Paper reviews flight control system requirements and various possible approaches to redundancy, each having its particular attractions and limitations; basic system concepts and typical applications of hydrologic redundant systems are described with emphasis on operate/fail-safe hydrologic system consisting of servovalve with dual tandem second stage power spool plus monitor channel driving dual tandem actuator; description of operating components; tabulation lists possible failures that proposed system can encounter indicating automatic action taken by system.
Hydrologic redundant systems
SAE-NASA -- Aerospace Vehicle Flight Control Conference -- Proc
Proceedings of the SAE-NASA Aerospace Vehicle Flight Control Conference ; 1965 Control equipment
1965
36 pages
Aufsatz (Konferenz)
Englisch
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SAE Technical Papers | 1965
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