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- W804495382 abstract "Flight control system (FCS) reliability is discussed in terms of sensors, computers and actuators. The servo/actuation bottleneck is discussed. FCS survivability is considered. Preliminary survivability issues. A Grumman study vehicle, R-14, and YF-16 aircraft configurations are studied. Goals of control are reviewed." @default.
- W804495382 created "2016-06-24" @default.
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- W804495382 date "1983-08-01" @default.
- W804495382 modified "2023-09-26" @default.
- W804495382 title "Robust Reconfiguration for High Reliability and Survivability for Advanced Aircraft" @default.
- W804495382 hasPublicationYear "1983" @default.
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