diff options
Diffstat (limited to 'src/modules/commander/commander.cpp')
-rw-r--r-- | src/modules/commander/commander.cpp | 80 |
1 files changed, 46 insertions, 34 deletions
diff --git a/src/modules/commander/commander.cpp b/src/modules/commander/commander.cpp index 0c4d48dea..2b528eef6 100644 --- a/src/modules/commander/commander.cpp +++ b/src/modules/commander/commander.cpp @@ -124,7 +124,7 @@ extern struct system_load_s system_load; #define STICK_ON_OFF_HYSTERESIS_TIME_MS 1000 #define STICK_ON_OFF_COUNTER_LIMIT (STICK_ON_OFF_HYSTERESIS_TIME_MS*COMMANDER_MONITORING_LOOPSPERMSEC) -#define POSITION_TIMEOUT (600 * 1000) /**< consider the local or global position estimate invalid after 600ms */ +#define POSITION_TIMEOUT (2 * 1000 * 1000) /**< consider the local or global position estimate invalid after 600ms */ #define FAILSAFE_DEFAULT_TIMEOUT (3 * 1000 * 1000) /**< hysteresis time - the failsafe will trigger after 3 seconds in this state */ #define RC_TIMEOUT 500000 #define DL_TIMEOUT 5 * 1000* 1000 @@ -163,7 +163,8 @@ static bool on_usb_power = false; static float takeoff_alt = 5.0f; static int parachute_enabled = 0; -static float eph_epv_threshold = 5.0f; +static float eph_threshold = 5.0f; +static float epv_threshold = 10.0f; static struct vehicle_status_s status; static struct actuator_armed_s armed; @@ -335,6 +336,7 @@ void print_status() { warnx("type: %s", (status.is_rotary_wing) ? "ROTARY" : "PLANE"); warnx("usb powered: %s", (on_usb_power) ? "yes" : "no"); + warnx("avionics rail: %6.2f V", (double)status.avionics_power_rail_voltage); /* read all relevant states */ int state_sub = orb_subscribe(ORB_ID(vehicle_status)); @@ -546,24 +548,19 @@ bool handle_command(struct vehicle_status_s *status_local, const struct safety_s } break; -#if 0 /* Flight termination */ - case VEHICLE_CMD_DO_SET_SERVO: { //xxx: needs its own mavlink command - - //XXX: to enable the parachute, a param needs to be set - //xxx: for safety only for now, param3 is unused by VEHICLE_CMD_DO_SET_SERVO - if (armed_local->armed && cmd->param3 > 0.5 && parachute_enabled) { - transition_result_t failsafe_res = failsafe_state_transition(status, FAILSAFE_STATE_TERMINATION); - cmd_result = VEHICLE_CMD_RESULT_ACCEPTED; - + case VEHICLE_CMD_DO_FLIGHTTERMINATION: { + if (cmd->param1 > 0.5f) { + //XXX update state machine? + armed_local->force_failsafe = true; + warnx("forcing failsafe"); } else { - /* reject parachute depoyment not armed */ - cmd_result = VEHICLE_CMD_RESULT_TEMPORARILY_REJECTED; + armed_local->force_failsafe = false; + warnx("disabling failsafe"); } - + cmd_result = VEHICLE_CMD_RESULT_ACCEPTED; } break; -#endif case VEHICLE_CMD_DO_SET_HOME: { bool use_current = cmd->param1 > 0.5f; @@ -741,6 +738,7 @@ int commander_thread_main(int argc, char *argv[]) // CIRCUIT BREAKERS status.circuit_breaker_engaged_power_check = false; + status.circuit_breaker_engaged_airspd_check = false; /* publish initial state */ status_pub = orb_advertise(ORB_ID(vehicle_status), &status); @@ -918,6 +916,11 @@ int commander_thread_main(int argc, char *argv[]) struct system_power_s system_power; memset(&system_power, 0, sizeof(system_power)); + /* Subscribe to actuator controls (outputs) */ + int actuator_controls_sub = orb_subscribe(ORB_ID_VEHICLE_ATTITUDE_CONTROLS); + struct actuator_controls_s actuator_controls; + memset(&actuator_controls, 0, sizeof(actuator_controls)); + control_status_leds(&status, &armed, true); /* now initialized */ @@ -977,6 +980,7 @@ int commander_thread_main(int argc, char *argv[]) param_get(_param_component_id, &(status.component_id)); status.circuit_breaker_engaged_power_check = circuit_breaker_enabled("CBRK_SUPPLY_CHK", CBRK_SUPPLY_CHK_KEY); + status.circuit_breaker_engaged_airspd_check = circuit_breaker_enabled("CBRK_AIRSPD_CHK", CBRK_AIRSPD_CHK_KEY); status_changed = true; @@ -1106,32 +1110,32 @@ int commander_thread_main(int argc, char *argv[]) /* update condition_global_position_valid */ /* hysteresis for EPH/EPV */ - bool eph_epv_good; + bool eph_good; if (status.condition_global_position_valid) { - if (global_position.eph > eph_epv_threshold * 2.0f || global_position.epv > eph_epv_threshold * 2.0f) { - eph_epv_good = false; + if (global_position.eph > eph_threshold * 2.5f) { + eph_good = false; } else { - eph_epv_good = true; + eph_good = true; } } else { - if (global_position.eph < eph_epv_threshold && global_position.epv < eph_epv_threshold) { - eph_epv_good = true; + if (global_position.eph < eph_threshold) { + eph_good = true; } else { - eph_epv_good = false; + eph_good = false; } } - check_valid(global_position.timestamp, POSITION_TIMEOUT, eph_epv_good, &(status.condition_global_position_valid), &status_changed); + check_valid(global_position.timestamp, POSITION_TIMEOUT, eph_good, &(status.condition_global_position_valid), &status_changed); /* check if GPS fix is ok */ /* update home position */ if (!status.condition_home_position_valid && status.condition_global_position_valid && !armed.armed && - (global_position.eph < eph_epv_threshold) && (global_position.epv < eph_epv_threshold)) { + (global_position.eph < eph_threshold) && (global_position.epv < epv_threshold)) { home.lat = global_position.lat; home.lon = global_position.lon; @@ -1161,8 +1165,8 @@ int commander_thread_main(int argc, char *argv[]) /* hysteresis for EPH */ bool local_eph_good; - if (status.condition_global_position_valid) { - if (local_position.eph > eph_epv_threshold * 2.0f) { + if (status.condition_local_position_valid) { + if (local_position.eph > eph_threshold * 2.5f) { local_eph_good = false; } else { @@ -1170,7 +1174,7 @@ int commander_thread_main(int argc, char *argv[]) } } else { - if (local_position.eph < eph_epv_threshold) { + if (local_position.eph < eph_threshold) { local_eph_good = true; } else { @@ -1199,13 +1203,17 @@ int commander_thread_main(int argc, char *argv[]) if (updated) { orb_copy(ORB_ID(battery_status), battery_sub, &battery); + orb_copy(ORB_ID_VEHICLE_ATTITUDE_CONTROLS, actuator_controls_sub, &actuator_controls); /* only consider battery voltage if system has been running 2s and battery voltage is valid */ if (hrt_absolute_time() > start_time + 2000000 && battery.voltage_filtered_v > 0.0f) { status.battery_voltage = battery.voltage_filtered_v; status.battery_current = battery.current_a; status.condition_battery_voltage_valid = true; - status.battery_remaining = battery_remaining_estimate_voltage(battery.voltage_filtered_v, battery.discharged_mah); + + /* get throttle (if armed), as we only care about energy negative throttle also counts */ + float throttle = (armed.armed) ? fabsf(actuator_controls.control[3]) : 0.0f; + status.battery_remaining = battery_remaining_estimate_voltage(battery.voltage_filtered_v, battery.discharged_mah, throttle); } } @@ -1267,13 +1275,13 @@ int commander_thread_main(int argc, char *argv[]) } /* if battery voltage is getting lower, warn using buzzer, etc. */ - if (status.condition_battery_voltage_valid && status.battery_remaining < 0.25f && !low_battery_voltage_actions_done) { + if (status.condition_battery_voltage_valid && status.battery_remaining < 0.18f && !low_battery_voltage_actions_done) { low_battery_voltage_actions_done = true; mavlink_log_critical(mavlink_fd, "LOW BATTERY, RETURN TO LAND ADVISED"); status.battery_warning = VEHICLE_BATTERY_WARNING_LOW; status_changed = true; - } else if (status.condition_battery_voltage_valid && status.battery_remaining < 0.1f && !critical_battery_voltage_actions_done && low_battery_voltage_actions_done) { + } else if (status.condition_battery_voltage_valid && status.battery_remaining < 0.09f && !critical_battery_voltage_actions_done && low_battery_voltage_actions_done) { /* critical battery voltage, this is rather an emergency, change state machine */ critical_battery_voltage_actions_done = true; mavlink_log_emergency(mavlink_fd, "CRITICAL BATTERY, LAND IMMEDIATELY"); @@ -1412,8 +1420,12 @@ int commander_thread_main(int argc, char *argv[]) arming_state_changed = true; } else if (arming_ret == TRANSITION_DENIED) { - /* DENIED here indicates bug in the commander */ - mavlink_log_critical(mavlink_fd, "arming state transition denied"); + /* + * the arming transition can be denied to a number of reasons: + * - pre-flight check failed (sensors not ok or not calibrated) + * - safety not disabled + * - system not in manual mode + */ tune_negative(true); } @@ -1441,7 +1453,7 @@ int commander_thread_main(int argc, char *argv[]) /* data links check */ bool have_link = false; for (int i = 0; i < TELEMETRY_STATUS_ORB_ID_NUM; i++) { - if (hrt_elapsed_time(&telemetry_last_heartbeat[i]) < DL_TIMEOUT) { + if (telemetry_last_heartbeat[i] != 0 && hrt_elapsed_time(&telemetry_last_heartbeat[i]) < DL_TIMEOUT) { /* handle the case where data link was regained */ if (telemetry_lost[i]) { mavlink_log_critical(mavlink_fd, "data link %i regained", i); @@ -1494,7 +1506,7 @@ int commander_thread_main(int argc, char *argv[]) /* update home position on arming if at least 2s from commander start spent to avoid setting home on in-air restart */ if (armed.armed && !was_armed && hrt_absolute_time() > start_time + 2000000 && status.condition_global_position_valid && - (global_position.eph < eph_epv_threshold) && (global_position.epv < eph_epv_threshold)) { + (global_position.eph < eph_threshold) && (global_position.epv < epv_threshold)) { // TODO remove code duplication home.lat = global_position.lat; |