Dynamics and flight support of a vehicle Ikar control system at orbiting Globalstar satellites

被引：0
|
作者：
Somov, YI
Butyrin, SA
Anshakov, GP
Antonov, YG
Makarov, VP
Manturov, AI
Ustalov, YM
机构：
[1] Samara State Tech Univ, Res Inst Mech Syst Reliabil, Samara 443100, Russia
[2] RKA, State Res & Prod Rocket Space Ctr TsSKB Progress, Russian Space Agcy, Samara 443009, Russia
来源：
CONTROL ENGINEERING PRACTICE | 2003年 / 11卷 / 05期
关键词：
launch vehicle; nonlinear control system; fault tolerance; flight control;
D O I：
10.1016/S0967-0661(02)00279-4
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 nonlinear logic-dynamic control and its applications to fault-tolerant motion control system of the maneuvering vehicle Ikar, developed by Russian State Research & Production Rocket-Space Center TsSKB-Progress and applied for the orbital placement of the Globalstar satellites, are presented. (C) 2003 Elsevier Science Ltd. All rights reserved.
引用
收藏
页码：585 / 597
页数：13
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