mirror of
https://gitee.com/mirrors_PX4/PX4-Autopilot.git
synced 2026-04-14 10:07:39 +08:00
FlightTaskManualAltitude: brake depends on acceleration; description clean up
This commit is contained in:
parent
09bf73945a
commit
deac27ee52
@ -49,14 +49,17 @@ FlightTaskManualAltitude::FlightTaskManualAltitude(control::SuperBlock *parent,
|
||||
FlightTaskManual(parent, name),
|
||||
_vel_max_down(parent, "MPC_Z_VEL_MAX_DN", false),
|
||||
_vel_max_up(parent, "MPC_Z_VEL_MAX_UP", false),
|
||||
_yaw_rate_scaling(parent, "MPC_MAN_Y_MAX", false)
|
||||
_yaw_rate_scaling(parent, "MPC_MAN_Y_MAX", false),
|
||||
_acc_max_up(parent, "MPC_ACC_UP_MAX", false),
|
||||
_acc_max_down(parent, "MPC_ACC_DOWN_MAX", false)
|
||||
{}
|
||||
|
||||
bool FlightTaskManualAltitude::activate()
|
||||
{
|
||||
_pos_sp_predicted = _pos_sp_z = _position(2);
|
||||
_yaw_sp_predicted = _yaw_sp = _yaw;
|
||||
_yaw_rate_sp = _vel_sp_z = NAN;
|
||||
_lock_time = 0.0f;
|
||||
_lock_time_max = 1.0f; // 1s time to brake as default
|
||||
|
||||
return FlightTaskManual::activate();
|
||||
}
|
||||
@ -64,7 +67,7 @@ bool FlightTaskManualAltitude::activate()
|
||||
void FlightTaskManualAltitude::scaleSticks()
|
||||
{
|
||||
|
||||
/* map stick to velocity */
|
||||
/* Map stick to velocity */
|
||||
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);
|
||||
_yaw_rate_sp = _sticks(3) * math::radians(_yaw_rate_scaling.get());
|
||||
@ -74,12 +77,12 @@ void FlightTaskManualAltitude::scaleSticks()
|
||||
void FlightTaskManualAltitude::updateHeadingSetpoints()
|
||||
{
|
||||
if (fabsf(_sticks(3)) < FLT_EPSILON) {
|
||||
/* want to hold yaw */
|
||||
/* Want to hold yaw */
|
||||
_yaw_rate_sp = NAN;
|
||||
_yaw_sp = _yaw_sp_predicted;
|
||||
|
||||
} else {
|
||||
/* want to change yaw based on yaw-rate */
|
||||
/* Want to change yaw based on yaw-rate */
|
||||
_yaw_sp = NAN;
|
||||
_yaw_sp_predicted = _wrap_pi(_yaw_sp_predicted + _yaw_rate_sp * _deltatime);
|
||||
}
|
||||
@ -88,14 +91,37 @@ void FlightTaskManualAltitude::updateHeadingSetpoints()
|
||||
void FlightTaskManualAltitude::updateZsetpoints()
|
||||
{
|
||||
if (fabsf(_sticks(2)) < FLT_EPSILON) {
|
||||
/* want to hold altitude */
|
||||
_vel_sp_z = NAN;
|
||||
_pos_sp_z = _pos_sp_predicted;
|
||||
|
||||
/* Want to hold altitude */
|
||||
|
||||
if (_lock_time <= _lock_time_max) {
|
||||
/* Don't lock: time has not been reached */
|
||||
_vel_sp_z = 0.0f;
|
||||
_pos_sp_z = NAN;
|
||||
_lock_time += _deltatime;
|
||||
|
||||
} else {
|
||||
_vel_sp_z = NAN;
|
||||
_pos_sp_z = _position(2);
|
||||
}
|
||||
|
||||
} else {
|
||||
/* want to change altitude through velocity */
|
||||
/* Want to change altitude through velocity */
|
||||
_pos_sp_z = NAN;
|
||||
_pos_sp_predicted = _position(2) + _vel_sp_z * _deltatime;
|
||||
|
||||
/* Maximum brake acceleration depends
|
||||
* on direction.
|
||||
*/
|
||||
float brake_acc = (_velocity(2) > 0.0f) ? _acc_max_up.get() : _acc_max_down.get();
|
||||
|
||||
if (PX4_ISFINITE(brake_acc)) {
|
||||
_lock_time_max = fabsf(_velocity(2)) / brake_acc;
|
||||
|
||||
} else {
|
||||
_lock_time_max = 1.0f; // 1 second time to brake if no acceleration is set
|
||||
}
|
||||
|
||||
_lock_time = 0.0f;
|
||||
}
|
||||
}
|
||||
|
||||
|
||||
@ -54,15 +54,17 @@ public:
|
||||
bool update() override;
|
||||
|
||||
protected:
|
||||
|
||||
float _vel_sp_z{0.0f}; /**< scaled velocity directly from stick */
|
||||
float _yaw_rate_sp{0.0f}; /** scaled yaw rate directly from stick */
|
||||
float _pos_sp_z{0.0f};
|
||||
float _yaw_sp{0.0f};
|
||||
float _yaw_rate_sp{0.0f}; /** scaled yaw rate directly from stick. NAN if yaw is locked */
|
||||
float _yaw_sp{0.0f}; /** yaw setpoint once locked. otherwise NAN */
|
||||
float _yaw_sp_predicted{0.0f}; /** _yaw_sp during lock; predicted yaw through _yaw_rate_sp demand */
|
||||
float _vel_sp_z{0.0f}; /**< scaled velocity directly from stick. During altitude lock is equal to NAN */
|
||||
float _pos_sp_z{0.0f}; /**< position setpoint in z during lock. Otherwise NAN. */
|
||||
|
||||
control::BlockParamFloat _vel_max_down; /**< maximum speed allowed to go up */
|
||||
control::BlockParamFloat _vel_max_up; /**< maximum speed allowed to go down */
|
||||
control::BlockParamFloat _yaw_rate_scaling; /**< scaling factor from stick to yaw rate */
|
||||
control::BlockParamFloat _acc_max_up; /**< maximum acceleration upward */
|
||||
control::BlockParamFloat _acc_max_down; /**< maximum acceleration downward */
|
||||
|
||||
virtual void updateSetpoints(); /**< updates all setpoints */
|
||||
virtual void scaleSticks(); /**< scales sticks to velocity */
|
||||
@ -71,7 +73,6 @@ private:
|
||||
void updateHeadingSetpoints(); /**< sets yaw or yaw speed */
|
||||
void updateZsetpoints(); /**< sets position or velocity setpoint */
|
||||
|
||||
float _pos_sp_predicted{0.0f}; /**< position setpoint computed in set_z_setpoints */
|
||||
float _yaw_sp_predicted{0.0f}; /**< yaw setpoint computed in set_heading_setpoints */
|
||||
|
||||
float _lock_time_max{0.0f}; /**< defines time when altitude lock occurs */
|
||||
float _lock_time{0.0f}; /**< time after stick are at zero position */
|
||||
};
|
||||
|
||||
Loading…
x
Reference in New Issue
Block a user