Application of Pulsar-Based Navigation for Deep-Space CubeSats

IF 0.1 4区 工程技术 Q4 ENGINEERING, AEROSPACE
Andrea Malgarini, V. Franzese, F. Topputo
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引用次数: 1

Abstract

This paper investigates the use of pulsar-based navigation for deep-space CubeSats. A novel approach for dealing with the onboard computation of navigational solutions and timekeeping capabilities of a spacecraft in a deep-space cruise is shown, and the related implementation and numerical simulations are discussed. The pulsar’s signal detection, processing, and exploitation are simulated for navigation onboard a spacecraft, thus showing the feasibility of autonomous state estimation in deep space even for miniaturized satellites.
脉冲星导航在深空立方体卫星中的应用
本文研究了基于脉冲星的深空立方体卫星导航的应用。提出了一种处理航天器在深空巡航中导航解和计时能力的机载计算的新方法,并讨论了相关的实现和数值模拟。通过对脉冲星信号的探测、处理和利用进行了航天器导航仿真,验证了小型卫星在深空自主状态估计的可行性。
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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来源期刊
Aerospace America
Aerospace America 工程技术-工程:宇航
自引率
0.00%
发文量
9
审稿时长
4-8 weeks
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