commander state machine helper pass battery and safety as const references

This commit is contained in:
Daniel Agar
2018-03-27 16:27:47 -04:00
parent 4ccfc280c8
commit db7e8635a2
4 changed files with 48 additions and 98 deletions
+21 -70
View File
@@ -410,10 +410,10 @@ int commander_main(int argc, char *argv[])
if (!strcmp(argv[1], "check")) {
int checkres = 0;
checkres = prearm_check(&status, &mavlink_log_pub, false, true, &status_flags, &battery, ARM_REQ_GPS_BIT, hrt_elapsed_time(&commander_boot_timestamp));
checkres = prearm_check(&mavlink_log_pub, false, true, &status_flags, battery, ARM_REQ_GPS_BIT, hrt_elapsed_time(&commander_boot_timestamp));
warnx("Preflight check: %s", (checkres == 0) ? "OK" : "FAILED");
checkres = prearm_check(&status, &mavlink_log_pub, true, true, &status_flags, &battery, arm_requirements, hrt_elapsed_time(&commander_boot_timestamp));
checkres = prearm_check(&mavlink_log_pub, true, true, &status_flags, battery, arm_requirements, hrt_elapsed_time(&commander_boot_timestamp));
warnx("Prearm check: %s", (checkres == 0) ? "OK" : "FAILED");
return 0;
@@ -622,8 +622,8 @@ transition_result_t arm_disarm(bool arm, orb_advert_t *mavlink_log_pub_local, co
// Transition the armed state. By passing mavlink_log_pub to arming_state_transition it will
// output appropriate error messages if the state cannot transition.
arming_res = arming_state_transition(&status,
&battery,
&safety,
battery,
safety,
arm ? vehicle_status_s::ARMING_STATE_ARMED : vehicle_status_s::ARMING_STATE_STANDBY,
&armed,
true /* fRunPreArmChecks */,
@@ -1854,17 +1854,10 @@ Commander::run()
arming_state_t new_arming_state = (status.arming_state == vehicle_status_s::ARMING_STATE_ARMED ? vehicle_status_s::ARMING_STATE_STANDBY :
vehicle_status_s::ARMING_STATE_STANDBY_ERROR);
if (TRANSITION_CHANGED == arming_state_transition(&status,
&battery,
&safety,
new_arming_state,
&armed,
true /* fRunPreArmChecks */,
&mavlink_log_pub,
&status_flags,
avionics_power_rail_voltage,
arm_requirements,
hrt_elapsed_time(&commander_boot_timestamp))) {
if (TRANSITION_CHANGED == arming_state_transition(&status, battery, safety, new_arming_state, &armed, true /* fRunPreArmChecks */, &mavlink_log_pub,
&status_flags, avionics_power_rail_voltage, arm_requirements, hrt_elapsed_time(&commander_boot_timestamp))
) {
status_changed = true;
}
}
@@ -2223,17 +2216,10 @@ Commander::run()
/* If in INIT state, try to proceed to STANDBY state */
if (!status_flags.condition_calibration_enabled && status.arming_state == vehicle_status_s::ARMING_STATE_INIT) {
arming_ret = arming_state_transition(&status,
&battery,
&safety,
vehicle_status_s::ARMING_STATE_STANDBY,
&armed,
true /* fRunPreArmChecks */,
&mavlink_log_pub,
&status_flags,
avionics_power_rail_voltage,
arm_requirements,
hrt_elapsed_time(&commander_boot_timestamp));
arming_ret = arming_state_transition(&status, battery, safety, vehicle_status_s::ARMING_STATE_STANDBY, &armed,
true /* fRunPreArmChecks */, &mavlink_log_pub, &status_flags, avionics_power_rail_voltage,
arm_requirements, hrt_elapsed_time(&commander_boot_timestamp));
if (arming_ret == TRANSITION_DENIED) {
/* do not complain if not allowed into standby */
@@ -2453,17 +2439,8 @@ Commander::run()
print_reject_arm("NOT DISARMING: Not in manual mode or landed yet.");
} else if ((stick_off_counter == rc_arm_hyst && stick_on_counter < rc_arm_hyst) || arm_switch_to_disarm_transition) {
arming_ret = arming_state_transition(&status,
&battery,
&safety,
vehicle_status_s::ARMING_STATE_STANDBY,
&armed,
true /* fRunPreArmChecks */,
&mavlink_log_pub,
&status_flags,
avionics_power_rail_voltage,
arm_requirements,
hrt_elapsed_time(&commander_boot_timestamp));
arming_ret = arming_state_transition(&status, battery, safety, vehicle_status_s::ARMING_STATE_STANDBY, &armed, true /* fRunPreArmChecks */,
&mavlink_log_pub, &status_flags, avionics_power_rail_voltage, arm_requirements, hrt_elapsed_time(&commander_boot_timestamp));
}
stick_off_counter++;
/* do not reset the counter when holding the arm button longer than needed */
@@ -2503,17 +2480,8 @@ Commander::run()
print_reject_arm("NOT ARMING: Geofence RTL requires valid home");
} else if (status.arming_state == vehicle_status_s::ARMING_STATE_STANDBY) {
arming_ret = arming_state_transition(&status,
&battery,
&safety,
vehicle_status_s::ARMING_STATE_ARMED,
&armed,
true /* fRunPreArmChecks */,
&mavlink_log_pub,
&status_flags,
avionics_power_rail_voltage,
arm_requirements,
hrt_elapsed_time(&commander_boot_timestamp));
arming_ret = arming_state_transition(&status, battery, safety, vehicle_status_s::ARMING_STATE_ARMED, &armed, true /* fRunPreArmChecks */,
&mavlink_log_pub, &status_flags, avionics_power_rail_voltage, arm_requirements, hrt_elapsed_time(&commander_boot_timestamp));
if (arming_ret != TRANSITION_CHANGED) {
usleep(100000);
@@ -4010,17 +3978,9 @@ void *commander_low_prio_loop(void *arg)
int calib_ret = PX4_ERROR;
/* try to go to INIT/PREFLIGHT arming state */
if (TRANSITION_DENIED == arming_state_transition(&status,
&battery,
&safety,
vehicle_status_s::ARMING_STATE_INIT,
&armed,
false /* fRunPreArmChecks */,
&mavlink_log_pub,
&status_flags,
avionics_power_rail_voltage,
arm_requirements,
hrt_elapsed_time(&commander_boot_timestamp))) {
if (TRANSITION_DENIED == arming_state_transition(&status, battery, safety, vehicle_status_s::ARMING_STATE_INIT, &armed,
false /* fRunPreArmChecks */, &mavlink_log_pub, &status_flags, avionics_power_rail_voltage,
arm_requirements, hrt_elapsed_time(&commander_boot_timestamp))) {
answer_command(cmd, vehicle_command_s::VEHICLE_CMD_RESULT_DENIED, command_ack_pub);
break;
@@ -4117,17 +4077,8 @@ void *commander_low_prio_loop(void *arg)
!(status.rc_input_mode >= vehicle_status_s::RC_IN_MODE_OFF), arm_requirements & ARM_REQ_GPS_BIT,
true, is_vtol(&status), hotplug_timeout, false, hrt_elapsed_time(&commander_boot_timestamp));
arming_state_transition(&status,
&battery,
&safety,
vehicle_status_s::ARMING_STATE_STANDBY,
&armed,
false /* fRunPreArmChecks */,
&mavlink_log_pub,
&status_flags,
avionics_power_rail_voltage,
arm_requirements,
hrt_elapsed_time(&commander_boot_timestamp));
arming_state_transition(&status, battery, safety, vehicle_status_s::ARMING_STATE_STANDBY, &armed, false /* fRunPreArmChecks */,
&mavlink_log_pub, &status_flags, avionics_power_rail_voltage, arm_requirements, hrt_elapsed_time(&commander_boot_timestamp));
} else {
tune_negative(true);