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 |
DOI | 10.1049/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 |
推荐引用方式 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. |
个性服务 |
查看访问统计 |
相关权益政策 |
暂无数据 |
收藏/分享 |
除非特别说明,本系统中所有内容都受版权保护,并保留所有权利。
修改评论