Nonlinear dynamics of gyromoment attitude control and precise antenna pointing by the SESAT spacecraft

被引：0
|
作者：
Titov, GP [1 ]
Somov, YI [1 ]
Rayevsky, VA [1 ]
Ovtchinnikov, AV [1 ]
Baiget, A [1 ]
Rogers, RC [1 ]
机构：
[1] RKA, RPA Appl Mech NPO PM, Krasnoyarsk 660026 26, Russia
来源：
AUTOMATIC CONTROL IN AEROSPACE 2001 | 2002年
关键词：
attitude determination; gyromoment control; dynamics; fault tolerance;
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：
New research and developments on attitude determination, nonlinear dynamics of precise gyromoment control and antenna pointing by the GEO communication spacecraft Sesat developed by Russian State Space Research & Production Association Applied Mechanics (NPO PM) in cooperation with Alcatel Space Industries (ASI, France) on the order of Eutelsat, are presented. Copyright(C) 2001 IFAC.
引用
收藏
页码：95 / 100
页数：6
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