Closed-form solutions for linear regulator design of mechanical systems including optimal weighting matrix selection /

Bibliographic Details
Main Author:	Hanks, Brantley R.
Corporate Author:	Langley Research Center
Other Authors:	Skelton, Robert E.
Format:	Government Document Book
Language:	English
Published:	Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1991]
Series:	NASA technical memorandum ; 104052.
Subjects:	Damping. Design analysis. Linear quadratic regulator. Matrices (Mathematics) Mechanical properties. Riccati equation. Spacecraft structures. Stiffness. Vibration. Weighting functions.
Online Access:	https://purl.fdlp.gov/GPO/LPS65741

Description
Item Description:	"March 1991." Microform.
Physical Description:	1 volume Also available via Internet from the NTRS web site. Address as of 12/16/05: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19910012259%5F1991012259.pdf; current access is available via PURL.
Bibliography:	Includes bibliographical references.