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- W3031388748 abstract "The problem of using redundancy that exists between dissimilar systems in aircraft flight control is addressed. That is, using the redundancy that exists between a rate gyro and an accelerometer--devices that have dissimilar outputs which are related only through the dynamics of the aircraft motion. Management of this type of redundancy requires advanced logic so that the system can monitor failure status and can reconfigure itself in the event of one or more failures. An optimal decision theory was tutorially developed for the management of sensor redundancy and the theory is applied to two aircraft examples. The first example is the space shuttle and the second is a highly maneuvering high performance aircraft--the F8-C. The examples illustrate the redundancy management design process and the performance of the algorithms presented in failure detection and control law reconfiguration." @default.
- W3031388748 created "2020-06-05" @default.
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- W3031388748 date "2017-09-29" @default.
- W3031388748 modified "2023-09-27" @default.
- W3031388748 title "Management of redundancy in flight control systems using optimal decision theory" @default.
- W3031388748 hasPublicationYear "2017" @default.
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