An optimized integrator windup protection technique applied to a turbofan engine control
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Author
Contributions
- Garg, Sanjay. - Contributor
- United States. National Aeronautics and Space Administration. - Contributor
Publication
1995 - 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 LibraryOL15420829M
Subjects
Topics
IntegratorsEngine controlTurbofan enginesCircuit protectionSystems engineeringDigital integratorsMultivariable controlControl systems designPower factor controllersPropulsion system configurations
Series Statement
- NASA technical memorandum -- 107035.
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