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FW LandDetector: disregard horizontal velocity if local_position.v_xy_valid is false #24133

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11 changes: 10 additions & 1 deletion src/modules/land_detector/FixedwingLandDetector.cpp
Original file line number Diff line number Diff line change
Expand Up @@ -114,6 +114,14 @@ bool FixedwingLandDetector::_get_landed_state()
const float acc_hor = matrix::Vector2f(_acceleration).norm();
_xy_accel_filtered = _xy_accel_filtered * 0.8f + acc_hor * 0.18f;

// Check for angular velocity (disregard yaw)
float max_rotation_threshold = math::radians(_param_lndfw_rot_max.get());
val = _angular_velocity.xy().norm(); // TODO: check if this should be low pass filtered
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in MC landing detector the angular velocity is not filtered. Unsure if it might be necessary for FW - I don't know how noisy the data usually is in comparison.


if (PX4_ISFINITE(val)) {
_velocity_rotational = val;
}

// make groundspeed threshold tighter if airspeed is invalid
const float vel_xy_max_threshold = airspeed_invalid ? 0.7f * _param_lndfw_vel_xy_max.get() :
_param_lndfw_vel_xy_max.get();
Expand All @@ -122,7 +130,8 @@ bool FixedwingLandDetector::_get_landed_state()
landDetected = _airspeed_filtered < _param_lndfw_airspd.get()
&& _velocity_xy_filtered < vel_xy_max_threshold
&& _velocity_z_filtered < _param_lndfw_vel_z_max.get()
&& _xy_accel_filtered < _param_lndfw_xyaccel_max.get();
&& _xy_accel_filtered < _param_lndfw_xyaccel_max.get()
&& _velocity_rotational < max_rotation_threshold;

} else {
// Control state topic has timed out and we need to assume we're landed.
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2 changes: 2 additions & 0 deletions src/modules/land_detector/FixedwingLandDetector.h
Original file line number Diff line number Diff line change
Expand Up @@ -75,13 +75,15 @@ class FixedwingLandDetector final : public LandDetector
float _velocity_xy_filtered{0.0f};
float _velocity_z_filtered{0.0f};
float _xy_accel_filtered{0.0f};
float _velocity_rotational{0.0f};

DEFINE_PARAMETERS_CUSTOM_PARENT(
LandDetector,
(ParamFloat<px4::params::LNDFW_XYACC_MAX>) _param_lndfw_xyaccel_max,
(ParamFloat<px4::params::LNDFW_AIRSPD_MAX>) _param_lndfw_airspd,
(ParamFloat<px4::params::LNDFW_VEL_XY_MAX>) _param_lndfw_vel_xy_max,
(ParamFloat<px4::params::LNDFW_VEL_Z_MAX>) _param_lndfw_vel_z_max,
(ParamFloat<px4::params::LNDFW_ROT_MAX>) _param_lndfw_rot_max,
(ParamFloat<px4::params::LNDFW_TRIG_TIME>) _param_lndfw_trig_time
);
};
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11 changes: 11 additions & 0 deletions src/modules/land_detector/land_detector_params_fw.c
Original file line number Diff line number Diff line change
Expand Up @@ -102,3 +102,14 @@ PARAM_DEFINE_FLOAT(LNDFW_AIRSPD_MAX, 6.00f);
* @group Land Detector
*/
PARAM_DEFINE_FLOAT(LNDFW_TRIG_TIME, 2.f);

/**
* Fixed-wing land detector: max rotation
*
* Maximum allowed angular velocity around each axis allowed in the landed state.
*
* @unit deg/s
* @decimal 1
* @group Land Detector
*/
PARAM_DEFINE_FLOAT(LNDFW_ROT_MAX, 5.0f);
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I made up this default value - needs to be verified/adjusted.

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