|
|
|
@ -50,9 +50,9 @@ FlightTaskManualAltitude::FlightTaskManualAltitude(control::SuperBlock *parent,
@@ -50,9 +50,9 @@ FlightTaskManualAltitude::FlightTaskManualAltitude(control::SuperBlock *parent,
|
|
|
|
|
|
|
|
|
|
bool FlightTaskManualAltitude::activate() |
|
|
|
|
{ |
|
|
|
|
_pos_sp_z = NAN; |
|
|
|
|
_vel_sp_z = 0.0f; |
|
|
|
|
return FlightTaskManualStabilized::activate(); |
|
|
|
|
bool ret = FlightTaskManualStabilized::activate(); |
|
|
|
|
_vel_sp(2) = 0.0f; |
|
|
|
|
return ret; |
|
|
|
|
} |
|
|
|
|
|
|
|
|
|
void FlightTaskManualAltitude::_scaleSticks() |
|
|
|
@ -62,7 +62,7 @@ void FlightTaskManualAltitude::_scaleSticks()
@@ -62,7 +62,7 @@ void FlightTaskManualAltitude::_scaleSticks()
|
|
|
|
|
|
|
|
|
|
/* Scale horizontal velocity with expo curve stick input*/ |
|
|
|
|
const float vel_max_z = (_sticks(2) > 0.0f) ? _vel_max_down.get() : _vel_max_up.get(); |
|
|
|
|
_vel_sp_z = vel_max_z * _sticks_expo(2); |
|
|
|
|
_vel_sp(2) = vel_max_z * _sticks_expo(2); |
|
|
|
|
} |
|
|
|
|
|
|
|
|
|
void FlightTaskManualAltitude::_updateAltitudeLock() |
|
|
|
@ -72,20 +72,23 @@ void FlightTaskManualAltitude::_updateAltitudeLock()
@@ -72,20 +72,23 @@ void FlightTaskManualAltitude::_updateAltitudeLock()
|
|
|
|
|
*/ |
|
|
|
|
|
|
|
|
|
/* handle position and altitude hold */ |
|
|
|
|
const bool apply_brake_z = fabsf(_vel_sp_z) <= FLT_EPSILON; |
|
|
|
|
const bool apply_brake_z = fabsf(_vel_sp(2)) <= FLT_EPSILON; |
|
|
|
|
const bool stopped_z = (_vel_hold_thr_z.get() < FLT_EPSILON || fabsf(_velocity(2)) < _vel_hold_thr_z.get()); |
|
|
|
|
|
|
|
|
|
if (apply_brake_z && stopped_z && !PX4_ISFINITE(_pos_sp_z)) { |
|
|
|
|
_pos_sp_z = _position(2); |
|
|
|
|
if (apply_brake_z && stopped_z && !PX4_ISFINITE(_pos_sp(2))) { |
|
|
|
|
_pos_sp(2) = _position(2); |
|
|
|
|
|
|
|
|
|
} else if (!apply_brake_z) { |
|
|
|
|
_pos_sp_z = NAN; |
|
|
|
|
_pos_sp(2) = NAN; |
|
|
|
|
} |
|
|
|
|
} |
|
|
|
|
|
|
|
|
|
void FlightTaskManualAltitude::_updateSetpoints() |
|
|
|
|
{ |
|
|
|
|
FlightTaskManualStabilized::_updateSetpoints(); // get yaw setpoint
|
|
|
|
|
FlightTaskManualStabilized::_updateSetpoints(); // get yaw and thrust setpoints
|
|
|
|
|
|
|
|
|
|
_thr_sp *= NAN; // Don't need thrust setpoint from Stabilized mode.
|
|
|
|
|
|
|
|
|
|
/* Thrust in xy are extracted directly from stick inputs. A magnitude of
|
|
|
|
|
* 1 means that maximum thrust along xy is required. A magnitude of 0 means no |
|
|
|
|
* thrust along xy is required. The maximum thrust along xy depends on the thrust |
|
|
|
@ -101,19 +104,5 @@ void FlightTaskManualAltitude::_updateSetpoints()
@@ -101,19 +104,5 @@ void FlightTaskManualAltitude::_updateSetpoints()
|
|
|
|
|
_thr_sp(0) = sp(0); |
|
|
|
|
_thr_sp(1) = sp(1); |
|
|
|
|
|
|
|
|
|
_updateAltitudeLock(); // get z setpoints
|
|
|
|
|
} |
|
|
|
|
|
|
|
|
|
bool FlightTaskManualAltitude::update() |
|
|
|
|
{ |
|
|
|
|
_scaleSticks(); |
|
|
|
|
_updateSetpoints(); |
|
|
|
|
|
|
|
|
|
_setPositionSetpoint(Vector3f(NAN, NAN, _pos_sp_z)); |
|
|
|
|
_setVelocitySetpoint(Vector3f(NAN, NAN, _vel_sp_z)); |
|
|
|
|
_setYawSetpoint(_yaw_sp); |
|
|
|
|
_setYawspeedSetpoint(_yaw_rate_sp); |
|
|
|
|
_setThrustSetpoint(Vector3f(_thr_sp(0), _thr_sp(1), NAN)); |
|
|
|
|
|
|
|
|
|
return true; |
|
|
|
|
_updateAltitudeLock(); |
|
|
|
|
} |
|
|
|
|