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Evaluation of a Set of Optimized Aerodynamic Computer Equations for
Human Reliability in Manned Space SystemsEstimation and Verification
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aerodynamic aeroelastic aircraft airframe airplane analog computer analysis angle of attack angular approach assumed mode methods attitude axis basic boundary characteristics cockpit coefficient configuration constant control system crew crew station damping damping ratio deflection device display Dutch roll dynamic effect elastic Engineering equations equipment error evaluation exit pupil experimental factors ﬂight flight simulator force frequency function gain handling qualities hover human reliability initial input integrated landing linear longitudinal loop maneuver measurement missile mission mode shapes motion nonlinear obtained operational optimum panel parameters performance period pole phase phugoid pilot rating pitch rate pitching moment pressure problem radar ratio reference response roll scale screen sensitivity sequence break shown in Figure solution speed stability static stick structural surface target task technique throttle thrust tion trainer trajectory values variables variation vehicle velocity visual simulation VTOL wing zero