Optimal Rendezvous Guidance Using Linear Quadratic Control

Optimal Rendezvous Guidance Using Linear Quadratic Control

This paper handles with an energy optimal guidance law for rendezvous mission, based on linear quadratic control (LQC) problem. Rendezvous of two satellites are expressed by a nonlinear relative orbit dynamic model. The LQC problem minimizes integral of control input quadratic term with given final...

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Bibliographic Details
Main Authors:	Moon Gun-Hee, Lee Byung-Yoon, Tahk Min-Jea, Shim David Hyunchul
Format:	Article
Language:	English
Published:	EDP Sciences 2016-01-01
Series:	MATEC Web of Conferences
Online Access:	http://dx.doi.org/10.1051/matecconf/20165409002

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