A dissimilar FCS based on fluidic technology, integrated with a redundant electronic FCS, promises to increase the mission reliability and survivability of high performance aircraft by providing protection from common mode and potential EMI/EMP induced failures. Current emphasis is on developing critical hydrofluidic servoactuation systems and components which will meet demanding requirements for performance, size, weight, reliability and power consumption.
Development of fluidic flight control and actuation systems for high performance aircraft
Entwicklung fluidischer Flugregelungs- und Stellsysteme fuer Hochleistungsflugzeuge
SAE-Papers ; Oct ; 1-9
1987
9 Seiten, 9 Bilder, 8 Quellen
Conference paper
English
Development of Fluidic Flight Control and Actuation Systems for High Performance Aircraft
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