Requirements established in Douglas design study for stability augmentation system of 35,000-lb ducted fan VTOL aircraft; stabilization of VTOL aircraft resulted in design of Bang-Bang constant servo rate stability augmentation system; phase plane analysis; results of electronic analog computer study; system mechanization and operation; functional block diagram and servo control schematic; advantages; extension of technique.
Application of Bang-Bang servo system to VTOL stability augmentation
SAE -- Paper
SAE Meeting ; 1962 VTOL-STOL
1962
9 pages
Conference paper
English
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