NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Multirate sampled-data yaw-damper and modal suppression system designA multirate control law synthesized algorithm based on an infinite-time quadratic cost function, was developed along with a method for analyzing the robustness of multirate systems. A generalized multirate sampled-data control law structure (GMCLS) was introduced. A new infinite-time-based parameter optimization multirate sampled-data control law synthesis method and solution algorithm were developed. A singular-value-based method for determining gain and phase margins for multirate systems was also developed. The finite-time-based parameter optimization multirate sampled-data control law synthesis algorithm originally intended to be applied to the aircraft problem was instead demonstrated by application to a simpler problem involving the control of the tip position of a two-link robot arm. The GMCLS, the infinite-time-based parameter optimization multirate control law synthesis method and solution algorithm, and the singular-value based method for determining gain and phase margins were all demonstrated by application to the aircraft control problem originally proposed for this project.
Document ID
19910010817
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Berg, Martin C.
(Washington Univ. Seattle, WA, United States)
Mason, Gregory S.
(Washington Univ. Seattle, WA, United States)
Date Acquired
September 6, 2013
Publication Date
December 1, 1990
Subject Category
Aircraft Stability And Control
Report/Patent Number
NAS 1.26:188017
NASA-CR-188017
Report Number: NAS 1.26:188017
Report Number: NASA-CR-188017
Accession Number
91N20130
Funding Number(s)
CONTRACT_GRANT: NAG1-1055
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available