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AirspeedSelector: do checks for data stopped in airspeed selector, not validator
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
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@@ -78,6 +78,8 @@ public:
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void update_airspeed_validator(const airspeed_validator_update_data &input_data);
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void reset_airspeed_to_invalid(const uint64_t timestamp);
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float get_IAS() { return _IAS; }
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float get_CAS() { return _CAS; }
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float get_TAS() { return _TAS; }
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@@ -125,12 +127,6 @@ private:
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float _TAS{0.0f}; ///< true airspeed in m/s
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float _CAS_scale{1.0f}; ///< scale factor from IAS to CAS
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uint64_t _time_last_airspeed{0}; ///< time last airspeed measurement was received (uSec)
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// states of data stopped check
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bool _data_stopped_failed{false}; ///< data_stopp check has detected failure
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hrt_abstime _previous_airspeed_timestamp{0}; ///< timestamp from previous measurement input, to check validity of measurement
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// states of innovation check
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float _tas_gate{1.0f}; ///< gate size of airspeed innovation (to calculate tas_test_ratio)
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bool _innovations_check_failed{false}; ///< true when airspeed innovations have failed consistency checks
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@@ -149,7 +145,7 @@ private:
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float _load_factor_ratio{0.5f}; ///< ratio of maximum load factor predicted by stall speed to measured load factor
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// states of airspeed valid declaration
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bool _airspeed_valid{false}; ///< airspeed valid (pitot or groundspeed-windspeed)
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bool _airspeed_valid{true}; ///< airspeed valid (pitot or groundspeed-windspeed)
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int _checks_fail_delay{3}; ///< delay for airspeed invalid declaration after single check failure (Sec)
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int _checks_clear_delay{3}; ///< delay for airspeed valid declaration after all checks passed again (Sec)
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uint64_t _time_checks_passed{0}; ///< time the checks have last passed (uSec)
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@@ -167,5 +163,6 @@ private:
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float estimator_status_mag_test_ratio);
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void check_load_factor(float accel_z);
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void update_airspeed_valid_status(const uint64_t timestamp);
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void reset();
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};
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