H-infinity Based Integrated Flight/propulsion Control Design for A STOVL Aircraft in Transition Flight

H-infinity Based Integrated Flight/propulsion Control Design for A STOVL Aircraft in Transition Flight

Microform - 1990
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Publisher: [Washington, D.C.] : NASA ; [Springfield, Va. : For sale by the National Technical Information Service, 1990]
Characteristics: 30 p. (microfiche) : ill
Additional Contributors: Garg, Sanjay
United States

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this is available, but you have to get it at the library


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