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SECTION IE OPERATIONAL AND FUNCTIONAL ANALYSES
Table Page 1 Feedback Parameters
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accelerometers actuator adaptive controller adaptive dampers adaptive gain aerodynamic airborne analyzer aircraft analog computer angle of attack autopilot ballistic checkout command configuration control surface damping dead band dead zone deg/sec degrees per second disengage displacement engaged error evaluation fixed gain fixed-gain flight conditions flight control system Flight Line Analyzer flight test program frequency function selector gain changer gain computer gyro high-passed hold mode Honeywell hydraulic indicated malfunction inertial launch limit cycle loop maximum MH-96 system normal acceleration nose notch filter operation oscillation output pass Must pass performance pickoff pilot pitch attitude pitch axis pitch rate plasma jet potentiometers pulse pyrometer rate feedback re-entry reaction control system redundant response roll attitude roll axis roll rate rudder pedal servo servo amplifier side stick sideslip signals simulator stick inputs surface effectiveness switch switch amplifier temperature three axes transients valve yaw axis yaw rate zero