Closed-form solutions for linear regulator design of mechanical systems including optimal weighting matrix selection
By: Brantley R. Hanks and Robert E. Skelton.
Contributors: Skelton, Robert E.; Langley Research Center.
Series: NASA technical memorandum -- 104052.
Publisher: National Aeronautics and Space Administration, Langley Research Center
Published: 1991
Place of publication: Hampton, Va
Language: eng
Format: Microform
Subjects: Damping.; Design analysis.; Linear quadratic regulator.; Matrices (Mathematics); Mechanical properties.; Riccati equation.; Spacecraft structures.; Stiffness.; Vibration.; Weighting functions.
Notes: "March 1991."

Includes bibliographical references.

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.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration,] 1991. 1 microfiche.