Modeling and Observer-Based Vibration Control of a Flexible Spacecraft With External Disturbances
This paper outlines the vibration reduction of a spacecraft with flexible appendage subject to external disturbances. The hybrid dynamic model of the spacecraft is described by both partial differential equations and ordinary differential equations. A vibration control scheme consisting of two bound...
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| Published in | IEEE transactions on industrial electronics (1982) Vol. 66; no. 11; pp. 8648 - 8658 |
|---|---|
| Main Authors | , , , |
| Format | Journal Article |
| Language | English |
| Published |
New York
IEEE
01.11.2019
The Institute of Electrical and Electronics Engineers, Inc. (IEEE) |
| Subjects | |
| Online Access | Get full text |
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| Abstract | This paper outlines the vibration reduction of a spacecraft with flexible appendage subject to external disturbances. The hybrid dynamic model of the spacecraft is described by both partial differential equations and ordinary differential equations. A vibration control scheme consisting of two boundary control laws and a distributed control law is developed to restrain the spacecraft's vibration and track the desired attitude. An infinite-dimensional disturbance observer is introduced as a feedforward compensator to handle unknown external disturbances. Based on the semigroup theory, the extended LaSalle's invariance principle and Lyapunov analysis, the well-posedness and stabilities of the designed control system are both discussed. Simulation results are given for validating the effectiveness of the developed vibration control scheme. |
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| AbstractList | This paper outlines the vibration reduction of a spacecraft with flexible appendage subject to external disturbances. The hybrid dynamic model of the spacecraft is described by both partial differential equations and ordinary differential equations. A vibration control scheme consisting of two boundary control laws and a distributed control law is developed to restrain the spacecraft's vibration and track the desired attitude. An infinite-dimensional disturbance observer is introduced as a feedforward compensator to handle unknown external disturbances. Based on the semigroup theory, the extended LaSalle's invariance principle and Lyapunov analysis, the well-posedness and stabilities of the designed control system are both discussed. Simulation results are given for validating the effectiveness of the developed vibration control scheme. |
| Author | Fu, Yun Liu, Yu Hui, Qing He, Wei |
| Author_xml | – sequence: 1 givenname: Yu orcidid: 0000-0002-4191-5974 surname: Liu fullname: Liu, Yu email: auylau@scut.edu.cn organization: School of Automation Science and Engineering, South China University of Technology, Guangzhou, China – sequence: 2 givenname: Yun surname: Fu fullname: Fu, Yun email: mafuyun@mail.scut.edu.cn organization: School of Automation Science and Engineering, South China University of Technology, Guangzhou, China – sequence: 3 givenname: Wei orcidid: 0000-0002-8944-9861 surname: He fullname: He, Wei email: hewei.ac@gmail.com organization: School of Automation and Electrical Engineering, University of Science and Technology Beijing, Beijing, China – sequence: 4 givenname: Qing orcidid: 0000-0001-9488-5257 surname: Hui fullname: Hui, Qing email: qing.hui@unl.edu organization: Department of Electrical and Computer Engineering, University of Nebraska-Lincoln, Lincoln, NE, USA |
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| Snippet | This paper outlines the vibration reduction of a spacecraft with flexible appendage subject to external disturbances. The hybrid dynamic model of the... |
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| SubjectTerms | Attitude control Boundary control Computer simulation Control systems Control systems design Control theory Decentralized control Disturbance observers Dynamic models Flexible spacecraft Mathematical model observers Ordinary differential equations Partial differential equations partial differential equations (PDEs) Space vehicles Spacecraft tracking Vibration control Vibrations Well posed problems well-posedness |
| Title | Modeling and Observer-Based Vibration Control of a Flexible Spacecraft With External Disturbances |
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