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AP_NavEKF: remove unused variables
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@ -80,7 +80,6 @@ private:
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float accel_gain; // gain from accel vector tilt error to rate gyro correction used by AHRS calculation
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Vector3f ahrs_accel; // filtered body frame specific force vector used by AHRS calculation (m/s/s)
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float ahrs_accel_norm; // length of body frame specific force vector used by AHRS calculation (m/s/s)
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bool ahrs_turn_comp_enabled; // true when compensation for centripetal acceleration in coordinated turns using true airspeed is being used.
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float true_airspeed; // true airspeed used to correct for centripetal acceleratoin in coordinated turns (m/s)
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// Runs quaternion prediction for the selected AHRS using IMU (and optionally true airspeed) data
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