ardupilot/ArduPlane/arming_checks.cpp

66 lines
2.1 KiB
C++

// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
/*
additional arming checks for plane
*/
#include "Plane.h"
const AP_Param::GroupInfo AP_Arming_Plane::var_info[] PROGMEM = {
// variables from parent vehicle
AP_NESTEDGROUPINFO(AP_Arming, 0),
// @Param: RUDDER
// @DisplayName: Rudder Arming
// @Description: Control arm/disarm by rudder input. When enabled arming is done with right rudder, disarming with left rudder. Rudder arming only works in manual throttle modes with throttle at zero
// @Values: 0:Disabled,1:ArmingOnly,2:ArmOrDisarm
// @User: Advanced
AP_GROUPINFO("RUDDER", 3, AP_Arming_Plane, rudder_arming_value, ARMING_RUDDER_ARMONLY),
AP_GROUPEND
};
/*
additional arming checks for plane
*/
bool AP_Arming_Plane::pre_arm_checks(bool report)
{
// call parent class checks
bool ret = AP_Arming::pre_arm_checks(report);
// Check airspeed sensor
ret &= AP_Arming::airspeed_checks(report);
if (plane.g.roll_limit_cd < 300) {
if (report) {
GCS_MAVLINK::send_statustext_all(MAV_SEVERITY_CRITICAL, PSTR("PreArm: LIM_ROLL_CD too small (%u)"), plane.g.roll_limit_cd);
}
ret = false;
}
if (plane.aparm.pitch_limit_max_cd < 300) {
if (report) {
GCS_MAVLINK::send_statustext_all(MAV_SEVERITY_CRITICAL, PSTR("PreArm: LIM_PITCH_MAX too small (%u)"), plane.aparm.pitch_limit_max_cd);
}
ret = false;
}
if (plane.aparm.pitch_limit_min_cd > -300) {
if (report) {
GCS_MAVLINK::send_statustext_all(MAV_SEVERITY_CRITICAL, PSTR("PreArm: LIM_PITCH_MIN too large (%u)"), 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->radio_max) {
if (report) {
GCS_MAVLINK::send_statustext_all(MAV_SEVERITY_CRITICAL, PSTR("PreArm: invalid THR_FS_VALUE for rev throttle"));
}
ret = false;
}
return ret;
}