An optimal control approach to spacecraft rendezvous on elliptical orbit

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An optimal control approach to spacecraft rendezvous on elliptical orbit

In this paper, we consider a linear quadratic regulator control problem for spacecraft rendezvous in an elliptical orbit. A new spacecraft rendezvous model is established. On the basis of this model, a linear quadratic regulator control problem is formulated. A parametric Lyapunov differential equat...

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Bibliographic Details
Main Authors:	Gao, Xiangyu, Teo, Kok Lay, Duan, Guang-Ren
Format:	Journal Article
Published:	John Wiley and Sons, Ltd. 2014
Subjects:	LQR PLDE spacecraft rendezvous numerical algorithm
Online Access:	http://hdl.handle.net/20.500.11937/39357

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