Fuel Minimizing Control for Constrained Relative Satellite Orbits

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Fuel Minimizing Control for Constrained Relative Satellite Orbits

In this paper, we study the fuel minimization problem of hovering satellite subject to a practical constraint on the trajectory of the deputy satellite. It is first shown that the constraint condition can be expressed equivalently as maximum flight time inequalities. On this basis, a cost function r...

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Bibliographic Details
Main Authors:	Gao, X., Teo, Kok Lay, Sun, Y., Duan, G.
Format:	Journal Article
Published:	WATAM Press 2011
Online Access:	http://hdl.handle.net/20.500.11937/48019

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