微卫星群无集中协调模式形成的实现

Khalfan Alremeithi, Jorge Miranda Dias, Giula de Masi
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引用次数: 1

摘要

航天任务商业化的新时代引入了多卫星任务的新思路和任务设计范式。这是不同卫星工业应用的趋势,如地球观测和卫星通信,因为它简单,便宜,增加了系统的稳健性。多卫星任务引入了不同的发展路线,如星座、轨迹形成和群形成,以适应不同类型的任务要求。受空间超低频射电天文台(SULFRO)项目的启发,基于一颗微卫星母星和12颗纳米卫星子星组成的星座概念,提出了一种不使用集中协调的分散群形成模型。该方法基于小卫星共享编队相对位置并通过高速星间链路通信的假设。假设微卫星编队和部署的空间为二维空间,该方法成功地将12颗微卫星部署在目标编队中。该方法包括编队跟踪、运动控制和避碰三种状态。这三个国家确保微型卫星共享位置并跟踪确保微型卫星群的稳定和安全所需的新编队,从而为该方法的成功作出了贡献。本文还对系统的功耗和系统的稳定性进行了研究。提出的方法在三种不同的验证场景中进行了模拟,并成功地获得了所需的地层。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Realization of Pattern Formation For Micro-satellite Swarms Without a Centralized Coordination
The new era of commercializing space missions introduced a new mindset and mission design paradigms of multi-satellite missions. This is trending in different satellite industry applications such as Earth observation and satellite communication as it is simple, cheap and increases the system robustness. Multi-satellite missions introduced different lines of development like constellations, trail formation and swarm formations to fit different type of missions requirements. Inspired by the Space Ultra-Low Frequency Radio Observatory (SULFRO) project, based on the concept of a constellation of a micro-satellite mothership and 12 nano-satellite daughters, designed for sky observation and space discovery, in this paper, we propose a model of decentralized swarm formation without using a centralized coordination. The proposed method is based on the assumption that micro-satellite share relative position of the formation and communicate through high speed inter-satellite link. Assuming a 2D space for the micro-satellite formation and deployment, the proposed methodology succeeded to deploy the 12 micro-satellites in their targeted formation. The proposed methodology consists of three states that are: Formation Tracking, Movement Control and Collision Avoidance. These three states contributed in the success of the methodology by ensuring that the micro-satellite share the positions and track the new formation needed to ensure the stability and safety of the micro-satellite swarm. The paper also investigated the power consumption of the system and the system stability. The proposed methodology is simulated in three different validation scenarios and successfully achieved the required formation.
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