Control design for the Rosetta comet lander.

被引：0
|
作者：
Ankersen, F [1 ]
机构：
[1] European Space Agcy, European Space Res & Technol Ctr, NL-2200 AG Noordwijk, Netherlands
来源：
AUTOMATIC CONTROL IN AEROSPACE 1998 | 1999年
关键词：
attitude control; PID; H-infinity; spacecraft autonomy; state observers; optimal trajectories;
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：
The problems of controlling a lander to land on a comet, for the Rosetta mission to comet Wirtanen, is the subject of this paper. The ejection problems of the lander from the Rosetta spacecraft, are described, and a design of an active control system onboard the lander will be performed and tested. Performance results of both lander attitude and landing accuracy are presented. (C) 1998 IFAC.
引用
收藏
页码：173 / 178
页数：6
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