DocumentCode :
982238
Title :
Closed-form Grammians and model reduction for flexible space structures
Author :
Williams, Trevor
Author_Institution :
NASA Langley Res. Center, Hampton, VA, USA
Volume :
35
Issue :
3
fYear :
1990
fDate :
3/1/1990 12:00:00 AM
Firstpage :
379
Lastpage :
382
Abstract :
The author derives analytical expressions for the Grammians of a model given in modal coordinates for the dynamics of a flexible space structure (FSS). These expressions are then used as the basis for a new algorithm to compute a dominant reduced-order model for such a system in an efficient manner. The resulting reduced-order model is obtained directly rather than by truncating a balanced model of the entire system, thus giving rise to significant efficiency gains for the typical FSS case where the reduced-order model is of very much lower order than the original system
Keywords :
aerospace control; controllability; Grammians; flexible space structures; modal coordinates; model reduction; reduced-order model; Aerodynamics; Algorithm design and analysis; Bandwidth; Costs; Design methodology; Equations; Optimal control; Optimization methods; Reduced order systems; Springs;
fLanguage :
English
Journal_Title :
Automatic Control, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9286
Type :
jour
DOI :
10.1109/9.50365
Filename :
50365
Link To Document :
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