MODEL OF CENTRIFUGAL EFFECT AND ATTITUDE MANEUVER STABILITY OF A COUPLED RIGID-FLEXIBLE SYSTEM

The influences of nonlinear centrifugal force to large overall attitude motion of coupled rigid-flexible system was investigated. First the nonlinear model of the coupled rigidflexible system was deduced from the idea of “centrifugal potential field”, and then the dynamic effects of the nonlinear ce...

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Published inApplied mathematics and mechanics Vol. 26; no. 5; pp. 594 - 603
Main Author 李智斌 王照林 王天舒 柳宁
Format Journal Article
LanguageEnglish
Published Beijing Institute of Control Engineering, P.O.Box 2729, Beijing 100080, P.R.China 01.05.2005
School of Aerospace, Tsinghua University, Beijing 100084, P.R. China%School of Aerospace, Tsinghua University, Beijing 100084, P.R. China
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ISSN0253-4827
1573-2754
DOI10.1007/bf02466333

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Abstract The influences of nonlinear centrifugal force to large overall attitude motion of coupled rigid-flexible system was investigated. First the nonlinear model of the coupled rigidflexible system was deduced from the idea of “centrifugal potential field”, and then the dynamic effects of the nonlinear centrifugal force to system attitude motion were analyzed by approximate calculation; At last, the Lyapunov function based on energy norm was selected,in the condition that only the measured values of attitude and attitude speed are available,and it is proved that the PD feedback control law can ensure the attitude stability during large angle maneuver.
AbstractList The influences of nonlinear centrifugal force to large overall attitude motion of coupled rigid-flexible system was investigated. First the nonlinear model of the coupled rigidflexible system was deduced from the idea of “centrifugal potential field”, and then the dynamic effects of the nonlinear centrifugal force to system attitude motion were analyzed by approximate calculation; At last, the Lyapunov function based on energy norm was selected,in the condition that only the measured values of attitude and attitude speed are available,and it is proved that the PD feedback control law can ensure the attitude stability during large angle maneuver.
O231%O317; The influences of nonlinear centrifugal force to large overall attitude motion of coupled rigid-flexible system was investigated. First the nonlinear model of the coupled rigidflexible system was deduced from the idea of "cenlrifugal potential field", and then the dynamic effects of the nonlinear centrifugal force to system attitude motion were analyzed by approximate calculation; At last, the Lyapunov function based on energy norm was selected,in the condition that only the measured values of attitude and attitude speed are available,and it is proved that the PD feedback control law can ensure the attitude stability during large angle maneuver.
Author 李智斌 王照林 王天舒 柳宁
AuthorAffiliation BeijingInstituteofControlEngineering,P.O.Box2729,Beijing100080,P.R.China//SchoolofAerospace,TsinghuaUniversity,Beijing100084,P.R.China SchoolofAerospace,TsinghuaUniversity,Beijing100084,P.R.China
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Cites_doi 10.1007/BF02460335
10.1016/0020-7683(72)90038-8
10.1109/9.35810
10.1007/BF00047531
10.2514/3.20195
10.1109/9.133188
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Keywords elastic vibration
rigid-body motion
nonlinear
Coupled rigid-flexible system
attitude stability
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Snippet The influences of nonlinear centrifugal force to large overall attitude motion of coupled rigid-flexible system was investigated. First the nonlinear model of...
O231%O317; The influences of nonlinear centrifugal force to large overall attitude motion of coupled rigid-flexible system was investigated. First the...
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StartPage 594
SubjectTerms 刚体运动
姿态稳定性
弹性变量
耦合刚性-韧性系统
非线性
Title MODEL OF CENTRIFUGAL EFFECT AND ATTITUDE MANEUVER STABILITY OF A COUPLED RIGID-FLEXIBLE SYSTEM
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