/* 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), // @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 +- deadzone (RCx_DZ) // @Values: 0:Disabled,1:ArmingOnly,2:ArmOrDisarm // @User: Advanced AP_GROUPINFO("RUDDER", 3, AP_Arming_Plane, rudder_arming_value, ARMING_RUDDER_ARMONLY), AP_GROUPEND }; enum HomeState AP_Arming_Plane::home_status() const { return plane.home_is_set; } bool AP_Arming_Plane::arm(uint8_t method) { // start logging here so we can check success or failure in // arm_checks if (plane.g.log_bitmask != NONE && !plane.DataFlash.logging_started()) { plane.start_logging(); } return AP_Arming::arm(method); } /* 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.aparm.roll_limit_cd < 300) { if (report) { GCS_MAVLINK::send_statustext_all(MAV_SEVERITY_CRITICAL, "PreArm: LIM_ROLL_CD too small (%u)", plane.aparm.roll_limit_cd); } ret = false; } if (plane.aparm.pitch_limit_max_cd < 300) { if (report) { GCS_MAVLINK::send_statustext_all(MAV_SEVERITY_CRITICAL, "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, "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->get_radio_max()) { if (report) { GCS_MAVLINK::send_statustext_all(MAV_SEVERITY_CRITICAL, "PreArm: Invalid THR_FS_VALUE for rev throttle"); } ret = false; } if (plane.quadplane.available() && plane.scheduler.get_loop_rate_hz() < 100) { if (report) { GCS_MAVLINK::send_statustext_all(MAV_SEVERITY_CRITICAL, "PreArm: quadplane needs SCHED_LOOP_RATE > 100"); } ret = false; } if (plane.control_mode == AUTO && plane.mission.num_commands() <= 1) { if (report) { GCS_MAVLINK::send_statustext_all(MAV_SEVERITY_CRITICAL, "PreArm: No mission loaded"); } ret = false; } // check adsb avoidance failsafe if (plane.failsafe.adsb) { if (report) { GCS_MAVLINK::send_statustext_all(MAV_SEVERITY_CRITICAL,"PreArm: ADSB threat detected"); } ret = false; } #if HAVE_PX4_MIXER if (plane.last_mixer_crc == -1) { if (report) { // if you ever get this error, a reboot is recommended. GCS_MAVLINK::send_statustext_all(MAV_SEVERITY_CRITICAL,"PreArm: Mixer error"); } ret = false; } #endif // CONFIG_HAL_BOARD return ret; } bool AP_Arming_Plane::ins_checks(bool report) { // call parent class checks if (!AP_Arming::ins_checks(report)) { return false; } // additional plane specific checks if ((checks_to_perform & ARMING_CHECK_ALL) || (checks_to_perform & ARMING_CHECK_INS)) { if (!ahrs.healthy()) { if (report) { const char *reason = ahrs.prearm_failure_reason(); if (reason) { GCS_MAVLINK::send_statustext_all(MAV_SEVERITY_CRITICAL, "PreArm: %s", reason); } else { GCS_MAVLINK::send_statustext_all(MAV_SEVERITY_CRITICAL, "PreArm: AHRS not healthy"); } } return false; } } return true; }