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# include "Copter.h"
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/*
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* High level calls to set and update flight modes logic for individual
* flight modes is in control_acro . cpp , control_stabilize . cpp , etc
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*/
// 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)
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// returns true if mode was successfully set
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// 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
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bool Copter : : set_mode ( control_mode_t mode , mode_reason_t reason )
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{
// boolean to record if flight mode could be set
bool success = false ;
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bool ignore_checks = ! motors - > armed ( ) ; // allow switching to any mode if disarmed. We rely on the arming check to perform
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// return immediately if we are already in the desired mode
if ( mode = = control_mode ) {
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prev_control_mode = control_mode ;
prev_control_mode_reason = control_mode_reason ;
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control_mode_reason = reason ;
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return true ;
}
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# 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 ( ) ) {
goto failed ;
}
# endif
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switch ( mode ) {
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case ACRO :
# if FRAME_CONFIG == HELI_FRAME
success = heli_acro_init ( ignore_checks ) ;
# else
success = acro_init ( ignore_checks ) ;
# endif
break ;
case STABILIZE :
# if FRAME_CONFIG == HELI_FRAME
success = heli_stabilize_init ( ignore_checks ) ;
# else
success = stabilize_init ( ignore_checks ) ;
# endif
break ;
case ALT_HOLD :
success = althold_init ( ignore_checks ) ;
break ;
case AUTO :
success = auto_init ( ignore_checks ) ;
break ;
case CIRCLE :
success = circle_init ( ignore_checks ) ;
break ;
case LOITER :
success = loiter_init ( ignore_checks ) ;
break ;
case GUIDED :
success = guided_init ( ignore_checks ) ;
break ;
case LAND :
success = land_init ( ignore_checks ) ;
break ;
case RTL :
success = rtl_init ( ignore_checks ) ;
break ;
case DRIFT :
success = drift_init ( ignore_checks ) ;
break ;
case SPORT :
success = sport_init ( ignore_checks ) ;
break ;
case FLIP :
success = flip_init ( ignore_checks ) ;
break ;
# if AUTOTUNE_ENABLED == ENABLED
case AUTOTUNE :
success = autotune_init ( ignore_checks ) ;
break ;
# endif
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# if POSHOLD_ENABLED == ENABLED
case POSHOLD :
success = poshold_init ( ignore_checks ) ;
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break ;
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# endif
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case BRAKE :
success = brake_init ( ignore_checks ) ;
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break ;
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case THROW :
success = throw_init ( ignore_checks ) ;
break ;
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case AVOID_ADSB :
success = avoid_adsb_init ( ignore_checks ) ;
break ;
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case GUIDED_NOGPS :
success = guided_nogps_init ( ignore_checks ) ;
break ;
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case SMART_RTL :
success = smart_rtl_init ( ignore_checks ) ;
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break ;
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default :
success = false ;
break ;
}
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# if FRAME_CONFIG == HELI_FRAME
failed :
# endif
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// update flight mode
if ( success ) {
// perform any cleanup required by previous flight mode
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exit_mode ( control_mode , mode ) ;
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prev_control_mode = control_mode ;
prev_control_mode_reason = control_mode_reason ;
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control_mode = mode ;
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control_mode_reason = reason ;
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DataFlash . Log_Write_Mode ( control_mode , control_mode_reason ) ;
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adsb . set_is_auto_mode ( ( mode = = AUTO ) | | ( mode = = RTL ) | | ( mode = = GUIDED ) ) ;
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# 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
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# if FRSKY_TELEM_ENABLED == ENABLED
frsky_telemetry . update_control_mode ( control_mode ) ;
# endif
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} else {
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// Log error that we failed to enter desired flight mode
Log_Write_Error ( ERROR_SUBSYSTEM_FLIGHT_MODE , mode ) ;
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gcs ( ) . send_text ( MAV_SEVERITY_WARNING , " Flight mode change failed " ) ;
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}
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// update notify object
if ( success ) {
notify_flight_mode ( control_mode ) ;
}
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// return success or failure
return success ;
}
// update_flight_mode - calls the appropriate attitude controllers based on flight mode
// called at 100hz or more
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void Copter : : update_flight_mode ( )
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{
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// Update EKF speed limit - used to limit speed when we are using optical flow
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ahrs . getEkfControlLimits ( ekfGndSpdLimit , ekfNavVelGainScaler ) ;
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switch ( control_mode ) {
case ACRO :
# if FRAME_CONFIG == HELI_FRAME
heli_acro_run ( ) ;
# else
acro_run ( ) ;
# endif
break ;
case STABILIZE :
# if FRAME_CONFIG == HELI_FRAME
heli_stabilize_run ( ) ;
# else
stabilize_run ( ) ;
# endif
break ;
case ALT_HOLD :
althold_run ( ) ;
break ;
case AUTO :
auto_run ( ) ;
break ;
case CIRCLE :
circle_run ( ) ;
break ;
case LOITER :
loiter_run ( ) ;
break ;
case GUIDED :
guided_run ( ) ;
break ;
case LAND :
land_run ( ) ;
break ;
case RTL :
rtl_run ( ) ;
break ;
case DRIFT :
drift_run ( ) ;
break ;
case SPORT :
sport_run ( ) ;
break ;
case FLIP :
flip_run ( ) ;
break ;
# if AUTOTUNE_ENABLED == ENABLED
case AUTOTUNE :
autotune_run ( ) ;
break ;
# endif
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# if POSHOLD_ENABLED == ENABLED
case POSHOLD :
poshold_run ( ) ;
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break ;
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# endif
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case BRAKE :
brake_run ( ) ;
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break ;
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case THROW :
throw_run ( ) ;
break ;
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case AVOID_ADSB :
avoid_adsb_run ( ) ;
break ;
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case GUIDED_NOGPS :
guided_nogps_run ( ) ;
break ;
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case SMART_RTL :
smart_rtl_run ( ) ;
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break ;
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default :
break ;
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}
}
// exit_mode - high level call to organise cleanup as a flight mode is exited
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void Copter : : exit_mode ( control_mode_t old_control_mode , control_mode_t new_control_mode )
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{
# if AUTOTUNE_ENABLED == ENABLED
if ( old_control_mode = = AUTOTUNE ) {
autotune_stop ( ) ;
}
# endif
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// stop mission when we leave auto mode
if ( old_control_mode = = AUTO ) {
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if ( mission . state ( ) = = AP_Mission : : MISSION_RUNNING ) {
mission . stop ( ) ;
}
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# if MOUNT == ENABLED
camera_mount . set_mode_to_default ( ) ;
# endif // MOUNT == ENABLED
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}
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// smooth throttle transition when switching from manual to automatic flight modes
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if ( mode_has_manual_throttle ( old_control_mode ) & & ! mode_has_manual_throttle ( new_control_mode ) & & motors - > armed ( ) & & ! ap . land_complete ) {
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// this assumes all manual flight modes use get_pilot_desired_throttle to translate pilot input to output throttle
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set_accel_throttle_I_from_pilot_throttle ( ) ;
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}
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// cancel any takeoffs in progress
takeoff_stop ( ) ;
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// call smart_rtl cleanup
if ( old_control_mode = = SMART_RTL ) {
smart_rtl_exit ( ) ;
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}
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# if FRAME_CONFIG == HELI_FRAME
// firmly reset the flybar passthrough to false when exiting acro mode.
if ( old_control_mode = = ACRO ) {
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attitude_control - > use_flybar_passthrough ( false , false ) ;
motors - > set_acro_tail ( false ) ;
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}
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// 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 ) ;
}
}
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# endif //HELI_FRAME
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}
// returns true or false whether mode requires GPS
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bool Copter : : mode_requires_GPS ( control_mode_t mode )
{
switch ( mode ) {
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case AUTO :
case GUIDED :
case LOITER :
case RTL :
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case SMART_RTL :
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case CIRCLE :
case DRIFT :
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case POSHOLD :
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case BRAKE :
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case AVOID_ADSB :
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case THROW :
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return true ;
default :
return false ;
}
}
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// mode_has_manual_throttle - returns true if the flight mode has a manual throttle (i.e. pilot directly controls throttle)
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bool Copter : : mode_has_manual_throttle ( control_mode_t mode )
{
switch ( mode ) {
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case ACRO :
case STABILIZE :
return true ;
default :
return false ;
}
}
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// mode_allows_arming - returns true if vehicle can be armed in the specified mode
// arming_from_gcs should be set to true if the arming request comes from the ground station
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bool Copter : : mode_allows_arming ( control_mode_t mode , bool arming_from_gcs )
{
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if ( mode_has_manual_throttle ( mode ) | | mode = = LOITER | | mode = = ALT_HOLD | | mode = = POSHOLD | | mode = = DRIFT | | mode = = SPORT | | mode = = THROW | | ( arming_from_gcs & & ( mode = = GUIDED | | mode = = GUIDED_NOGPS ) ) ) {
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return true ;
}
return false ;
}
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// notify_flight_mode - sets notify object based on flight mode. Only used for OreoLED notify device
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void Copter : : notify_flight_mode ( control_mode_t mode )
{
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AP_Notify : : flags . flight_mode = mode ;
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switch ( mode ) {
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case AUTO :
case GUIDED :
case RTL :
case CIRCLE :
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case AVOID_ADSB :
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case GUIDED_NOGPS :
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case LAND :
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case SMART_RTL :
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// autopilot modes
AP_Notify : : flags . autopilot_mode = true ;
break ;
default :
// all other are manual flight modes
AP_Notify : : flags . autopilot_mode = false ;
break ;
}
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// set flight mode string
switch ( mode ) {
case STABILIZE :
notify . set_flight_mode_str ( " STAB " ) ;
break ;
case ACRO :
notify . set_flight_mode_str ( " ACRO " ) ;
break ;
case ALT_HOLD :
notify . set_flight_mode_str ( " ALTH " ) ;
break ;
case AUTO :
notify . set_flight_mode_str ( " AUTO " ) ;
break ;
case GUIDED :
notify . set_flight_mode_str ( " GUID " ) ;
break ;
case LOITER :
notify . set_flight_mode_str ( " LOIT " ) ;
break ;
case RTL :
notify . set_flight_mode_str ( " RTL " ) ;
break ;
case CIRCLE :
notify . set_flight_mode_str ( " CIRC " ) ;
break ;
case LAND :
notify . set_flight_mode_str ( " LAND " ) ;
break ;
case DRIFT :
notify . set_flight_mode_str ( " DRIF " ) ;
break ;
case SPORT :
notify . set_flight_mode_str ( " SPRT " ) ;
break ;
case FLIP :
notify . set_flight_mode_str ( " FLIP " ) ;
break ;
case AUTOTUNE :
notify . set_flight_mode_str ( " ATUN " ) ;
break ;
case POSHOLD :
notify . set_flight_mode_str ( " PHLD " ) ;
break ;
case BRAKE :
notify . set_flight_mode_str ( " BRAK " ) ;
break ;
case THROW :
notify . set_flight_mode_str ( " THRW " ) ;
break ;
case AVOID_ADSB :
notify . set_flight_mode_str ( " AVOI " ) ;
break ;
case GUIDED_NOGPS :
notify . set_flight_mode_str ( " GNGP " ) ;
break ;
default :
notify . set_flight_mode_str ( " ---- " ) ;
break ;
}
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}