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
Conference paper
No indication
English
Wiley | 2000
|SHIP-LANDING EVALUATION DISPLAY SYSTEM AND SHIP-LANDING EVALUATION DISPLAY METHOD
European Patent Office | 2024
|Wiley | 2000
|