人工拉格朗日轨道约束控制下太阳帆的可控度

2019 IEEE 4th Advanced Information Technology, Electronic and Automation Control Conference (IAEAC) Pub Date : 2019-12-01 DOI:10.1109/IAEAC47372.2019.8997864

Bin Du, G. Vukovich

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引用次数: 0

摘要

太阳能航行是一项仍处于起步阶段的新技术，它具有巨大的潜力，可以完成传统航天器无法完成的大量任务。本文利用系统离散化计算的方法，对人工拉格朗日轨道上具有约束控制输入的太阳帆的可控性进行了评价。结果表明，太阳帆的可控性随人工拉格朗日轨道位置的不同以及控制输入的约束而变化，这为我们更好地了解太阳帆的特性提供了更多的定量信息，并可能有助于改进未来空间任务中太阳帆的设计。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

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Degree of Controllability of Solar Sail with Constrained Control in Artificial Lagrangian Orbits

Solar sailing is a novel technology that is still in its infancy, with great potential for a large number of missions that are not possible with conventional spacecraft. The degree of controllability of solar sail with constrained control inputs in artificial Lagrangian orbits is evaluated in this paper, using a method to compute the degree of controllability via system discretization. The results reveal that the controllability of solar sail varies depending on the location in the artificial Lagrangian orbits, as well as the constrained control inputs of the sail, which give us more quantitative information to better understand the characteristics of solar sail, and may help to improve the design of solar sails for future space missions.

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2019 IEEE 4th Advanced Information Technology, Electronic and Automation Control Conference (IAEAC)

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