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AirspeedValidator: remove unused variable _tas_gate

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Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
This commit is contained in:
Silvan Fuhrer
2022-01-13 10:40:02 +01:00
committed by Daniel Agar
parent 3b6c9448aa
commit 1a4b2b37bb
1 changed files with 0 additions and 2 deletions
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src/modules/airspeed_selector/AirspeedValidator.hpp
-2
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@@ -98,7 +98,6 @@ public:
void set_wind_estimator_beta_noise(float beta_var) { _wind_estimator.set_beta_noise(beta_var); } void set_wind_estimator_beta_noise(float beta_var) { _wind_estimator.set_beta_noise(beta_var); }
void set_wind_estimator_tas_gate(uint8_t gate_size) void set_wind_estimator_tas_gate(uint8_t gate_size)
{ {
_tas_gate = gate_size;
_wind_estimator.set_tas_gate(gate_size); _wind_estimator.set_tas_gate(gate_size);
} }
@@ -147,7 +146,6 @@ private:
static constexpr uint64_t DATA_STUCK_TIMEOUT{2_s}; ///< timeout after which data stuck check triggers when data is flat static constexpr uint64_t DATA_STUCK_TIMEOUT{2_s}; ///< timeout after which data stuck check triggers when data is flat
// states of innovation check // states of innovation check
float _tas_gate{1.0f}; ///< gate size of airspeed innovation (to calculate tas_test_ratio)
bool _innovations_check_failed{false}; ///< true when airspeed innovations have failed consistency checks bool _innovations_check_failed{false}; ///< true when airspeed innovations have failed consistency checks
float _tas_innov_threshold{1.0}; ///< innovation error threshold for triggering innovation check failure float _tas_innov_threshold{1.0}; ///< innovation error threshold for triggering innovation check failure
float _tas_innov_integ_threshold{-1.0}; ///< integrator innovation error threshold for triggering innovation check failure float _tas_innov_integ_threshold{-1.0}; ///< integrator innovation error threshold for triggering innovation check failure