基于进化接触计划设计的纳米卫星星座控制框架

Carlos E. Gonzalez, Alexandre Bergel, Marcos A. Diaz
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引用次数: 1

摘要

航天机构、教育机构和民营企业利用立方体卫星开展新时代的科学研究、培训、技术示范和天基产业。这一不断变化的空间部门的下一步是由数百或数千颗小型或纳米卫星组成的大型卫星星座的组装和运行。这一背景对这些空间项目的生产和操作线提出了新的要求和挑战。本文主要研究具有星间通信的大型纳米卫星星座的敏捷运行问题。提出利用星座接触拓扑结构设计进化算法的接触计划,并利用接触计划信息控制星座运行。然后使用联系人计划创建一个Global Flight plan表,该表总结了执行拟议任务所需的所有操作。因此,卫星和地面站节点只需要一个能够排队、执行和传输飞行计划命令的飞行软件。进化接触计划设计方法显示出良好的可扩展性,为控制由数百或数千颗纳米卫星组成的卫星超级星座提供了可能。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Nanosatellite constellation control framework using evolutionary contact plan design
Space agencies, educational institutions, and private companies have adopted CubeSat nanosatellites to do scientific research, training, technology demonstration, and space-based industries in the New Space era. The next step in this changing space sector corresponds to the assembly and operation of large satellite constellations consisting of hundreds or thousands of small- or nano-satellites. This context adds new requirements and challenges to the production and operation lines of these space projects. This work focuses on the agile operation of a large nanosatellite constellation with inter-satellite communications. We propose using the constellation contact topology to design contact plans using evolutionary algorithms and use the contact plan information to control the constellation operations. The contact plan is then used to create a Global Flight Plan table that summarizes all the operations required to execute a proposed task. Thus, satellites and ground station nodes only need a flight software capable of queuing, executing, and transferring Flight Plan commands. The evolutionary contact plan design approach shows promising scalability results opening the possibility of controlling satellite mega constellation of hundreds or thousands of nanosatellites.
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