A computer-aided optimal pilot modeling procedure was utilized to develop flight director laws for implementation in the longitudinal mode of a 'head-down' cockpit display for a vertical take-off and landing aircraft. These flight director laws were intended to enhance the instrument hover and landing capabilities of the Bell UH-1H helicopter equipped with a multi-function stroke-written cathode ray tube display.
A Model Based Technique for Flight Director Design: Helicopter Hovering Flight
1975
50 pages
Report
Keine Angabe
Englisch
Aeronautics , Helicopters , Hovering , Aircraft landings , Flight control systems , Display systems , Cockpits , Computer applications , Man machine systems , Mathematical models , Optimization , Cathode ray tube screens , Turbulence , Pilots , Aircraft , Theses , Flight director systems , UH-1H aircraft , H-1 aircraft , Head down displays
Helicopter stability in hovering flight
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Engineering Index Backfile | 1948
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NTIS | 1977