An optimal control approach to spacecraft rendezvous on elliptical orbit

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

Internet

http://hdl.handle.net/20.500.11937/39357

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