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Enhanced predictor-corrector Mars entry guidance approach with atmospheric uncertainties
Xu Jianwei; Qiao Jianzhong; Guo Lei; Chen Wenhua
刊名IET CONTROL THEORY AND APPLICATIONS
2019
卷号13页码:1612-1618
关键词Mars aerospace control entry descent and landing (spacecraft) space vehicles predictor-corrector methods enhanced predictor-corrector Mars entry guidance approach atmospheric uncertainties long-range data communication complex Mars environment high precision landing future Mars missions enhanced predictor-corrector guidance method Mars landing predictor-corrector guidance algorithm composite guidance method Mars lander guidance system Mars lander entry guidance system
ISSN号1751-8644
DOI10.1049/iet-cta.2018.5782
URL标识查看原文
收录类别SCIE ; EI
WOS记录号WOS:000473532200004
内容类型期刊论文
URI标识http://www.corc.org.cn/handle/1471x/5918399
专题北京航空航天大学
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GB/T 7714
Xu Jianwei,Qiao Jianzhong,Guo Lei,et al. Enhanced predictor-corrector Mars entry guidance approach with atmospheric uncertainties[J]. IET CONTROL THEORY AND APPLICATIONS,2019,13:1612-1618.
APA Xu Jianwei,Qiao Jianzhong,Guo Lei,&Chen Wenhua.(2019).Enhanced predictor-corrector Mars entry guidance approach with atmospheric uncertainties.IET CONTROL THEORY AND APPLICATIONS,13,1612-1618.
MLA Xu Jianwei,et al."Enhanced predictor-corrector Mars entry guidance approach with atmospheric uncertainties".IET CONTROL THEORY AND APPLICATIONS 13(2019):1612-1618.
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