DocumentCode
286656
Title
Model reduction methods for the analysis of control-structure interaction in flexible space structures
Author
Spanjaard, J.
Author_Institution
Stirling Dynamics Ltd., Bristol, UK
fYear
1993
fDate
34134
Firstpage
42675
Lastpage
42681
Abstract
Highlights some of the problems a design engineer encounters when reducing the order of a flexible space structure model. The choice of the appropriate method in a particular situation is dependant on characteristics of the model, the error criterion of importance and the end use of the model. Other methods of measuring errors in reduced order models are also studied. A realistic space vehicle mathematical model is currently being obtained and will be investigated using multiple inputs and outputs
Keywords
aerospace control; error analysis; finite element analysis; aerospace control; control-structure interaction; error criterion; finite element methods; flexible space structures; reduced order models;
fLanguage
English
Publisher
iet
Conference_Titel
High Accuracy Platform Control in Space, IEE Colloquium on
Conference_Location
London
Type
conf
Filename
255862
Link To Document