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US09026377B2 Method and system for detecting forces on aircraft 有权
用于检测飞机上的力的方法和系统

Method and system for detecting forces on aircraft
Abstract:
A method for sensing a force applied to an aircraft includes receiving a derivative of the acceleration of a motion of a portion of the aircraft, determining whether the derivative of the acceleration of the motion of the portion of the aircraft exceeds a threshold, and outputting an indication that a force has been applied to the portion of the aircraft responsive to determining that the derivative of the acceleration of motion of the portion of the aircraft exceeds the threshold.
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