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Record Nr. |
UNINA9910700358203321 |
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Autore |
Connolly Joseph W |
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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 |
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Pubbl/distr/stampa |
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Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010] |
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Descrizione fisica |
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1 online resource (19 pages) : illustrations (color) |
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Collana |
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Altri autori (Persone) |
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Soggetti |
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Supersonic flight |
Control systems design |
Supersonic transports |
Specifications |
Supersonic inlets |
Dynamic models |
Loops |
Feedback control |
Supersonic wind tunnels |
Flow distribution |
Computational fluid dynamics |
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Lingua di pubblicazione |
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Formato |
Materiale a stampa |
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Livello bibliografico |
Monografia |
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Note generali |
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Title from title screen (viewed on June 13, 2011). |
"October 2010." |
"AIAA-2010-7068." |
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Nota di bibliografia |
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Includes bibliographical references (pages 18-19). |
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