An optimal control approach has been used to model pilot performance during STOL flare and landing. The model is used to predict pilot landing performance for three STOL configurations, each having a different level of automatic control augmentation. Model predictions are compared with flight simulator data. It is concluded that the model can be effective design tool for studying analytically the effects of display modifications, different stability augmentation systems, and proposed changes in the landing area geometry.
A predictive pilot model for STOL aircraft landing
01.03.1974
Report
Keine Angabe
Englisch
A predictive pilot model for STOL aircraft landing
TIBKAT | 1974
|Arrested landing studies for STOL aircraft
AIAA | 1973
|Arrested Landing Studies for STOL Aircraft
AIAA | 1974
|STOL aircraft flight and landing area considerations.
NTRS | 1973
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