NDLI: Decentralized attitude cooperative regulation of spacecraft formation without angular velocity feedback

Content Provider	IEEE Xplore Digital Library
Author	Lv Yueyong Hu Qinglei Ma Guangfu
Copyright Year	2011
Description	Author affiliation: Harbin Institute of Technology, 150001, China (Lv Yueyong; Hu Qinglei; Ma Guangfu)
Abstract	This paper treats the decentralized cooperative attitude regulation problem without angular-velocity feedback for spacecraft formation flying. The nonlinear attitude dynamic and kinematic equations are considered for the case that the relative quaternion and angular velocity are employed such that the dynamics of formation agents are strongly coupled. More specifically, the controller structure includes a lead filter which is derived without explicit differentiation of attitude to synthesize angular velocity-like signals. And the stability of such a formation is also investigated by the development of a novel Lyapunov function candidate containing cross/mixed terms. Considering the affect of external disturbance, a modified controller is developed to confer the closed-loop system the capability of L2-gain disturbance attenuation. A sufficient condition is provided under which this controller could render the system uniformly ultimately bounded stable. As such, the closed-loop system is robust with respect to any disturbance within a quantifiable restriction on the amplitude. Numerical examples are presented to demonstrate the efficacy of the proposed controllers to maintain the relative attitude cooperation by correcting for initial offsets and external perturbation effects that tend to disperse the formation.
Starting Page	239
Ending Page	244
File Size	153813
Page Count	6
File Format	PDF
ISBN	9781457706776
ISSN	21612927
e-ISBN	9789881725592
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	2011-07-22
Publisher Place	China
Access Restriction	Subscribed
Rights Holder	Chinese Assoc of Automati
Subject Keyword	Space vehicles L2-gain Torque Attitude control Quaternions Cooperative attitude control Spacecraft formation flying Computer architecture Attenuation Angular velocity Attitude regulation Decentralized output feedback
Content Type	Text
Resource Type	Article

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