Optimal Deployment of a Tethered Satellite using Tension Control

被引：11

作者：

Steindl, Alois ^{[1
]}

机构：

[1] Vienna Univ Technol, Inst Mech & Mechatron, Vienna, Austria

来源：

IFAC PAPERSONLINE | 2015年 / 48卷 / 01期

关键词：

Tension control; Time optimal control; Pontryagin's Maximum Principle; Elliptic orbit;

D O I：

10.1016/j.ifacol.2015.05.173

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

We investigate the deployment of a tethered satellite from the space station, which moves along a Keplerian elliptic orbit with small eccentricity. The control of the satellite's motion is performed by applying a restricted tension force along the connecting tether. The goal of the control is to steer the satellite from a periodic state close to the local vertical position to a periodic motion farther away from the space station in shortest time. (C) 2015, IFAC (International Antomatic Control) Hosting by Elsevier Ltd. All rights reserved.

引用

页码：53 / +

页数：2

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