H-infinity based integrated flight/propulsion control design for a STOVL aircraft in transition flight [microform] / Sanjay Garg [and others] ; prepared for the Guidance, Navigation and Control Conference sponsored by the American Institute of Aeronautics and Astronautics, Portland, Oregon, August 20-22, 1990.

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Bibliographic Details
Corporate Author: United States. National Aeronautics and Space Administration
Other Authors: Garg, Sanjay
Other title:H infinity based integrated flight propulsion control design for a STOVL aircraft in transition flight.
Format: Government Document Microfilm Book
Language:English
Published: [Washington, D.C.] : [Springfield, Va.] : NASA ; [For sale by the National Technical Information Service], [1990]
Series:NASA technical memorandum ; 103198.
Subjects:

MARC

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490 1 |a NASA technical memorandum ;  |v 103198. 
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504 |a Includes bibliographical references (pages 21-22) 
533 |a Microfiche.  |b [Washington, D.C.? :  |b National Aeronautics and Space Administration,  |d 1990]  |e 1 microfiche : negative. 
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650 0 |a Short take-off and landing aircraft  |x Jet propulsion.  |0 http://id.loc.gov/authorities/subjects/sh85121969. 
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650 7 |a Controllers.  |2 nasat. 
650 7 |a Flight characteristics.  |2 nasat. 
650 7 |a Models.  |2 nasat. 
650 7 |a Propulsion.  |2 nasat. 
650 7 |a Transition flight.  |2 nasat. 
650 7 |a V/STOL aircraft.  |2 nasat. 
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