Development of Fluidic Flight Control and Actuation Systems for High Performance Aircraft 871875
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.
Citation: Hair, K., "Development of Fluidic Flight Control and Actuation Systems for High Performance Aircraft," SAE Technical Paper 871875, 1987, https://doi.org/10.4271/871875. Download Citation
Author(s):
Kenneth A. Hair
Pages: 12
Event:
Aerospace Technology Conference and Exposition
ISSN:
0148-7191
e-ISSN:
2688-3627
Related Topics:
Energy consumption
Aircraft
Reliability
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