A pilot-vehicle-display model is used to study information and display requirements and the effects on system performance and reliability of pilot-induced randomness, wind gusts, configurational changes, etc. A brief description of a control theoretic systems model is given and its use and validity are demonstrated by applying it in a piloted approach to landing situation. The analysis procedure assumes that the vehicle dynamics are represented by linearized equations of motion.
Analytic evaluation of display requirements for approach to landing
1972-01-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
Wiley | 2000
|Wiley | 2000
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