NDLI: On characteristic modeling of a class of flight vehicles’ attitude dynamics

Content Provider	Springer Nature Link
Author	Meng, Bin Wu, HongXin
Copyright Year	2010
Abstract	The characteristic modeling problem of flight vehicles’ attitude dynamics is considered in this paper. In terms of the affine nonlinear system with triangle form of flight vehicles’ attitude dynamics, a general method is presented to compress the dynamics into the characteristic model parameters, by introducing the time scale of nonlinear systems and a class of system states related compress functions. The parameter region and limit of the characteristic model are also given. From the given parameter region it is seen that the bound of the characteristic model parameters is dependent on the sampling period, the modeling error, the system order and the system change rate. The modeling error of the established characteristic model can be arbitrarily small according to the control precision, showing the difference between the characteristic model and other model reduction methods, that is, no system information is lost using this approach. On the basis of this modeling approach, the characteristic model of the flexible satellite attitude is established, as well as the bound and limit of the parameters, which sets a theoretical foundation for characteristic model based control design of flight vehicles.
Starting Page	2074
Ending Page	2080
Page Count	7
File Format	PDF
ISSN	16747321
Journal	Science in China Series E: Technological Sciences
Volume Number	53
Issue Number	8
e-ISSN	1862281X
Language	English
Publisher	SP Science China Press
Publisher Date	2010-07-15
Publisher Place	Heidelberg
Access Restriction	One Nation One Subscription (ONOS)
Subject Keyword	characteristic modeling modeling error time scale of nonlinear systems spacecraft attitude dynamics Engineering
Content Type	Text
Resource Type	Article
Subject	Engineering Materials Science

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