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Loop Shaping control design for a supersonic propulsion system model using quantitative feedback theory (QFT) specifications and bounds /

Bibliographic Details
Main Author: Connolly, Joseph W.
Corporate Authors: NASA Glenn Research Center, AIAA/ASME/SAE/ASEE Joint Propulsion Conference
Other Authors: Kopasakis, George
Format: Government Document Conference Proceeding eBook
Language:English
Published: Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2010]
Series:NASA technical memorandum ; 216897.
Subjects:
Supersonic flight.
Control systems design.
Supersonic transports.
Specifications.
Supersonic inlets.
Dynamic models.
Loops.
Feedback control.
Supersonic wind tunnels.
Flow distribution.
Computational fluid dynamics.
Online Access:https://purl.fdlp.gov/GPO/gpo8439

Internet

https://purl.fdlp.gov/GPO/gpo8439

Available Online

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Call Number: NAS 1.15:2010-216897
 
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NAS 1.15:2010-216897 Available