NDLI: Attitude maneuver control of two-flywheel spacecraft using potential function method

Content Provider	IEEE Xplore Digital Library
Author	Guo Yanning Song Bin Ma Guangfu
Copyright Year	2013
Description	Author affiliation: Aerosp. Syst. Eng. Shanghai, Shanghai, China (Song Bin) \|\| Harbin Inst. of Technol., Harbin, China (Guo Yanning; Ma Guangfu)
Abstract	This paper investigates the attitude maneuver control problem of spacecraft actuated by two arbitrarily installed flywheels. Most of the previous studies assume that the under-actuated axis coincides with one of the inertial principal axes, while more general case is considered in this paper. When only two flywheels remain active in a redundant flywheel array, an under-actuated attitude controller is proposed based on potential function method, where the desired attitude is used to construct the attractive potential function, and the repulsive potential function is devised by considering the rotation around the under-actuated axis as an obstacle. Moreover, an arc tangent function is adopted to restrict the magnitude of control torque. Accordingly, a control parameter adaptive algorithm is then developed to ensure the stability of the system. Numerical simulations are provided at last to illustrate the effectiveness of the proposed algorithms.
Starting Page	5132
Ending Page	5137
File Size	283531
Page Count	6
File Format	PDF
ISBN	9789881563835
ISSN	19341768
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	2013-07-26
Publisher Place	China
Access Restriction	Subscribed
Rights Holder	TCCT, CAA
Subject Keyword	Space vehicles Attitude control Flywheel Spacecraft Systems engineering and theory Potential function Electronic mail Flywheels Attitude Control Under-actuated Aerospace engineering
Content Type	Text
Resource Type	Article

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