NASA Logo

NTRS

NTRS - NASA Technical Reports Server

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

Back to Results
Analysis of limit cycles in control systems for joint dominated structuresAn approach to the modeling of limit cycles due to joint nonlinearities in large joint dominated space structures is presented which makes it possible to predict limit cycles and determine their stability. An actively controlled truss structure with nonlinear joints is modeled as a linear system with nonlinear feedback by separating the joint load-displacement characteristics into a linear part, which prevails at large displacements, and a nonlinear part. By replacing the joints by their linear parts, it is possible to perform a standard model decomposition which yields a reduced order linear model. Linear control laws can be easily included into the linear part of the system; nonlinear control laws can be implemented but they must be fed back to the linear model. The modeling approach described here allows straightforward limit cycle analysis.
Document ID
19890024319
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mercadal, M.
(Massachusetts Inst. of Tech. Cambridge, MA, United States)
Vander Velde, W. E.
(MIT Cambridge, MA, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1988
Subject Category
Cybernetics
Meeting Information
Meeting: VPI&SU/AIAA Symposium
Location: Blacksburg, VA
Country: United States
Start Date: June 29, 1987
End Date: July 1, 1987
Accession Number
89A11690
Funding Number(s)
CONTRACT_GRANT: NAG1-126
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available