Optimal Control of Payload Tossing Using Space Tethered System

被引：5

作者：

Shi, Lu Hong ^{[1
]}

Wang Changqing ^{[1
]}

Yuriy, Zabolotnov ^{[2
]}

Aijun, Li ^{[1
]}

机构：

[1] Northwestern Polytech Univ, Xian 710072, Shanxi, Peoples R China

[2] Samara State Aerosp Univ, Samara 443086, Russia

来源：

IFAC PAPERSONLINE | 2016年 / 49卷 / 17期

关键词：

Space Tethered System; Payload Tossing; Optimal Control; Hamilton Energy; ELLIPTIC ORBITS; DYNAMICS;

D O I：

10.1016/j.ifacol.2016.09.047

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

To transport payload into lunar transfer orbit using spinning tether system, reusable payload tossing system was proposed based on cislunar transfer mission, and optimal control law was developed for payload tossing stage. In the case of insufficient thrust, Hamilton equation was adopted to solve the problem. The numerical result shows that the tossing design is able to transport payload into desired orbit, and the control law could meet mission requirement. Compared to conventional rocket transport, much less propellant is required by the designed system with reusability. (C) 2016, IFAC (International Federation of Automatic Control) Hosting Elsevier Ltd. All rights reseirved.

引用

页码：272 / 277

页数：6

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