H-infinity based integrated flight/propulsion control design for a STOVL aircraft in transition flight
By: Sanjay Garg ... [et al.] ; prepared for the Guidance, Navigation and Control Conference sponsored by the American Institute of Aeronautics and Astronautics, Portland, Oregon, August 20-22, 1990.
Contributors: Garg, Sanjay.; United States. National Aeronautics and Space Administration.
Series: NASA technical memorandum -- 103198.
Publisher: NASA; For sale by the National Technical Information Service
Published: 1990
Place of publication: [Washington, D.C.]; [Springfield, Va
Language: eng
Format: Microform
Number of pages: 30
Subjects: Short take-off and landing aircraft -- Jet propulsion.; Control systems design.; Controllers.; Flight characteristics.; Models.; Propulsion.; Transition flight.; V/STOL aircraft.
Other titles: H infinity based integrated flight propulsion control design for a STOVL aircraft in transition flight.
Notes: Cover title.

Distributed to depository libraries in microfiche.

Includes bibliographical references (p. 21-22).

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration, 1990] 1 microfiche : negative.

505-62-01.