ASD Technical Report, Numéro 60

Accelerometer adaptive channels adaptive controller adaptive gain aerodynamic Airborne Analyzer aircraft analog computer angle of attack autopilot checkout command configuration control stick control surface d-c signals damper damping dead band dead zone deg/sec degrees per second DEMODULATOR disengage monitor dual electrical engaged error Figure fixed gain flight conditions Flight Control System frequency function selector gain changer hardover failure high-passed hold mode Honeywell hydraulic hysteresis inertial lateral acceleration Lead Amplifier limit cycle loop maximum MH-96 system mission normal acceleration notch filter operation oscillation performance pickoff pilot pitch attitude pitch axis pitch rate PITCH STICK PORT SERVO position transmitter rate feedback re-entry reaction control system REACTION THRUST redundant reliability response roll attitude roll axis ROLL RATE Root Locus rudder pedal Section I Volume SERVO AMPLIFIER SERVO DISPLACEMENT SERVO MONITOR side stick stick inputs surface effectiveness switch amplifier synchronizer transient vehicle volts yaw axis YAW RATE zero