| http://www.w3.org/ns/prov#value | - In this approach,signals available on an aircraft, such as airspeed, controlattitudes, accelerations, altitude, and rates of pitch, roll,and yaw, are processed into desired output loads such asfore/aft cyclic boost tube oscillatory axial load (OAL),lateral cyclic boost tube OAL, collective boost tube OAL,main rotor pitch link OAL, etc.
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