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https://gitee.com/mirrors_PX4/PX4-Autopilot.git
synced 2026-10-31 02:11:35 +08:00
FlightTask: move position and stick data subscription into tasks, Orbit introduce variable center position
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@@ -49,6 +49,7 @@ class FlightTaskManual : public FlightTask
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public:
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FlightTaskManual(SuperBlock *parent, const char *name) :
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FlightTask(parent, name),
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_sub_manual_control_setpoint(ORB_ID(manual_control_setpoint), 0, 0, &getSubscriptions()),
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_xy_vel_man_expo(parent, "MPC_XY_MAN_EXPO", false),
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_z_vel_man_expo(parent, "MPC_Z_MAN_EXPO", false),
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_hold_dz(parent, "MPC_HOLD_DZ", false),
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@@ -103,13 +104,11 @@ public:
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*/
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virtual int update()
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{
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FlightTask::update();
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int ret = FlightTask::update();
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ret += _evaluate_sticks();
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/* prepare stick input */
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matrix::Vector2f stick_xy; /**< horizontal two dimensional stick input within a unit circle */
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stick_xy(0) = math::expo_deadzone(_sticks(0), _xy_vel_man_expo.get(), _hold_dz.get());
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stick_xy(1) = math::expo_deadzone(_sticks(1), _xy_vel_man_expo.get(), _hold_dz.get());
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float stick_z = -math::expo_deadzone(_sticks(2), _z_vel_man_expo.get(), _hold_dz.get());
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matrix::Vector2f stick_xy(_sticks.data()); /**< horizontal two dimensional stick input within a unit circle */
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const float stick_xy_norm = stick_xy.norm();
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@@ -119,7 +118,7 @@ public:
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}
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/* rotate stick input to produce velocity setpoint in NED frame */
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matrix::Vector3f velocity_setpoint(stick_xy(0), stick_xy(1), stick_z);
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matrix::Vector3f velocity_setpoint(stick_xy(0), stick_xy(1), _sticks(3));
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velocity_setpoint = matrix::Dcmf(matrix::Eulerf(0.0f, 0.0f, get_input_frame_yaw())) * velocity_setpoint;
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/* scale [0,1] length velocity vector to maximal manual speed (in m/s) */
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@@ -129,14 +128,14 @@ public:
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velocity_setpoint = velocity_setpoint.emult(vel_scale);
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/* smooth out velocity setpoint by slewrate and return it */
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vel_sp_slewrate(velocity_setpoint, stick_xy, stick_z);
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vel_sp_slewrate(velocity_setpoint, stick_xy, _sticks(3));
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_set_velocity_setpoint(velocity_setpoint);
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/* handle position and altitude hold */
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const bool stick_xy_zero = stick_xy_norm <= FLT_EPSILON;
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const bool stick_z_zero = fabsf(stick_z) <= FLT_EPSILON;
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const bool stick_z_zero = fabsf(_sticks(3)) <= FLT_EPSILON;
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float velocity_xy_norm = matrix::Vector2f(_velocity._data).norm();
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float velocity_xy_norm = matrix::Vector2f(_velocity.data()).norm();
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const bool stopped_xy = (_hold_max_xy.get() < FLT_EPSILON || velocity_xy_norm < _hold_max_xy.get());
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const bool stopped_z = (_hold_max_z.get() < FLT_EPSILON || fabsf(_velocity(2)) < _hold_max_z.get());
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@@ -157,16 +156,20 @@ public:
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}
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_set_position_setpoint(_hold_position);
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return 0;
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return ret;
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};
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protected:
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matrix::Vector<float, 4> _sticks;
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float get_input_frame_yaw()
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{
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return _yaw;
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};
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private:
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uORB::Subscription<manual_control_setpoint_s> _sub_manual_control_setpoint;
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control::BlockParamFloat _xy_vel_man_expo; /**< ratio of exponential curve for stick input in xy direction pos mode */
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control::BlockParamFloat _z_vel_man_expo; /**< ratio of exponential curve for stick input in xy direction pos mode */
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control::BlockParamFloat _hold_dz; /**< deadzone around the center for the sticks when flying in position mode */
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@@ -178,6 +181,27 @@ private:
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matrix::Vector3f _hold_position; /**< position at which the vehicle stays while the input is zero velocity */
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int _evaluate_sticks()
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{
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if (hrt_elapsed_time(&_sub_manual_control_setpoint.get().timestamp) < _timeout) {
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/* get data and scale correctly */
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_sticks(0) = _sub_manual_control_setpoint.get().x; /* NED x, "pitch" [-1,1] */
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_sticks(1) = _sub_manual_control_setpoint.get().y; /* NED y, "roll" [-1,1] */
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_sticks(2) = -(_sub_manual_control_setpoint.get().z - 0.5f) * 2.f; /* NED z, "thrust" resacaled from [0,1] to [-1,1] */
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_sticks(3) = _sub_manual_control_setpoint.get().r; /* "yaw" [-1,1] */
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/* apply expo and deadzone */
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_sticks(0) = math::expo_deadzone(_sticks(0), _xy_vel_man_expo.get(), _hold_dz.get());
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_sticks(1) = math::expo_deadzone(_sticks(1), _xy_vel_man_expo.get(), _hold_dz.get());
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_sticks(2) = math::expo_deadzone(_sticks(2), _z_vel_man_expo.get(), _hold_dz.get());
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return 0;
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} else {
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_sticks.zero(); /* default is all zero */
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return 1;
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}
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}
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/* --- Acceleration Smoothing --- */
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