General Electric Co designed, fabricated and evaluated bread-board model of failure-correcting, rate-maneuvering flight control proving feasibility of triple-redundant majority logic voting using HYDAPT (hybrid digital-analog pulse time) concept; following techniques developed or used in General Electric programs or contracts are described -- triple redundancy with majority logic voting, hammock networks, dual actuators with model and automatic fault removal and failure-correcting redundant power supplies.
Development of failure-correcting flight control system
SAE-NASA -- Aerospace Vehicle Flight Control Conference -- Proc
Proceedings of the SAE-NASA Aerospace Vehicle Flight Control Conference ; 1965 Control equipment
1965
Aufsatz (Konferenz)
Englisch
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Development of Failure-Correcting Flight Control System
SAE Technical Papers | 1965
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