
+/**
+* Transition from one hil state to another
+*/
+int hil_state_transition(hil_state_t new_state, int status_pub, struct vehicle_status_s *current_status, int control_mode_pub, struct vehicle_control_mode_s *current_control_mode, const int mavlink_fd)
+{
+ bool valid_transition = false;
+ int ret = ERROR;
+
+ warnx("Current state: %d, requested state: %d", current_status->hil_state, new_state);
+
+ if (current_status->hil_state == new_state) {
+ warnx("Hil state not changed");
+ valid_transition = true;
+
+ } else {
+
+ switch (new_state) {
+
+ case HIL_STATE_OFF:
+
+ if (current_status->arming_state == ARMING_STATE_INIT
+ || current_status->arming_state == ARMING_STATE_STANDBY) {
+
+ current_control_mode->flag_system_hil_enabled = false;
+ mavlink_log_critical(mavlink_fd, "Switched to OFF hil state");
+ valid_transition = true;
+ }
+
+ break;
+
+ case HIL_STATE_ON:
+
+ if (current_status->arming_state == ARMING_STATE_INIT
+ || current_status->arming_state == ARMING_STATE_STANDBY) {
+
+ current_control_mode->flag_system_hil_enabled = true;
+ mavlink_log_critical(mavlink_fd, "Switched to ON hil state");
+ valid_transition = true;
+ }
+
+ break;
+
+ default:
+ warnx("Unknown hil state");
+ break;
+ }
+ }
+
+ if (valid_transition) {
+ current_status->hil_state = new_state;
+
+ current_status->counter++;
+ current_status->timestamp = hrt_absolute_time();
+ orb_publish(ORB_ID(vehicle_status), status_pub, current_status);
+
+ current_control_mode->timestamp = hrt_absolute_time();
+ orb_publish(ORB_ID(vehicle_control_mode), control_mode_pub, current_control_mode);
+
+ ret = OK;
+
+ } else {
+ mavlink_log_critical(mavlink_fd, "REJECTING invalid hil state transition");
+ }
+
+ return ret;
+}
+
+
+
+// /*
+// * 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;
+// }
+
+// }
+
+
+///* END SUBSYSTEM/EMERGENCY FUNCTIONS*/
+//
+//int update_state_machine_mode_request(int status_pub, struct vehicle_status_s *current_status, const int mavlink_fd, uint8_t mode)
+//{
+// int 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_fmu_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_fmu_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_fmu_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;
+//}
+