Review of deployment technology for tethered satellite systems

查看全文 作　　者：[1]B.S.Yu;[1]H.Wen;[1]D.P.Jin

机构地区：[1]State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics

出　　处：《Acta Mechanica Sinica》索引2018年第34卷第4期,共15页

基　　金：funded by the National Natural Science Foundation of China (11672125, 11732006);the Civil Aerospace Pre-research Project of China (D010305);the Research Fund of State Key Laboratory of Mechanics and Control of Mechanical Structures (Nanjing University of Aeronautics and Astronautics, MCMS-0116K01);the Fundamental Research Funds for the Central Universities (NS2016009) 摘　　要：Tethered satellite systems(TSSs) have attracted significant attention due to their potential and valuable applications for scientific research. With the development of various launched on-orbit missions, the deployment of tethers is considered a crucial technology for operation of a TSS. Both past orbiting experiments and numerical results have shown that oscillations of the deployed tether due to the Coriolis force and environmental perturbations are inevitable and that the impact between the space tether and end-body at the end of the deployment process leads to complicated nonlinear phenomena. Hence, a set of suitable control methods plays a fundamental role in tether deployment. This review article summarizes previous work on aspects of the dynamics, control, and ground-based experiments of tether deployment. The relevant basic principles, analytical expressions, simulation cases, and experimental results are presented as well. 关键词：卫星系统技术 CORIOLIS 评论科学研究结果表现 TSS 非线性

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Review of deployment technology for tethered satellite systems

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耦合文献(44)

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