/**************************************************************************** * * Copyright (C) 2012 PX4 Development Team. All rights reserved. * Author: Thomas Gubler * Julian Oes * * 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 #include #include #include #include #include #include #include #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; fprintf(stderr, "[cmd] EMERGENCY LANDING!\n"); mavlink_log_critical(mavlink_fd, "[cmd] 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; fprintf(stderr, "[cmd] EMERGENCY MOTOR CUTOFF!\n"); mavlink_log_critical(mavlink_fd, "[cmd] 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; fprintf(stderr, "[cmd] GROUND ERROR, locking down propulsion system\n"); mavlink_log_critical(mavlink_fd, "[cmd] GROUND ERROR, locking down propulsion 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, "[cmd] Switched to PREFLIGHT state"); } else { invalid_state = true; mavlink_log_critical(mavlink_fd, "[cmd] 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) { invalid_state = false; /* set system flags according to state */ current_status->flag_system_armed = false; mavlink_log_critical(mavlink_fd, "[cmd] REBOOTING SYSTEM"); usleep(500000); up_systemreset(); /* SPECIAL CASE: NEVER RETURNS FROM THIS FUNCTION CALL */ } else { invalid_state = true; mavlink_log_critical(mavlink_fd, "[cmd] 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, "[cmd] 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, "[cmd] 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, "[cmd] 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, "[cmd] 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, "[cmd] 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, "[cmd] 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) { fprintf(stderr, "[cmd] 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 { fprintf(stderr, "[cmd] 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; /* enable attitude control per default */ current_status->flag_control_attitude_enabled = true; current_status->flag_control_rates_enabled = true; 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->flag_vector_flight_mode_ok) { mavlink_log_critical(mavlink_fd, "NO POS LOCK, REJ. STAB MODE"); 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] stabilized 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_hold(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. HOLD MODE"); 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] stabilized mode\n"); int old_mode = current_status->flight_mode; current_status->flight_mode = VEHICLE_FLIGHT_MODE_HOLD; 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, "[cmd] REJECTING HIL, disarm first!") } else { mavlink_log_critical(mavlink_fd, "[cmd] 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_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)) { fprintf(stderr, "[cmd] DENYING request to switch off HIL. Please power cycle (safety reasons)\n"); mavlink_log_critical(mavlink_fd, "[cmd] 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) { printf("system will reboot\n"); mavlink_log_critical(mavlink_fd, "[cmd] 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; }