文章基本信息

标题：Motion Modeling and Deployment Control of a Long Tethered Spacecraft System with an Atmospheric Sounder
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作者：Zhe Dong ; Yuriy M. Zabolotnov ; Changqing Wang 等
期刊名称：Engineering Letters
印刷版ISSN：1816-093X
电子版ISSN：1816-0948
出版年度：2018
卷号：26
期号：4
页码：478-488
出版社：Newswood Ltd
摘要：The paper studies the deployment dynamics of along tethered spacecraft system (TSS) with an atmosphericsounder. The tether (several ten kilometers) is deployed from thespacecraft by means of a mechanism that works only for braking.A dynamic nominal deployment control law is designed in anorbital moving coordinate system taking into account theaerodynamic forces acting on the end-bodies (the spacecraft andatmospheric sounder) and inextensible tether. The motionstability of the TSS is analyzed. The deployment process isstudied in a geocentric coordinate system with consideration ofthe dynamics of control mechanism operation, tether elasticity,and other perturbations. The numerical simulations show thatdesigning the nominal deployment control law taking intoaccount the aerodynamic force reduces the system’s controlerror several times for the deployment process.
关键词：Tethered spacecraft system; atmospheric;sounder; modeling; nominal deployment control law; motion;stability; control error