# include "Copter.h"
/*
* High level calls to set and update flight modes logic for individual
* flight modes is in control_acro . cpp , control_stabilize . cpp , etc
*/
// return the static controller object corresponding to supplied mode
Copter : : FlightMode * Copter : : flightmode_for_mode ( const uint8_t mode )
{
Copter : : FlightMode * ret = nullptr ;
switch ( mode ) {
case ACRO :
ret = & flightmode_acro ;
break ;
case STABILIZE :
ret = & flightmode_stabilize ;
break ;
case ALT_HOLD :
ret = & flightmode_althold ;
break ;
case AUTO :
ret = & flightmode_auto ;
break ;
case CIRCLE :
ret = & flightmode_circle ;
break ;
case LOITER :
ret = & flightmode_loiter ;
break ;
case GUIDED :
ret = & flightmode_guided ;
break ;
case LAND :
ret = & flightmode_land ;
break ;
case RTL :
ret = & flightmode_rtl ;
break ;
case DRIFT :
ret = & flightmode_drift ;
break ;
case SPORT :
ret = & flightmode_sport ;
break ;
case FLIP :
ret = & flightmode_flip ;
break ;
# if AUTOTUNE_ENABLED == ENABLED
case AUTOTUNE :
ret = & flightmode_autotune ;
break ;
# endif
# if POSHOLD_ENABLED == ENABLED
case POSHOLD :
ret = & flightmode_poshold ;
break ;
# endif
case BRAKE :
ret = & flightmode_brake ;
break ;
case THROW :
ret = & flightmode_throw ;
break ;
case AVOID_ADSB :
ret = & flightmode_avoid_adsb ;
break ;
case GUIDED_NOGPS :
ret = & flightmode_guided_nogps ;
break ;
case SMART_RTL :
ret = & flightmode_smartrtl ;
break ;
default :
break ;
}
return ret ;
}
// set_mode - change flight mode and perform any necessary initialisation
// optional force parameter used to force the flight mode change (used only first time mode is set)
// returns true if mode was successfully set
// ACRO, STABILIZE, ALTHOLD, LAND, DRIFT and SPORT can always be set successfully but the return state of other flight modes should be checked and the caller should deal with failures appropriately
bool Copter : : set_mode ( control_mode_t mode , mode_reason_t reason )
{
// return immediately if we are already in the desired mode
if ( mode = = control_mode ) {
control_mode_reason = reason ;
return true ;
}
Copter : : FlightMode * new_flightmode = flightmode_for_mode ( mode ) ;
if ( new_flightmode = = nullptr ) {
gcs ( ) . send_text ( MAV_SEVERITY_WARNING , " No such mode " ) ;
Log_Write_Error ( ERROR_SUBSYSTEM_FLIGHT_MODE , mode ) ;
return false ;
}
bool ignore_checks = ! motors - > armed ( ) ; // allow switching to any mode if disarmed. We rely on the arming check to perform
if ( ! new_flightmode - > init ( ignore_checks ) ) {
gcs ( ) . send_text ( MAV_SEVERITY_WARNING , " Flight mode change failed " ) ;
Log_Write_Error ( ERROR_SUBSYSTEM_FLIGHT_MODE , mode ) ;
return false ;
}
# if FRAME_CONFIG == HELI_FRAME
// do not allow helis to enter a non-manual throttle mode if the
// rotor runup is not complete
if ( ! ignore_checks & & ! mode_has_manual_throttle ( mode ) & & ! motors - > rotor_runup_complete ( ) ) {
return false ;
}
# endif
// perform any cleanup required by previous flight mode
exit_mode ( control_mode , mode ) ;
// update flight mode
flightmode = new_flightmode ;
control_mode = mode ;
control_mode_reason = reason ;
DataFlash . Log_Write_Mode ( control_mode ) ;
adsb . set_is_auto_mode ( ( mode = = AUTO ) | | ( mode = = RTL ) | | ( mode = = GUIDED ) ) ;
# if AC_FENCE == ENABLED
// pilot requested flight mode change during a fence breach indicates pilot is attempting to manually recover
// this flight mode change could be automatic (i.e. fence, battery, GPS or GCS failsafe)
// but it should be harmless to disable the fence temporarily in these situations as well
fence . manual_recovery_start ( ) ;
# endif
# if FRSKY_TELEM_ENABLED == ENABLED
frsky_telemetry . update_control_mode ( control_mode ) ;
# endif
# if CAMERA == ENABLED
camera . set_is_auto_mode ( control_mode = = AUTO ) ;
# endif
// update notify object
notify_flight_mode ( ) ;
// return success
return true ;
}
// update_flight_mode - calls the appropriate attitude controllers based on flight mode
// called at 100hz or more
void Copter : : update_flight_mode ( )
{
// Update EKF speed limit - used to limit speed when we are using optical flow
ahrs . getEkfControlLimits ( ekfGndSpdLimit , ekfNavVelGainScaler ) ;
flightmode - > run ( ) ;
}
// exit_mode - high level call to organise cleanup as a flight mode is exited
void Copter : : exit_mode ( control_mode_t old_control_mode , control_mode_t new_control_mode )
{
# if AUTOTUNE_ENABLED == ENABLED
if ( old_control_mode = = AUTOTUNE ) {
flightmode_autotune . autotune_stop ( ) ;
}
# endif
// stop mission when we leave auto mode
if ( old_control_mode = = AUTO ) {
if ( mission . state ( ) = = AP_Mission : : MISSION_RUNNING ) {
mission . stop ( ) ;
}
# if MOUNT == ENABLED
camera_mount . set_mode_to_default ( ) ;
# endif // MOUNT == ENABLED
}
// smooth throttle transition when switching from manual to automatic flight modes
if ( mode_has_manual_throttle ( old_control_mode ) & & ! mode_has_manual_throttle ( new_control_mode ) & & motors - > armed ( ) & & ! ap . land_complete ) {
// this assumes all manual flight modes use get_pilot_desired_throttle to translate pilot input to output throttle
set_accel_throttle_I_from_pilot_throttle ( ) ;
}
// cancel any takeoffs in progress
takeoff_stop ( ) ;
// call smart_rtl cleanup
if ( old_control_mode = = SMART_RTL ) {
flightmode_smartrtl . exit ( ) ;
}
# if FRAME_CONFIG == HELI_FRAME
// firmly reset the flybar passthrough to false when exiting acro mode.
if ( old_control_mode = = ACRO ) {
attitude_control - > use_flybar_passthrough ( false , false ) ;
motors - > set_acro_tail ( false ) ;
}
// if we are changing from a mode that did not use manual throttle,
// stab col ramp value should be pre-loaded to the correct value to avoid a twitch
// heli_stab_col_ramp should really only be active switching between Stabilize and Acro modes
if ( ! mode_has_manual_throttle ( old_control_mode ) ) {
if ( new_control_mode = = STABILIZE ) {
input_manager . set_stab_col_ramp ( 1.0 ) ;
} else if ( new_control_mode = = ACRO ) {
input_manager . set_stab_col_ramp ( 0.0 ) ;
}
}
# endif //HELI_FRAME
}
// mode_has_manual_throttle - returns true if the flight mode has a manual throttle (i.e. pilot directly controls throttle)
bool Copter : : mode_has_manual_throttle ( control_mode_t mode )
{
switch ( mode ) {
case ACRO :
case STABILIZE :
return true ;
default :
return false ;
}
}
// notify_flight_mode - sets notify object based on current flight mode. Only used for OreoLED notify device
void Copter : : notify_flight_mode ( ) {
AP_Notify : : flags . autopilot_mode = flightmode - > is_autopilot ( ) ;
notify . set_flight_mode_str ( flightmode - > name4 ( ) ) ;
}