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

Description
Item Description:	Title from title screen (viewed on June 13, 2011). "October 2010." "AIAA-2010-7068." Electronic resource.
Physical Description:	1 online resource (19 pages) : illustrations (color).
Bibliography:	Includes bibliographical references (pages 18-19).