@ -166,17 +166,17 @@ private:
@@ -166,17 +166,17 @@ private:
ParametersG2 g2 ;
// main loop scheduler
AP_Scheduler scheduler = AP_Scheduler : : create ( ) ;
AP_Scheduler scheduler ;
// mapping between input channels
RCMapper rcmap = RCMapper : : create ( ) ;
RCMapper rcmap ;
// board specific config
AP_BoardConfig BoardConfig = AP_BoardConfig : : create ( ) ;
AP_BoardConfig BoardConfig ;
// board specific config for CAN bus
# if HAL_WITH_UAVCAN
AP_BoardConfig_CAN BoardConfig_CAN = AP_BoardConfig_CAN : : create ( ) ;
AP_BoardConfig_CAN BoardConfig_CAN ;
# endif
// primary input channels
@ -186,7 +186,7 @@ private:
@@ -186,7 +186,7 @@ private:
RC_Channel * channel_rudder ;
// notification object for LEDs, buzzers etc (parameter set to false disables external leds)
AP_Notify notify = AP_Notify : : create ( ) ;
AP_Notify notify ;
DataFlash_Class DataFlash ;
@ -195,39 +195,39 @@ private:
@@ -195,39 +195,39 @@ private:
int32_t pitch_limit_min_cd ;
// Sensors
AP_GPS gps = AP_GPS : : create ( ) ;
AP_GPS gps ;
// flight modes convenience array
AP_Int8 * flight_modes = & g . flight_mode1 ;
AP_Baro barometer = AP_Baro : : create ( ) ;
Compass compass = Compass : : create ( ) ;
AP_Baro barometer ;
Compass compass ;
AP_InertialSensor ins = AP_InertialSensor : : create ( ) ;
AP_InertialSensor ins ;
RangeFinder rangefinder = RangeFinder : : create ( serial_manager , ROTATION_PITCH_270 ) ;
RangeFinder rangefinder { serial_manager , ROTATION_PITCH_270 } ;
AP_Vehicle : : FixedWing : : Rangefinder_State rangefinder_state ;
AP_RPM rpm_sensor = AP_RPM : : create ( ) ;
AP_RPM rpm_sensor ;
// Inertial Navigation EKF
# if AP_AHRS_NAVEKF_AVAILABLE
NavEKF2 EKF2 = NavEKF2 : : create ( & ahrs , barometer , rangefinder ) ;
NavEKF3 EKF3 = NavEKF3 : : create ( & ahrs , barometer , rangefinder ) ;
AP_AHRS_NavEKF ahrs = AP_AHRS_NavEKF : : create ( ins , barometer , gps , EKF2 , EKF3 ) ;
NavEKF2 EKF2 { & ahrs , barometer , rangefinder } ;
NavEKF3 EKF3 { & ahrs , barometer , rangefinder } ;
AP_AHRS_NavEKF ahrs { ins , barometer , gps , EKF2 , EKF3 } ;
# else
AP_AHRS_DCM ahrs = AP_AHRS_DCM : : create ( ins , barometer , gps ) ;
AP_AHRS_DCM ahrs { ins , barometer , gps } ;
# endif
AP_TECS TECS_controller = AP_TECS : : create ( ahrs , aparm , landing , g2 . soaring_controller ) ;
AP_L1_Control L1_controller = AP_L1_Control : : create ( ahrs , & TECS_controller ) ;
AP_TECS TECS_controller { ahrs , aparm , landing , g2 . soaring_controller } ;
AP_L1_Control L1_controller { ahrs , & TECS_controller } ;
// Attitude to servo controllers
AP_RollController rollController = AP_RollController : : create ( ahrs , aparm , DataFlash ) ;
AP_PitchController pitchController = AP_PitchController : : create ( ahrs , aparm , DataFlash ) ;
AP_YawController yawController = AP_YawController : : create ( ahrs , aparm ) ;
AP_SteerController steerController = AP_SteerController : : create ( ahrs ) ;
AP_RollController rollController { ahrs , aparm , DataFlash } ;
AP_PitchController pitchController { ahrs , aparm , DataFlash } ;
AP_YawController yawController { ahrs , aparm } ;
AP_SteerController steerController { ahrs } ;
# if CONFIG_HAL_BOARD == HAL_BOARD_SITL
SITL : : SITL sitl ;
@ -254,7 +254,7 @@ private:
@@ -254,7 +254,7 @@ private:
// external failsafe boards during baro and airspeed calibration
bool in_calibration ;
AP_SerialManager serial_manager = AP_SerialManager : : create ( ) ;
AP_SerialManager serial_manager ;
// GCS selection
GCS_Plane _gcs ; // avoid using this; use gcs()
@ -267,26 +267,26 @@ private:
@@ -267,26 +267,26 @@ private:
AP_SpdHgtControl * SpdHgt_Controller = & TECS_controller ;
// Relay
AP_Relay relay = AP_Relay : : create ( ) ;
AP_Relay relay ;
// handle servo and relay events
AP_ServoRelayEvents ServoRelayEvents = AP_ServoRelayEvents : : create ( relay ) ;
AP_ServoRelayEvents ServoRelayEvents { relay } ;
// Camera
# if CAMERA == ENABLED
AP_Camera camera = AP_Camera : : create ( & relay , MASK_LOG_CAMERA , current_loc , ahrs ) ;
AP_Camera camera { & relay , MASK_LOG_CAMERA , current_loc , ahrs } ;
# endif
# if OPTFLOW == ENABLED
// Optical flow sensor
OpticalFlow optflow = OpticalFlow : : create ( ahrs ) ;
OpticalFlow optflow { ahrs } ;
# endif
// Rally Ponints
AP_Rally rally = AP_Rally : : create ( ahrs ) ;
AP_Rally rally { ahrs } ;
// RSSI
AP_RSSI rssi = AP_RSSI : : create ( ) ;
AP_RSSI rssi ;
// This is the state of the flight control system
// There are multiple states defined such as MANUAL, FBW-A, AUTO
@ -391,11 +391,11 @@ private:
@@ -391,11 +391,11 @@ private:
int32_t altitude_error_cm ;
// Battery Sensors
AP_BattMonitor battery = AP_BattMonitor : : create ( ) ;
AP_BattMonitor battery ;
# if FRSKY_TELEM_ENABLED == ENABLED
// FrSky telemetry support
AP_Frsky_Telem frsky_telemetry = AP_Frsky_Telem : : create ( ahrs , battery , rangefinder ) ;
AP_Frsky_Telem frsky_telemetry { ahrs , battery , rangefinder } ;
# endif
// Variables for extended status MAVLink messages
@ -599,33 +599,33 @@ private:
@@ -599,33 +599,33 @@ private:
float smoothed_airspeed ;
// Mission library
AP_Mission mission = AP_Mission : : create ( ahrs ,
AP_Mission mission { ahrs ,
FUNCTOR_BIND_MEMBER ( & Plane : : start_command_callback , bool , const AP_Mission : : Mission_Command & ) ,
FUNCTOR_BIND_MEMBER ( & Plane : : verify_command_callback , bool , const AP_Mission : : Mission_Command & ) ,
FUNCTOR_BIND_MEMBER ( & Plane : : exit_mission_callback , void ) ) ;
FUNCTOR_BIND_MEMBER ( & Plane : : exit_mission_callback , void ) } ;
# if PARACHUTE == ENABLED
AP_Parachute parachute = AP_Parachute : : create ( relay ) ;
AP_Parachute parachute { relay } ;
# endif
// terrain handling
# if AP_TERRAIN_AVAILABLE
AP_Terrain terrain = AP_Terrain : : create ( ahrs , mission , rally ) ;
AP_Terrain terrain { ahrs , mission , rally } ;
# endif
AP_Landing landing = AP_Landing : : create ( mission , ahrs , SpdHgt_Controller , nav_controller , aparm ,
FUNCTOR_BIND_MEMBER ( & Plane : : set_target_altitude_proportion , void , const Location & , float ) ,
FUNCTOR_BIND_MEMBER ( & Plane : : constrain_target_altitude_location , void , const Location & , const Location & ) ,
FUNCTOR_BIND_MEMBER ( & Plane : : adjusted_altitude_cm , int32_t ) ,
FUNCTOR_BIND_MEMBER ( & Plane : : adjusted_relative_altitude_cm , int32_t ) ,
FUNCTOR_BIND_MEMBER ( & Plane : : disarm_if_autoland_complete , void ) ,
FUNCTOR_BIND_MEMBER ( & Plane : : update_flight_stage , void ) ) ;
AP_Landing landing { mission , ahrs , SpdHgt_Controller , nav_controller , aparm ,
FUNCTOR_BIND_MEMBER ( & Plane : : set_target_altitude_proportion , void , const Location & , float ) ,
FUNCTOR_BIND_MEMBER ( & Plane : : constrain_target_altitude_location , void , const Location & , const Location & ) ,
FUNCTOR_BIND_MEMBER ( & Plane : : adjusted_altitude_cm , int32_t ) ,
FUNCTOR_BIND_MEMBER ( & Plane : : adjusted_relative_altitude_cm , int32_t ) ,
FUNCTOR_BIND_MEMBER ( & Plane : : disarm_if_autoland_complete , void ) ,
FUNCTOR_BIND_MEMBER ( & Plane : : update_flight_stage , void ) } ;
AP_ADSB adsb = AP_ADSB : : create ( ahrs ) ;
AP_ADSB adsb { ahrs } ;
// avoidance of adsb enabled vehicles (normally manned vheicles)
AP_Avoidance_Plane avoidance_adsb = AP_Avoidance_Plane : : create ( ahrs , adsb ) ;
AP_Avoidance_Plane avoidance_adsb { ahrs , adsb } ;
// Outback Challenge Failsafe Support
AP_AdvancedFailsafe_Plane afs { mission , barometer , gps , rcmap } ;
@ -768,11 +768,11 @@ private:
@@ -768,11 +768,11 @@ private:
// Camera/Antenna mount tracking and stabilisation stuff
# if MOUNT == ENABLED
// current_loc uses the baro/gps soloution for altitude rather than gps only.
AP_Mount camera_mount = AP_Mount : : create ( ahrs , current_loc ) ;
AP_Mount camera_mount { ahrs , current_loc } ;
# endif
// Arming/Disarming mangement class
AP_Arming_Plane arming = AP_Arming_Plane : : create ( ahrs , barometer , compass , battery ) ;
AP_Arming_Plane arming { ahrs , barometer , compass , battery } ;
AP_Param param_loader { var_info } ;