Concept for development of truly universal automatic flight control system for VTOL aircraft is described; system is built around core system which replaces (typically) mechanical flight control system with "fly-by-wire" controls; principles of inner and outer loop; some of leading problems associated with actual development of such system are indicated; it is believed that achievement of standardized control systems hinges on prior development and acceptance of fly-by-wire control systems.
Concept for development of universal automatic flight control system for VTOL aircraft
Am Helicopter Soc -- J
American Helicopter Society -- Journal ; 10 , n 1
1965
16 pages
Article (Journal)
English
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Automatic flight control for VTOL aircraft
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