Augmentation theory is discussed; prototype hover-augmentation system that reduces pilot's task in maintaining position with respect to inertial reference; system modifies response characteristic of aircraft by feedback of inertially derived acceleration and velocity information to reduce number of integrations between command and aircraft position change.
Path-damping system for VTOL aircraft
Sperry Eng Rev
Sperry Engineering Review ; 20 , n 1
1967
7 pages
Article (Journal)
English
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AUTOLAND SYSTEM FOR VTOL AIRCRAFT, VTOL AIRCRAFT, AND LANDING CONTROL METHOD FOR VTOL AIRCRAFT
European Patent Office | 2024
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