Guidance, navigation, control of SELENE lunar landing mission

被引：0

作者：

Kawakatsu, Y ^{[1
]}

Kinoshita, T ^{[1
]}

Takizawa, Y ^{[1
]}

机构：

[1] Natl Space Dev Agcy Japan, NASDA, Tsukuba, Ibaraki 305, Japan

来源：

SECOND INTERNATIONAL CONFERENCE ON NONLINEAR PROBLEMS IN AVIATION & AEROSPACE VOL 1 AND 2 | 1999年

关键词：

D O I：

暂无

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

One of the major objectives of SELENE mission is to develop and acquire the soft-landing technology. After one year operation on orbit, Propulsion Module of the orbiter separates from Mission Module and demonstrates soft-landing on the lunar surface. This paper focuses on the guidance, navigation, and control aspects of the landing sequence. The guidance and navigation methods through separation to landing are explained. After that, the results of the navigation and guidance error analysis are shown.

引用

页码：349 / 356

页数：4