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# include "Copter.h"
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# if MODE_RTL_ENABLED == ENABLED
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/*
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* Init and run calls for RTL flight mode
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*
* There are two parts to RTL , the high level decision making which controls which state we are in
* and the lower implementation of the waypoint or landing controllers within those states
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*/
// rtl_init - initialise rtl controller
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bool ModeRTL : : init ( bool ignore_checks )
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{
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if ( ! ignore_checks ) {
if ( ! AP : : ahrs ( ) . home_is_set ( ) ) {
return false ;
}
}
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// initialise waypoint and spline controller
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wp_nav - > wp_and_spline_init ( g . rtl_speed_cms ) ;
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_state = SubMode : : STARTING ;
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_state_complete = true ; // see run() method below
terrain_following_allowed = ! copter . failsafe . terrain ;
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// reset flag indicating if pilot has applied roll or pitch inputs during landing
copter . ap . land_repo_active = false ;
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// this will be set true if prec land is later active
copter . ap . prec_land_active = false ;
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# if AC_PRECLAND_ENABLED
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// initialise precland state machine
copter . precland_statemachine . init ( ) ;
# endif
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return true ;
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}
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// re-start RTL with terrain following disabled
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void ModeRTL : : restart_without_terrain ( )
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{
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AP : : logger ( ) . Write_Error ( LogErrorSubsystem : : NAVIGATION , LogErrorCode : : RESTARTED_RTL ) ;
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terrain_following_allowed = false ;
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_state = SubMode : : STARTING ;
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_state_complete = true ;
gcs ( ) . send_text ( MAV_SEVERITY_CRITICAL , " Restarting RTL - Terrain data missing " ) ;
}
ModeRTL : : RTLAltType ModeRTL : : get_alt_type ( ) const
{
// sanity check parameter
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switch ( ( ModeRTL : : RTLAltType ) g . rtl_alt_type ) {
case RTLAltType : : RTL_ALTTYPE_RELATIVE . . . RTLAltType : : RTL_ALTTYPE_TERRAIN :
return g . rtl_alt_type ;
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}
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// user has an invalid value
return RTLAltType : : RTL_ALTTYPE_RELATIVE ;
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}
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// rtl_run - runs the return-to-launch controller
// should be called at 100hz or more
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void ModeRTL : : run ( bool disarm_on_land )
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{
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if ( ! motors - > armed ( ) ) {
return ;
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}
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// check if we need to move to next state
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if ( _state_complete ) {
switch ( _state ) {
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case SubMode : : STARTING :
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build_path ( ) ;
climb_start ( ) ;
break ;
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case SubMode : : INITIAL_CLIMB :
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return_start ( ) ;
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break ;
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case SubMode : : RETURN_HOME :
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loiterathome_start ( ) ;
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break ;
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case SubMode : : LOITER_AT_HOME :
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if ( rtl_path . land | | copter . failsafe . radio ) {
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land_start ( ) ;
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} else {
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descent_start ( ) ;
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}
break ;
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case SubMode : : FINAL_DESCENT :
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// do nothing
break ;
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case SubMode : : LAND :
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// do nothing - rtl_land_run will take care of disarming motors
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break ;
}
}
// call the correct run function
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switch ( _state ) {
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case SubMode : : STARTING :
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// should not be reached:
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_state = SubMode : : INITIAL_CLIMB ;
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FALLTHROUGH ;
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case SubMode : : INITIAL_CLIMB :
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climb_return_run ( ) ;
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break ;
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case SubMode : : RETURN_HOME :
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climb_return_run ( ) ;
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break ;
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case SubMode : : LOITER_AT_HOME :
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loiterathome_run ( ) ;
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break ;
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case SubMode : : FINAL_DESCENT :
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descent_run ( ) ;
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break ;
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case SubMode : : LAND :
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land_run ( disarm_on_land ) ;
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break ;
}
}
// rtl_climb_start - initialise climb to RTL altitude
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void ModeRTL : : climb_start ( )
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{
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_state = SubMode : : INITIAL_CLIMB ;
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_state_complete = false ;
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// set the destination
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if ( ! wp_nav - > set_wp_destination_loc ( rtl_path . climb_target ) | | ! wp_nav - > set_wp_destination_next_loc ( rtl_path . return_target ) ) {
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// this should not happen because rtl_build_path will have checked terrain data was available
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gcs ( ) . send_text ( MAV_SEVERITY_CRITICAL , " RTL: unexpected error setting climb target " ) ;
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AP : : logger ( ) . Write_Error ( LogErrorSubsystem : : NAVIGATION , LogErrorCode : : FAILED_TO_SET_DESTINATION ) ;
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copter . set_mode ( Mode : : Number : : LAND , ModeReason : : TERRAIN_FAILSAFE ) ;
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return ;
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}
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// hold current yaw during initial climb
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auto_yaw . set_mode ( AutoYaw : : Mode : : HOLD ) ;
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}
// rtl_return_start - initialise return to home
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void ModeRTL : : return_start ( )
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{
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_state = SubMode : : RETURN_HOME ;
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_state_complete = false ;
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if ( ! wp_nav - > set_wp_destination_loc ( rtl_path . return_target ) ) {
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// failure must be caused by missing terrain data, restart RTL
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restart_without_terrain ( ) ;
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}
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// initialise yaw to point home (maybe)
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auto_yaw . set_mode_to_default ( true ) ;
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}
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// rtl_climb_return_run - implements the initial climb, return home and descent portions of RTL which all rely on the wp controller
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// called by rtl_run at 100hz or more
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void ModeRTL : : climb_return_run ( )
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{
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// if not armed set throttle to zero and exit immediately
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if ( is_disarmed_or_landed ( ) ) {
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make_safe_ground_handling ( ) ;
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return ;
}
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// set motors to full range
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motors - > set_desired_spool_state ( AP_Motors : : DesiredSpoolState : : THROTTLE_UNLIMITED ) ;
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// run waypoint controller
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copter . failsafe_terrain_set_status ( wp_nav - > update_wpnav ( ) ) ;
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// WP_Nav has set the vertical position control targets
// run the vertical position controller and set output throttle
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pos_control - > update_z_controller ( ) ;
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// call attitude controller with auto yaw
attitude_control - > input_thrust_vector_heading ( pos_control - > get_thrust_vector ( ) , auto_yaw . get_heading ( ) ) ;
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// check if we've completed this stage of RTL
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_state_complete = wp_nav - > reached_wp_destination ( ) ;
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}
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// loiterathome_start - initialise return to home
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void ModeRTL : : loiterathome_start ( )
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{
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_state = SubMode : : LOITER_AT_HOME ;
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_state_complete = false ;
_loiter_start_time = millis ( ) ;
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// yaw back to initial take-off heading yaw unless pilot has already overridden yaw
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if ( auto_yaw . default_mode ( true ) ! = AutoYaw : : Mode : : HOLD ) {
auto_yaw . set_mode ( AutoYaw : : Mode : : RESETTOARMEDYAW ) ;
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} else {
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auto_yaw . set_mode ( AutoYaw : : Mode : : HOLD ) ;
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}
}
// rtl_climb_return_descent_run - implements the initial climb, return home and descent portions of RTL which all rely on the wp controller
// called by rtl_run at 100hz or more
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void ModeRTL : : loiterathome_run ( )
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{
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// if not armed set throttle to zero and exit immediately
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if ( is_disarmed_or_landed ( ) ) {
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make_safe_ground_handling ( ) ;
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return ;
}
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// set motors to full range
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motors - > set_desired_spool_state ( AP_Motors : : DesiredSpoolState : : THROTTLE_UNLIMITED ) ;
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// run waypoint controller
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copter . failsafe_terrain_set_status ( wp_nav - > update_wpnav ( ) ) ;
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// WP_Nav has set the vertical position control targets
// run the vertical position controller and set output throttle
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pos_control - > update_z_controller ( ) ;
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// call attitude controller with auto yaw
attitude_control - > input_thrust_vector_heading ( pos_control - > get_thrust_vector ( ) , auto_yaw . get_heading ( ) ) ;
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// check if we've completed this stage of RTL
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if ( ( millis ( ) - _loiter_start_time ) > = ( uint32_t ) g . rtl_loiter_time . get ( ) ) {
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if ( auto_yaw . mode ( ) = = AutoYaw : : Mode : : RESETTOARMEDYAW ) {
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// check if heading is within 2 degrees of heading when vehicle was armed
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if ( abs ( wrap_180_cd ( ahrs . yaw_sensor - copter . initial_armed_bearing ) ) < = 200 ) {
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_state_complete = true ;
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}
} else {
// we have loitered long enough
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_state_complete = true ;
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}
}
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}
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// rtl_descent_start - initialise descent to final alt
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void ModeRTL : : descent_start ( )
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{
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_state = SubMode : : FINAL_DESCENT ;
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_state_complete = false ;
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// initialise altitude target to stopping point
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pos_control - > init_z_controller_stopping_point ( ) ;
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// initialise yaw
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auto_yaw . set_mode ( AutoYaw : : Mode : : HOLD ) ;
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# if AP_LANDINGGEAR_ENABLED
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// optionally deploy landing gear
copter . landinggear . deploy_for_landing ( ) ;
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# endif
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# if AP_FENCE_ENABLED
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// disable the fence on landing
copter . fence . auto_disable_fence_for_landing ( ) ;
# endif
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}
// rtl_descent_run - implements the final descent to the RTL_ALT
// called by rtl_run at 100hz or more
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void ModeRTL : : descent_run ( )
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{
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Vector2f vel_correction ;
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// if not armed set throttle to zero and exit immediately
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if ( is_disarmed_or_landed ( ) ) {
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make_safe_ground_handling ( ) ;
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return ;
}
// process pilot's input
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if ( ! copter . failsafe . radio ) {
if ( ( g . throttle_behavior & THR_BEHAVE_HIGH_THROTTLE_CANCELS_LAND ) ! = 0 & & copter . rc_throttle_control_in_filter . get ( ) > LAND_CANCEL_TRIGGER_THR ) {
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AP : : logger ( ) . Write_Event ( LogEvent : : LAND_CANCELLED_BY_PILOT ) ;
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// exit land if throttle is high
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if ( ! copter . set_mode ( Mode : : Number : : LOITER , ModeReason : : THROTTLE_LAND_ESCAPE ) ) {
copter . set_mode ( Mode : : Number : : ALT_HOLD , ModeReason : : THROTTLE_LAND_ESCAPE ) ;
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}
}
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if ( g . land_repositioning ) {
// apply SIMPLE mode transform to pilot inputs
update_simple_mode ( ) ;
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// convert pilot input to reposition velocity
vel_correction = get_pilot_desired_velocity ( wp_nav - > get_wp_acceleration ( ) * 0.5 ) ;
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// record if pilot has overridden roll or pitch
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if ( ! vel_correction . is_zero ( ) ) {
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if ( ! copter . ap . land_repo_active ) {
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AP : : logger ( ) . Write_Event ( LogEvent : : LAND_REPO_ACTIVE ) ;
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}
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copter . ap . land_repo_active = true ;
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}
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}
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}
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// set motors to full range
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motors - > set_desired_spool_state ( AP_Motors : : DesiredSpoolState : : THROTTLE_UNLIMITED ) ;
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Vector2f accel ;
pos_control - > input_vel_accel_xy ( vel_correction , accel ) ;
pos_control - > update_xy_controller ( ) ;
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// WP_Nav has set the vertical position control targets
// run the vertical position controller and set output throttle
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pos_control - > set_alt_target_with_slew ( rtl_path . descent_target . alt ) ;
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pos_control - > update_z_controller ( ) ;
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// roll & pitch from waypoint controller, yaw rate from pilot
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attitude_control - > input_thrust_vector_heading ( pos_control - > get_thrust_vector ( ) , auto_yaw . get_heading ( ) ) ;
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// check if we've reached within 20cm of final altitude
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_state_complete = labs ( rtl_path . descent_target . alt - copter . current_loc . alt ) < 20 ;
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}
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// land_start - initialise controllers to loiter over home
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void ModeRTL : : land_start ( )
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{
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_state = SubMode : : LAND ;
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_state_complete = false ;
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// set horizontal speed and acceleration limits
pos_control - > set_max_speed_accel_xy ( wp_nav - > get_default_speed_xy ( ) , wp_nav - > get_wp_acceleration ( ) ) ;
pos_control - > set_correction_speed_accel_xy ( wp_nav - > get_default_speed_xy ( ) , wp_nav - > get_wp_acceleration ( ) ) ;
// initialise loiter target destination
if ( ! pos_control - > is_active_xy ( ) ) {
pos_control - > init_xy_controller ( ) ;
}
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// initialise the vertical position controller
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if ( ! pos_control - > is_active_z ( ) ) {
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pos_control - > init_z_controller ( ) ;
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}
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// initialise yaw
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auto_yaw . set_mode ( AutoYaw : : Mode : : HOLD ) ;
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# if AP_LANDINGGEAR_ENABLED
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// optionally deploy landing gear
copter . landinggear . deploy_for_landing ( ) ;
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# endif
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# if AP_FENCE_ENABLED
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// disable the fence on landing
copter . fence . auto_disable_fence_for_landing ( ) ;
# endif
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}
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bool ModeRTL : : is_landing ( ) const
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{
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return _state = = SubMode : : LAND ;
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}
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// land_run - run the landing controllers to put the aircraft on the ground
// called by rtl_run at 100hz or more
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void ModeRTL : : land_run ( bool disarm_on_land )
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{
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// check if we've completed this stage of RTL
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_state_complete = copter . ap . land_complete ;
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// disarm when the landing detector says we've landed
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if ( disarm_on_land & & copter . ap . land_complete & & motors - > get_spool_state ( ) = = AP_Motors : : SpoolState : : GROUND_IDLE ) {
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copter . arming . disarm ( AP_Arming : : Method : : LANDED ) ;
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}
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// if not armed set throttle to zero and exit immediately
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if ( is_disarmed_or_landed ( ) ) {
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make_safe_ground_handling ( ) ;
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return ;
}
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// set motors to full range
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motors - > set_desired_spool_state ( AP_Motors : : DesiredSpoolState : : THROTTLE_UNLIMITED ) ;
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// run normal landing or precision landing (if enabled)
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land_run_normal_or_precland ( ) ;
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}
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void ModeRTL : : build_path ( )
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{
// origin point is our stopping point
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Vector3p stopping_point ;
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pos_control - > get_stopping_point_xy_cm ( stopping_point . xy ( ) ) ;
pos_control - > get_stopping_point_z_cm ( stopping_point . z ) ;
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rtl_path . origin_point = Location ( stopping_point . tofloat ( ) , Location : : AltFrame : : ABOVE_ORIGIN ) ;
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rtl_path . origin_point . change_alt_frame ( Location : : AltFrame : : ABOVE_HOME ) ;
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// compute return target
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compute_return_target ( ) ;
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// climb target is above our origin point at the return altitude
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rtl_path . climb_target = Location ( rtl_path . origin_point . lat , rtl_path . origin_point . lng , rtl_path . return_target . alt , rtl_path . return_target . get_alt_frame ( ) ) ;
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// descent target is below return target at rtl_alt_final
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rtl_path . descent_target = Location ( rtl_path . return_target . lat , rtl_path . return_target . lng , g . rtl_alt_final , Location : : AltFrame : : ABOVE_HOME ) ;
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// set land flag
rtl_path . land = g . rtl_alt_final < = 0 ;
}
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// compute the return target - home or rally point
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// return target's altitude is updated to a higher altitude that the vehicle can safely return at (frame may also be set)
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void ModeRTL : : compute_return_target ( )
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{
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// set return target to nearest rally point or home position (Note: alt is absolute)
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# if HAL_RALLY_ENABLED
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rtl_path . return_target = copter . rally . calc_best_rally_or_home_location ( copter . current_loc , ahrs . get_home ( ) . alt ) ;
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# else
rtl_path . return_target = ahrs . get_home ( ) ;
# endif
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// curr_alt is current altitude above home or above terrain depending upon use_terrain
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int32_t curr_alt = copter . current_loc . alt ;
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// determine altitude type of return journey (alt-above-home, alt-above-terrain using range finder or alt-above-terrain using terrain database)
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ReturnTargetAltType alt_type = ReturnTargetAltType : : RELATIVE ;
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if ( terrain_following_allowed & & ( get_alt_type ( ) = = RTLAltType : : RTL_ALTTYPE_TERRAIN ) ) {
// convert RTL_ALT_TYPE and WPNAV_RFNG_USE parameters to ReturnTargetAltType
switch ( wp_nav - > get_terrain_source ( ) ) {
case AC_WPNav : : TerrainSource : : TERRAIN_UNAVAILABLE :
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alt_type = ReturnTargetAltType : : RELATIVE ;
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AP : : logger ( ) . Write_Error ( LogErrorSubsystem : : NAVIGATION , LogErrorCode : : RTL_MISSING_RNGFND ) ;
gcs ( ) . send_text ( MAV_SEVERITY_CRITICAL , " RTL: no terrain data, using alt-above-home " ) ;
break ;
case AC_WPNav : : TerrainSource : : TERRAIN_FROM_RANGEFINDER :
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alt_type = ReturnTargetAltType : : RANGEFINDER ;
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break ;
case AC_WPNav : : TerrainSource : : TERRAIN_FROM_TERRAINDATABASE :
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alt_type = ReturnTargetAltType : : TERRAINDATABASE ;
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break ;
}
}
// set curr_alt and return_target.alt from range finder
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if ( alt_type = = ReturnTargetAltType : : RANGEFINDER ) {
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if ( copter . get_rangefinder_height_interpolated_cm ( curr_alt ) ) {
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// set return_target.alt
rtl_path . return_target . set_alt_cm ( MAX ( curr_alt + MAX ( 0 , g . rtl_climb_min ) , MAX ( g . rtl_altitude , RTL_ALT_MIN ) ) , Location : : AltFrame : : ABOVE_TERRAIN ) ;
} else {
// fallback to relative alt and warn user
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alt_type = ReturnTargetAltType : : RELATIVE ;
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gcs ( ) . send_text ( MAV_SEVERITY_CRITICAL , " RTL: rangefinder unhealthy, using alt-above-home " ) ;
AP : : logger ( ) . Write_Error ( LogErrorSubsystem : : NAVIGATION , LogErrorCode : : RTL_MISSING_RNGFND ) ;
}
}
// set curr_alt and return_target.alt from terrain database
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if ( alt_type = = ReturnTargetAltType : : TERRAINDATABASE ) {
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// set curr_alt to current altitude above terrain
// convert return_target.alt from an abs (above MSL) to altitude above terrain
// Note: the return_target may be a rally point with the alt set above the terrain alt (like the top of a building)
int32_t curr_terr_alt ;
if ( copter . current_loc . get_alt_cm ( Location : : AltFrame : : ABOVE_TERRAIN , curr_terr_alt ) & &
rtl_path . return_target . change_alt_frame ( Location : : AltFrame : : ABOVE_TERRAIN ) ) {
curr_alt = curr_terr_alt ;
} else {
// fallback to relative alt and warn user
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alt_type = ReturnTargetAltType : : RELATIVE ;
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AP : : logger ( ) . Write_Error ( LogErrorSubsystem : : TERRAIN , LogErrorCode : : MISSING_TERRAIN_DATA ) ;
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gcs ( ) . send_text ( MAV_SEVERITY_CRITICAL , " RTL: no terrain data, using alt-above-home " ) ;
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}
}
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// for the default case we must convert return-target alt (which is an absolute alt) to alt-above-home
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if ( alt_type = = ReturnTargetAltType : : RELATIVE ) {
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if ( ! rtl_path . return_target . change_alt_frame ( Location : : AltFrame : : ABOVE_HOME ) ) {
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// this should never happen but just in case
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rtl_path . return_target . set_alt_cm ( 0 , Location : : AltFrame : : ABOVE_HOME ) ;
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gcs ( ) . send_text ( MAV_SEVERITY_WARNING , " RTL: unexpected error calculating target alt " ) ;
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}
}
// set new target altitude to return target altitude
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// Note: this is alt-above-home or terrain-alt depending upon rtl_alt_type
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// Note: ignore negative altitudes which could happen if user enters negative altitude for rally point or terrain is higher at rally point compared to home
int32_t target_alt = MAX ( rtl_path . return_target . alt , 0 ) ;
// increase target to maximum of current altitude + climb_min and rtl altitude
target_alt = MAX ( target_alt , curr_alt + MAX ( 0 , g . rtl_climb_min ) ) ;
target_alt = MAX ( target_alt , MAX ( g . rtl_altitude , RTL_ALT_MIN ) ) ;
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// reduce climb if close to return target
float rtl_return_dist_cm = rtl_path . return_target . get_distance ( rtl_path . origin_point ) * 100.0f ;
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// don't allow really shallow slopes
if ( g . rtl_cone_slope > = RTL_MIN_CONE_SLOPE ) {
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target_alt = MAX ( curr_alt , MIN ( target_alt , MAX ( rtl_return_dist_cm * g . rtl_cone_slope , curr_alt + RTL_ABS_MIN_CLIMB ) ) ) ;
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}
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// set returned target alt to new target_alt (don't change altitude type)
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rtl_path . return_target . set_alt_cm ( target_alt , ( alt_type = = ReturnTargetAltType : : RELATIVE ) ? Location : : AltFrame : : ABOVE_HOME : Location : : AltFrame : : ABOVE_TERRAIN ) ;
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# if AP_FENCE_ENABLED
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// ensure not above fence altitude if alt fence is enabled
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// Note: because the rtl_path.climb_target's altitude is simply copied from the return_target's altitude,
// if terrain altitudes are being used, the code below which reduces the return_target's altitude can lead to
// the vehicle not climbing at all as RTL begins. This can be overly conservative and it might be better
// to apply the fence alt limit independently on the origin_point and return_target
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if ( ( copter . fence . get_enabled_fences ( ) & AC_FENCE_TYPE_ALT_MAX ) ! = 0 ) {
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// get return target as alt-above-home so it can be compared to fence's alt
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if ( rtl_path . return_target . get_alt_cm ( Location : : AltFrame : : ABOVE_HOME , target_alt ) ) {
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float fence_alt = copter . fence . get_safe_alt_max ( ) * 100.0f ;
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if ( target_alt > fence_alt ) {
// reduce target alt to the fence alt
rtl_path . return_target . alt - = ( target_alt - fence_alt ) ;
}
}
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}
# endif
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// ensure we do not descend
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rtl_path . return_target . alt = MAX ( rtl_path . return_target . alt , curr_alt ) ;
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}
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bool ModeRTL : : get_wp ( Location & destination ) const
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{
// provide target in states which use wp_nav
switch ( _state ) {
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case SubMode : : STARTING :
case SubMode : : INITIAL_CLIMB :
case SubMode : : RETURN_HOME :
case SubMode : : LOITER_AT_HOME :
case SubMode : : FINAL_DESCENT :
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return wp_nav - > get_oa_wp_destination ( destination ) ;
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case SubMode : : LAND :
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return false ;
}
// we should never get here but just in case
return false ;
}
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uint32_t ModeRTL : : wp_distance ( ) const
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{
return wp_nav - > get_wp_distance_to_destination ( ) ;
}
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int32_t ModeRTL : : wp_bearing ( ) const
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{
return wp_nav - > get_wp_bearing_to_destination ( ) ;
}
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// returns true if pilot's yaw input should be used to adjust vehicle's heading
bool ModeRTL : : use_pilot_yaw ( void ) const
{
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const bool allow_yaw_option = ( copter . g2 . rtl_options . get ( ) & uint32_t ( Options : : IgnorePilotYaw ) ) = = 0 ;
const bool land_repositioning = g . land_repositioning & & ( _state = = SubMode : : FINAL_DESCENT ) ;
const bool final_landing = _state = = SubMode : : LAND ;
return allow_yaw_option | | land_repositioning | | final_landing ;
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}
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# endif