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Demonstration of the dynamic flowgraph methodology using the Titan II space launch vehicle digital flight control system

Demonstration of the dynamic flowgraph methodology using the Titan II space launch vehicle digital flight control system

By M. Yau

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Publish Date

1994

Publisher

Mechanical, Aerospace, and Nuclear Engineering Dept., University of California,National Aeronautics and Space Administration,National Technical Information Service, distributor

Language

eng

Pages

-

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