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:	Short take-off and landing aircraft > Jet propulsion. Control systems design. Controllers. Flight characteristics. Models. Propulsion. Transition flight. V/STOL aircraft.

Norlin Library - Government Information - Microform

Holdings details from Norlin Library - Government Information - Microform
Call Number:	NAS 1.15:103198
NAS 1.15:103198	Restricted Place a Hold