Attitude and vibration control of the space station

被引：24

作者：

Grewal, A

Modi, VJ

机构：

[1] Department of Mechanical Engineering, University of British Columbia, Vancouver

来源：

ACTA ASTRONAUTICA | 1996年 / 38卷 / 03期

关键词：

D O I：

10.1016/0094-5765(96)00073-2

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

Simultaneous attitude and vibration control of a space platform is studied using the LQG/LTR approach with the linearized equations obtained through a novel finite difference procedure. Results show the control strategy to be quite effective in damping a wide variety of disturbances including the Shuttle docking, manipulator maneuvers, solar array tracking and initial displacements imparted to the system as well as its subassemblies. Copyright (C) 1996 Elsevier Science Ltd

引用

页码：139 / 160

页数：22

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