An optimal control approach to robust control of nonlinear spacecraft rendezvous system with θ-D technique

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An optimal control approach to robust control of nonlinear spacecraft rendezvous system with θ-D technique

In this paper, a new optimal robust control design approach is proposed for the task of spacecraft rendezvous such that both the stabilization and optimal performance are achieved. An approximate closed-form solution to the nonlinear optimal control problem is obtained by employing the θ-D technique...

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Bibliographic Details
Main Authors:	Gao, X., Teo, Kok Lay, Duan, G.
Format:	Journal Article
Published:	ICIC International 2013
Subjects:	robust control uncertainties spacecraft rendezvous optimal control
Online Access:	http://hdl.handle.net/20.500.11937/12266

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