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dc.contributor.authorZhou, J.
dc.contributor.authorTeo, Kok Lay
dc.contributor.authorZhou, D.
dc.contributor.authorZhao, G.
dc.contributor.editorX.M. Yang, Y. Gao
dc.date.accessioned2017-01-30T11:56:10Z
dc.date.available2017-01-30T11:56:10Z
dc.date.created2010-03-15T20:02:30Z
dc.date.issued2009
dc.identifier.citationZhou, Jingyang and Teo, Kok Lay and Zhou, Di and Zhao, G. 2009. Optimal guidance for lunar module soft landing, in X.M. Yang, Y. Gao (ed), 4th Int. Conf. Optimization and Control with Applications, Nov 6 2009. Harbin, China: Harbin Institute of Technology Press.
dc.identifier.urihttp://hdl.handle.net/20.500.11937/16513
dc.publisherHarbin Inatitute of Technology Press
dc.titleOptimal guidance for lunar module soft landing
dc.typeConference Paper
dcterms.source.titleProc. 4th Int. Conf. Optimizaiton and Control with Applications
dcterms.source.seriesProc. 4th Int. Conf. Optimizaiton and Control with Applications
dcterms.source.conference4th Int. Conf. Optimizaiton and Control with Applications
dcterms.source.conference-start-dateNov 6 2009
dcterms.source.conferencelocationHarbin, China
dcterms.source.placeHarbin, China
curtin.accessStatusFulltext not available
curtin.facultySchool of Science and Computing
curtin.facultyDepartment of Mathematics and Statistics
curtin.facultyFaculty of Science and Engineering


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