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 in | Applied mathematics and mechanics Vol. 26; no. 5; pp. 594 - 603 |
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Main Author | |
Format | Journal Article |
Language | English |
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 |
Subjects | |
Online Access | Get full text |
ISSN | 0253-4827 1573-2754 |
DOI | 10.1007/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. |
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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 |
AuthorAffiliation_xml | – name: Beijing Institute of Control Engineering, P.O.Box 2729, Beijing 100080, P.R.China; School of Aerospace, Tsinghua University, Beijing 100084, P.R. China%School of Aerospace, Tsinghua University, Beijing 100084, 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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References | Ma Xingrui (BF02466333_CR1) 2001 Xiao Shifu (BF02466333_CR8) 1998; 18 Enrique Barbieri (BF02466333_CR5) 1988; 110 Li Zhibin (BF02466333_CR10) 2002 P W Likins (BF02466333_CR3) 1972; 8 A M Bloch (BF02466333_CR7) 1989; 15 Hu Zhendong (BF02466333_CR9) 1999; 20 T R Kane (BF02466333_CR2) 1987; 10 Y Sakawa (BF02466333_CR4) 1989; 34 Ö Mörgul (BF02466333_CR6) 1991; 36 |
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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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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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