Approach taken by Lycoming-Stratford Div, Avco Corp, in development of mechanical servo actuator for all-mechanical flight control system for advanced supersonic aircraft and space vehicles; description of actuator and its basic design criteria; component and system test results, including parametric and theoretical analyses, substantiate feasibility of approach; techniques for tailoring performance to specific requirement and approach to mechanical cascading for control power amplification are considered. SAE-Paper 650580.
Analysis of toroidal actuation systems for aerospace vehicles
SAE-NASA -- Proc
Proceedings of the Aerospace Vehicle Flight Control Conference ; 1965 Control
1965
12 pages
Aufsatz (Konferenz)
Englisch
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