GNC DESIGN AND VALIDATION FOR PRECISION LANDING AT THE MOON AND MARS

被引：0
|
作者：
Hamel, Jean-Francois [1 ]
Beaudette, David [1 ]
Simard-Bilodeau, Vincent [1 ]
de Lafontaine, Jean [1 ]
Di Sotto, Emanuele
Paulino, Nuno
Branco, Joao
Johns, Guy
de Rosa, Diego
机构：
[1] NGC Aerosp Ltd, Sherbrooke, PQ, Canada
来源：
GUIDANCE AND CONTROL 2012 | 2012年 / 144卷
关键词：
D O I：
暂无
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
Precision landing is a critical and challenging requirement for future planetary exploration landing missions. In order to meet these requirements, a GNC architecture is proposed for autonomous planetary landing applications. The GNC design proves to meet a 200 m landing accuracy at the Moon and a 10 km landing accuracy at Mars, relying on vision-based navigation technologies (for Moon), guided entry (for Mars) and innovative navigation concepts. Performance of the GNC is validated through Monte-Carlo simulations campaigns, in closed-loop in a high-fidelity simulation environment.
引用
收藏
页码：869 / 884
页数：16
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