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MultiCopterLandDetector: Implement ModuleParams inheritance (#12356)
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@@ -52,6 +52,7 @@
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#include <uORB/topics/actuator_controls.h>
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#include <uORB/topics/battery_status.h>
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#include <uORB/topics/parameter_update.h>
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#include <uORB/topics/sensor_bias.h>
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#include <uORB/topics/vehicle_acceleration.h>
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#include <uORB/topics/vehicle_angular_velocity.h>
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#include <uORB/topics/vehicle_attitude.h>
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@@ -81,6 +82,14 @@ protected:
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float _get_max_altitude() override;
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private:
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/* get control mode dependent pilot throttle threshold with which we should quit landed state and take off */
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float _get_takeoff_throttle();
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bool _has_low_thrust();
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bool _has_minimal_thrust();
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bool _has_altitude_lock();
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bool _has_position_lock();
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bool _is_climb_rate_enabled();
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/** Time in us that landing conditions have to hold before triggering a land. */
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static constexpr hrt_abstime LAND_DETECTOR_TRIGGER_TIME_US = 300_ms;
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@@ -97,35 +106,22 @@ private:
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* @brief Handles for interesting parameters
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**/
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struct {
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param_t maxClimbRate;
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param_t maxVelocity;
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param_t maxRotation;
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param_t minThrottle;
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param_t hoverThrottle;
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param_t minManThrottle;
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param_t freefall_acc_threshold;
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param_t freefall_trigger_time;
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param_t altitude_max;
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param_t landSpeed;
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param_t low_thrust_threshold;
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} _paramHandle{};
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struct {
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float maxClimbRate;
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float maxVelocity;
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float maxRotation_rad_s;
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float minThrottle;
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float hoverThrottle;
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float minManThrottle;
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float freefall_acc_threshold;
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float freefall_trigger_time;
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float altitude_max;
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float landSpeed;
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float low_thrust_threshold;
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} _params{};
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uORB::Subscription _actuator_controls_sub{ORB_ID(actuator_controls_0)};
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uORB::Subscription _battery_sub{ORB_ID(battery_status)};
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uORB::Subscription _sensor_bias_sub{ORB_ID(sensor_bias)};
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uORB::Subscription _vehicle_acceleration_sub{ORB_ID(vehicle_acceleration)};
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uORB::Subscription _vehicle_angular_velocity_sub{ORB_ID(vehicle_angular_velocity)};
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uORB::Subscription _vehicle_attitude_sub{ORB_ID(vehicle_attitude)};
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@@ -136,7 +132,7 @@ private:
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actuator_controls_s _actuator_controls {};
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battery_status_s _battery_status {};
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vehicle_control_mode_s _control_mode {};
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vehicle_acceleration_s _vehicle_acceleration{};
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vehicle_acceleration_s _vehicle_acceleration{};
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vehicle_attitude_s _vehicle_attitude {};
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vehicle_angular_velocity_s _vehicle_angular_velocity{};
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vehicle_local_position_s _vehicle_local_position {};
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@@ -148,14 +144,16 @@ private:
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bool _in_descend{false}; ///< vehicle is desending
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bool _horizontal_movement{false}; ///< vehicle is moving horizontally
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/* get control mode dependent pilot throttle threshold with which we should quit landed state and take off */
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float _get_takeoff_throttle();
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bool _has_altitude_lock();
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bool _has_position_lock();
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bool _has_minimal_thrust();
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bool _has_low_thrust();
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bool _is_climb_rate_enabled();
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DEFINE_PARAMETERS_CUSTOM_PARENT(
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LandDetector,
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(ParamFloat<px4::params::LNDMC_ALT_MAX>) _param_lndmc_alt_max,
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(ParamFloat<px4::params::LNDMC_FFALL_THR>) _param_lndmc_ffall_thr,
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(ParamFloat<px4::params::LNDMC_FFALL_TTRI>) _param_lndmc_ffall_ttri,
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(ParamFloat<px4::params::LNDMC_LOW_T_THR>) _param_lndmc_low_t_thr,
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(ParamFloat<px4::params::LNDMC_ROT_MAX>) _param_lndmc_rot_max,
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(ParamFloat<px4::params::LNDMC_XY_VEL_MAX>) _param_lndmc_xy_vel_max,
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(ParamFloat<px4::params::LNDMC_Z_VEL_MAX>) _param_lndmc_z_vel_max
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);
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};
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} // namespace land_detector
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