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A preliminary look at control augmented dynamic response of structuresThis report deals with the augmentation of structural characteristics, mass, damping, and stiffness through the use of control theory in lieu of structural redesign or augmentation. Treated first is the standard single-degree-of-freedom system followed by a treatment of the same system using control augmentation. The system is extended to elastic structure using single and multisensor approaches and concludes with a brief discussion of potential application to large orbiting space structures.
Document ID
19830048607
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Jewell, R. E.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Ryan, R. S.
(NASA Marshall Space Flight Center Structural Dynamics Div., Huntsville, AL, United States)
Date Acquired
August 11, 2013
Publication Date
January 1, 1983
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 83-0850
Report Number: AIAA PAPER 83-0850
Meeting Information
Meeting: Structures, Structural Dynamics and Materials Conference
Location: Lake Tahoe, NV
Start Date: May 2, 1983
End Date: May 4, 1983
Accession Number
83A29825
Distribution Limits
Public
Copyright
Other

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