NASA Logo

NTRS

NTRS - NASA Technical Reports Server

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

Back to Results
Linearized flexibility models in multibody dynamics and controlSimulation of structural response of multi-flexible-body systems by linearized flexible motion combined with nonlinear rigid motion is discussed. Advantages and applicability of such an approach for accurate simulation with greatly reduced computational costs and turnaround times are described, restricting attention to the control design environment. Requirements for updating the linearized flexibility model to track large angular motions are discussed. Validation of such an approach by comparison with other existing codes is included. Application to a flexible robot manipulator system is described.
Document ID
19900000783
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Cimino, William W.
(Boeing Aerospace Co. Seattle, WA, United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1989
Publication Information
Publication: NASA. Langley Research Center, Proceedings of the Workshop on Computational Aspects in the Control of Flexible Systems, Part 1
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
90N10099
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available