The problem of pilot performance estimates during the aircraft design phase is discussed. The following are found to influence such estimates: low altitude turbulence model, aircraft model, mission model and pilot response model. Pilot responses to stochastic gust disturbances are evaluated and the aircraft transfer functions are calculated. Flight controllers are needed for low altitude flight. Elastic degrees of aircraft motion should be included in the calculation. (Author)
On the Question of Pilot Deterioration During Low Altitude Flight
1974
20 pages
Report
Keine Angabe
Englisch
Effect of Gas Turbine Engine Deterioration on Flight Speed-Altitude Performances
British Library Conference Proceedings | 1996
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