Turbofan engine control system design using the LQG/LTR methodology
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Author
Contributions
- United States. National Aeronautics and Space Administration. - Contributor
Publication
1989 - National Technical Information Service, distributor, Washington, D.C., District of Columbia
Language
English
Word Count
0 words, Guess
Page Count
0 pages
Physical Format
Microform
Identifiers
- Open LibraryOL15408680M
Subjects
Topics
Turbofan enginesFeedback controlControl systems designTurbojet engine controlLinear quadratic Gaussian control
Series Statement
- NASA contractor report -- 182303.
- NASA contractor report -- NASA CR-182303.
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