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Dual redundant sensor FDI techniques applied to the NASA F8C DFBW aircraft
Home
Publications
Dual redundant sensor FDI techniques applied to the NASA F8C DFBW aircraft
Dual redundant sensor FDI techniques applied to the NASA F8C DFBW aircraft
MD
M. Desai
M. Desai
JD
J. Deckert
J. Deckert
JD
J. Deyst
J. Deyst
AW
A. Willsky
A. Willsky
EC
E. Chow
E. Chow
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16 August 1976
conference paper
Published by
American Institute of Aeronautics and Astronautics (AIAA)
https://doi.org/10.2514/6.1976-1976
Abstract
No abstract available
Cited by 6 articles