/* plane specific AP_AdvancedFailsafe class */ #include "Plane.h" #if ADVANCED_FAILSAFE == ENABLED // Constructor AP_AdvancedFailsafe_Plane::AP_AdvancedFailsafe_Plane(AP_Mission &_mission, const AP_GPS &_gps) : AP_AdvancedFailsafe(_mission, _gps) {} /* setup radio_out values for all channels to termination values */ void AP_AdvancedFailsafe_Plane::terminate_vehicle(void) { plane.g2.servo_channels.disable_passthrough(true); if (_terminate_action == TERMINATE_ACTION_LAND) { plane.landing.terminate(); } else { // aerodynamic termination is the default approach to termination SRV_Channels::set_output_scaled(SRV_Channel::k_flap_auto, 100); SRV_Channels::set_output_scaled(SRV_Channel::k_flap, 100); SRV_Channels::set_output_scaled(SRV_Channel::k_aileron, SERVO_MAX); SRV_Channels::set_output_scaled(SRV_Channel::k_rudder, SERVO_MAX); SRV_Channels::set_output_scaled(SRV_Channel::k_elevator, SERVO_MAX); if (plane.have_reverse_thrust()) { // configured for reverse thrust, use TRIM SRV_Channels::set_output_limit(SRV_Channel::k_throttle, SRV_Channel::SRV_CHANNEL_LIMIT_TRIM); SRV_Channels::set_output_limit(SRV_Channel::k_throttleLeft, SRV_Channel::SRV_CHANNEL_LIMIT_TRIM); SRV_Channels::set_output_limit(SRV_Channel::k_throttleRight, SRV_Channel::SRV_CHANNEL_LIMIT_TRIM); } else { // use MIN SRV_Channels::set_output_limit(SRV_Channel::k_throttle, SRV_Channel::SRV_CHANNEL_LIMIT_MIN); SRV_Channels::set_output_limit(SRV_Channel::k_throttleLeft, SRV_Channel::SRV_CHANNEL_LIMIT_MIN); SRV_Channels::set_output_limit(SRV_Channel::k_throttleRight, SRV_Channel::SRV_CHANNEL_LIMIT_MIN); } SRV_Channels::set_output_limit(SRV_Channel::k_manual, SRV_Channel::SRV_CHANNEL_LIMIT_TRIM); SRV_Channels::set_output_limit(SRV_Channel::k_none, SRV_Channel::SRV_CHANNEL_LIMIT_TRIM); } plane.servos_output(); plane.quadplane.afs_terminate(); // also disarm to ensure that ignition is cut plane.arming.disarm(); } void AP_AdvancedFailsafe_Plane::setup_IO_failsafe(void) { // all aux channels SRV_Channels::set_failsafe_limit(SRV_Channel::k_flap_auto, SRV_Channel::SRV_CHANNEL_LIMIT_MAX); SRV_Channels::set_failsafe_limit(SRV_Channel::k_flap, SRV_Channel::SRV_CHANNEL_LIMIT_MAX); SRV_Channels::set_failsafe_limit(SRV_Channel::k_aileron, SRV_Channel::SRV_CHANNEL_LIMIT_MIN); SRV_Channels::set_failsafe_limit(SRV_Channel::k_rudder, SRV_Channel::SRV_CHANNEL_LIMIT_MAX); SRV_Channels::set_failsafe_limit(SRV_Channel::k_elevator, SRV_Channel::SRV_CHANNEL_LIMIT_MAX); if (plane.have_reverse_thrust()) { // configured for reverse thrust, use TRIM SRV_Channels::set_failsafe_limit(SRV_Channel::k_throttle, SRV_Channel::SRV_CHANNEL_LIMIT_TRIM); SRV_Channels::set_failsafe_limit(SRV_Channel::k_throttleLeft, SRV_Channel::SRV_CHANNEL_LIMIT_TRIM); SRV_Channels::set_failsafe_limit(SRV_Channel::k_throttleRight, SRV_Channel::SRV_CHANNEL_LIMIT_TRIM); } else { // normal throttle, use MIN SRV_Channels::set_failsafe_limit(SRV_Channel::k_throttle, SRV_Channel::SRV_CHANNEL_LIMIT_MIN); SRV_Channels::set_failsafe_limit(SRV_Channel::k_throttleLeft, SRV_Channel::SRV_CHANNEL_LIMIT_MIN); SRV_Channels::set_failsafe_limit(SRV_Channel::k_throttleRight, SRV_Channel::SRV_CHANNEL_LIMIT_MIN); } SRV_Channels::set_failsafe_limit(SRV_Channel::k_manual, SRV_Channel::SRV_CHANNEL_LIMIT_TRIM); SRV_Channels::set_failsafe_limit(SRV_Channel::k_none, SRV_Channel::SRV_CHANNEL_LIMIT_TRIM); if (plane.quadplane.available()) { // setup AP_Motors outputs for failsafe uint16_t mask = plane.quadplane.motors->get_motor_mask(); hal.rcout->set_failsafe_pwm(mask, plane.quadplane.thr_min_pwm); } } /* return an AFS_MODE for current control mode */ AP_AdvancedFailsafe::control_mode AP_AdvancedFailsafe_Plane::afs_mode(void) { if (plane.auto_throttle_mode) { return AP_AdvancedFailsafe::AFS_AUTO; } if (plane.control_mode == &plane.mode_manual) { return AP_AdvancedFailsafe::AFS_MANUAL; } return AP_AdvancedFailsafe::AFS_STABILIZED; } #endif // ADVANCED_FAILSAFE