Lyapunov optimal control laws for flexible structure maneuver and vibration control

被引：0

作者：

Bang, H. ^{[1
]}

Junkins, John L. ^{[1
]}

Fleming, Peter J. ^{[1
]}

机构：

[1] Naval Postgraduate Sch, Monterey, United States

来源：

| 1600年 / 41期

关键词：

Flexible structures;

D O I：

暂无

中图分类号：

学科分类号：

摘要：

引用

共 50 条

[1] LYAPUNOV OPTIMAL-CONTROL LAWS FOR FLEXIBLE STRUCTURE MANEUVER AND VIBRATION CONTROL
BANG, H
JUNKINS, JL
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JOURNAL OF THE ASTRONAUTICAL SCIENCES, 1993, 41 (01): : 91 - 118
[2] Variable structure attitude maneuver and vibration control of flexible spacecraft
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J. Harbin Inst. Technol., 2008, 5 (705-710):
[3] OPTIMAL CONTROL OF MANEUVER-INDUCED VIBRATION IN FLEXIBLE AEROSPACE VEHICLES
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[4] Maneuver control and active vibration suppression of a two-link flexible arm using a hybrid variable structure/Lyapunov control design
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[5] OPTIMAL VIBRATION CONTROL OF FLEXIBLE SPACECRAFT DURING A MINIMUM-TIME MANEUVER
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[7] Active vibration control of a flexible structure using optimal control and piezoelectric actuators
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[8] Slew maneuver control of flexible spacecraft for vibration suppression
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[9] Neural optimal control of flexible spacecraft slew maneuver
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[10] Variable structure control and active vibration suppression of flexible spacecraft during attitude maneuver
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