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
Sae Technical Papers
Aerospace Technology Conference and Exposition ; 1987
1987-10-01
Aufsatz (Konferenz)
Englisch
Aircraft flight control actuation system design
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