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Loop Shaping control design for a supersonic propulsion system model using quantitative feedback theory (QFT) specifications and bounds [[electronic resource] /] / Joseph W. Connolly and George Kopasakis ; prepared for the 46th Joint Propulsion Conference and Exhibit cosponsored by AIAA, ASME, SAE, and ASEE, Nashville, Tennessee, July 25-28, 2010



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Autore: Connolly Joseph W Visualizza persona
Titolo: Loop Shaping control design for a supersonic propulsion system model using quantitative feedback theory (QFT) specifications and bounds [[electronic resource] /] / Joseph W. Connolly and George Kopasakis ; prepared for the 46th Joint Propulsion Conference and Exhibit cosponsored by AIAA, ASME, SAE, and ASEE, Nashville, Tennessee, July 25-28, 2010 Visualizza cluster
Pubblicazione: Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010]
Descrizione fisica: 1 online resource (19 pages) : illustrations (color)
Soggetto topico: Supersonic flight
Control systems design
Supersonic transports
Specifications
Supersonic inlets
Dynamic models
Loops
Feedback control
Supersonic wind tunnels
Flow distribution
Computational fluid dynamics
Altri autori: KopasakisGeorge  
Note generali: Title from title screen (viewed on June 13, 2011).
"October 2010."
"AIAA-2010-7068."
Nota di bibliografia: Includes bibliographical references (pages 18-19).
Altri titoli varianti: Loop Shaping control design for a supersonic propulsion system model using quantitative feedback theory
Titolo autorizzato: Loop Shaping control design for a supersonic propulsion system model using quantitative feedback theory (QFT) specifications and bounds  Visualizza cluster
Formato: Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione: Inglese
Record Nr.: 9910700358203321
Lo trovi qui: Univ. Federico II
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