Automatic fore-aft detection for an aircraft
作者： T. Todd Griffith
DOI:
关键词: Landing gear 、 Orientation (geometry) 、 Clockwise 、 Accelerometer 、 Engineering 、 Acceleration 、 Acoustics 、 Brake control 、 Automotive engineering
摘要: An automatic fore/aft detection procedure as described herein may be implemented in connection with an aircraft brake control system that utilizes wheel-mounted accelerometers detect landing gear acceleration for purposes of antiskid control. The automatically determines the is moving a forward direction based upon current wheel speed and rotational wheels. Once detected, assigned to each (clockwise or counterclockwise) orientation can accelerometer wheel.
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