ardupilot/ArduPlane/AP_Arming.cpp

239 lines
7.0 KiB
C++

/*
additional arming checks for plane
*/
#include "AP_Arming.h"
#include "Plane.h"
const AP_Param::GroupInfo AP_Arming_Plane::var_info[] = {
// variables from parent vehicle
AP_NESTEDGROUPINFO(AP_Arming, 0),
// index 3 was RUDDER and should not be used
AP_GROUPEND
};
/*
additional arming checks for plane
*/
bool AP_Arming_Plane::pre_arm_checks(bool display_failure)
{
//are arming checks disabled?
if (checks_to_perform == 0) {
return true;
}
if (hal.util->was_watchdog_armed()) {
// on watchdog reset bypass arming checks to allow for
// in-flight arming if we were armed before the reset. This
// allows a reset on a BVLOS flight to return home if the
// operator can command arming over telemetry
return true;
}
// call parent class checks
bool ret = AP_Arming::pre_arm_checks(display_failure);
// Check airspeed sensor
ret &= AP_Arming::airspeed_checks(display_failure);
if (plane.g.fs_timeout_long < plane.g.fs_timeout_short && plane.g.fs_action_short != FS_ACTION_SHORT_DISABLED) {
check_failed(display_failure, "FS_LONG_TIMEOUT < FS_SHORT_TIMEOUT");
ret = false;
}
if (plane.aparm.roll_limit_cd < 300) {
check_failed(display_failure, "LIM_ROLL_CD too small (%u)", (unsigned)plane.aparm.roll_limit_cd);
ret = false;
}
if (plane.aparm.pitch_limit_max_cd < 300) {
check_failed(display_failure, "LIM_PITCH_MAX too small (%u)", (unsigned)plane.aparm.pitch_limit_max_cd);
ret = false;
}
if (plane.aparm.pitch_limit_min_cd > -300) {
check_failed(display_failure, "LIM_PITCH_MIN too large (%u)", (unsigned)plane.aparm.pitch_limit_min_cd);
ret = false;
}
if (plane.channel_throttle->get_reverse() &&
plane.g.throttle_fs_enabled &&
plane.g.throttle_fs_value <
plane.channel_throttle->get_radio_max()) {
check_failed(display_failure, "Invalid THR_FS_VALUE for rev throttle");
ret = false;
}
if (plane.quadplane.enabled() && !plane.quadplane.available()) {
check_failed(display_failure, "Quadplane enabled but not running");
ret = false;
}
if (plane.quadplane.available() && plane.scheduler.get_loop_rate_hz() < 100) {
check_failed(display_failure, "quadplane needs SCHED_LOOP_RATE >= 100");
ret = false;
}
if (plane.quadplane.enabled() && plane.quadplane.available()) {
// ensure controllers are OK with us arming:
char failure_msg[50];
if (!plane.quadplane.pos_control->pre_arm_checks("PSC", failure_msg, ARRAY_SIZE(failure_msg))) {
check_failed(ARMING_CHECK_PARAMETERS, display_failure, "Bad parameter: %s", failure_msg);
return false;
}
if (!plane.quadplane.attitude_control->pre_arm_checks("ATC", failure_msg, ARRAY_SIZE(failure_msg))) {
check_failed(ARMING_CHECK_PARAMETERS, display_failure, "Bad parameter: %s", failure_msg);
return false;
}
}
if (plane.control_mode == &plane.mode_auto && plane.mission.num_commands() <= 1) {
check_failed(display_failure, "No mission loaded");
ret = false;
}
// check adsb avoidance failsafe
if (plane.failsafe.adsb) {
check_failed(display_failure, "ADSB threat detected");
ret = false;
}
if (SRV_Channels::get_emergency_stop()) {
check_failed(display_failure,"Motors Emergency Stopped");
ret = false;
}
return ret;
}
bool AP_Arming_Plane::ins_checks(bool display_failure)
{
// call parent class checks
if (!AP_Arming::ins_checks(display_failure)) {
return false;
}
// additional plane specific checks
if ((checks_to_perform & ARMING_CHECK_ALL) ||
(checks_to_perform & ARMING_CHECK_INS)) {
if (!AP::ahrs().prearm_healthy()) {
const char *reason = AP::ahrs().prearm_failure_reason();
if (reason == nullptr) {
reason = "AHRS not healthy";
}
check_failed(ARMING_CHECK_INS, display_failure, "%s", reason);
return false;
}
}
return true;
}
bool AP_Arming_Plane::arm_checks(AP_Arming::Method method)
{
//are arming checks disabled?
if (checks_to_perform == 0) {
return true;
}
if (hal.util->was_watchdog_armed()) {
// on watchdog reset bypass arming checks to allow for
// in-flight arming if we were armed before the reset. This
// allows a reset on a BVLOS flight to return home if the
// operator can command arming over telemetry
gcs().send_text(MAV_SEVERITY_WARNING, "watchdog: Bypassing arming checks");
return true;
}
#if GEOFENCE_ENABLED == ENABLED
if (plane.g.fence_autoenable == 3) {
if (!plane.geofence_set_enabled(true)) {
gcs().send_text(MAV_SEVERITY_WARNING, "Fence: cannot enable for arming");
return false;
} else if (!plane.geofence_prearm_check()) {
plane.geofence_set_enabled(false);
return false;
} else {
gcs().send_text(MAV_SEVERITY_WARNING, "Fence: auto-enabled for arming");
}
}
#endif
// call parent class checks
return AP_Arming::arm_checks(method);
}
/*
update HAL soft arm state and log as needed
*/
void AP_Arming_Plane::change_arm_state(void)
{
Log_Write_Arm_Disarm();
update_soft_armed();
plane.quadplane.set_armed(hal.util->get_soft_armed());
}
bool AP_Arming_Plane::arm(const AP_Arming::Method method, const bool do_arming_checks)
{
if (!AP_Arming::arm(method, do_arming_checks)) {
return false;
}
change_arm_state();
gcs().send_text(MAV_SEVERITY_INFO, "Throttle armed");
return true;
}
/*
disarm motors
*/
bool AP_Arming_Plane::disarm(void)
{
if (!AP_Arming::disarm()) {
return false;
}
if (plane.control_mode != &plane.mode_auto) {
// reset the mission on disarm if we are not in auto
plane.mission.reset();
}
// suppress the throttle in auto-throttle modes
plane.throttle_suppressed = plane.auto_throttle_mode;
//only log if disarming was successful
change_arm_state();
// reload target airspeed which could have been modified by a mission
plane.aparm.airspeed_cruise_cm.load();
#if QAUTOTUNE_ENABLED
//save qautotune gains if enabled and success
if (plane.control_mode == &plane.mode_qautotune) {
plane.quadplane.qautotune.save_tuning_gains();
} else {
plane.quadplane.qautotune.reset();
}
#endif
gcs().send_text(MAV_SEVERITY_INFO, "Throttle disarmed");
#if GEOFENCE_ENABLED == ENABLED
if (plane.g.fence_autoenable == 3) {
plane.geofence_set_enabled(false);
}
#endif
return true;
}
void AP_Arming_Plane::update_soft_armed()
{
hal.util->set_soft_armed(is_armed() &&
hal.util->safety_switch_state() != AP_HAL::Util::SAFETY_DISARMED);
AP::logger().set_vehicle_armed(hal.util->get_soft_armed());
}