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公开(公告)号:US11422150B2
公开(公告)日:2022-08-23
申请号:US17007364
申请日:2020-08-31
申请人: Aerosonic LLC
发明人: Rick Snyder , Charles Lang
摘要: An aircraft airflow sensor probe configured to correct measurements based on aircraft movement includes a vane assembly configured to sense a direction of local airflow outside an aircraft, at least one accelerometer configured to detect aircraft movement, a sensor configured to sense and output a rotational position of the vane assembly, and an angle of attack processor configured to determine at least a measured angle of attack of the aircraft based on the rotational position of the vane assembly. The angle of attack processor further configured to determine a correction value based on the aircraft movement data provided by the at least one accelerometer and output a corrected angle of attack of the aircraft.