Development of flight simulation and supporting elements; control system dynamics element heart of which is closed-loop electro-hydraulic servo system, is described; system takes force signal from force transducer on stick to computer model which computes commanded stick position and sends it to high-response hydraulic servo which positions stick; test results show that friction is most significant control system property in small stick deflection range of flying.
Flight control studies in small stick deflection area
AIAA -- Simulation Aerospace Flight Conference -- Tech Papers
AIAA Meeting -- Simulation for Aerospace Flight Conference ; 1963 Simulators
1963
6 pages
Conference paper
English
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