Fuel Minimizing Control for Constrained Relative Satellite Orbits

dc.contributor.author	Gao, X.
dc.contributor.author	Teo, Kok Lay
dc.contributor.author	Sun, Y.
dc.contributor.author	Duan, G.
dc.date.accessioned	2017-01-30T15:36:58Z
dc.date.available	2017-01-30T15:36:58Z
dc.date.created	2012-03-26T20:01:28Z
dc.date.issued	2011
dc.identifier.citation	Gao, Xiang-Yu and Teo, K.L. and Sun, Yong and Duan, Guang-Ren. 2011. Fuel Minimizing Control for Constrained Relative Satellite Orbits. Dynamics of Continuous, Discrete and Impulsive Systems B: Applications & Algorithms. 18: pp. 461-472.
dc.identifier.uri	http://hdl.handle.net/20.500.11937/48019
dc.description.abstract	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 relating to the fuel burn is formulated. A numerical procedure is developed and an illustrative example is solved.
dc.publisher	WATAM Press
dc.title	Fuel Minimizing Control for Constrained Relative Satellite Orbits
dc.type	Journal Article
dcterms.source.volume	18
dcterms.source.startPage	461
dcterms.source.endPage	472
dcterms.source.issn	1492-8760
dcterms.source.title	Dynamics of Continuous, Discrete and Impulsive Systems B
curtin.department	Department of Mathematics and Statistics
curtin.accessStatus	Fulltext not available