Methodology for CubeSat Debris Collision Avoidance Based on Its Active ADCS System

Author:

González-Rodríguez Desiree1,Orgeira-Crespo Pedro2ORCID,Cappelletti Chantal3,Aguado-Agelet Fernando4ORCID

Affiliation:

1. Doctoral Program in Aerospace Technology, Electromagnetic, Electronic, Computer and Mechanical Engineering, School of Telecommunications, University of Vigo, 36310 Vigo, Spain

2. Department of Mechanical Engineering, Heat Engines and Machines and Fluids, Aerospace Engineering School, University of Vigo, Campus Orense, 32004 Orense, Spain

3. Department of Mechanical, Materials and Manufacturing Engineering, University of Nottingham, Nottingham NG7 2RD, UK

4. Telecommunication Engineering School, University of Vigo, 36310 Vigo, Spain

Abstract

This research assesses the feasibility of a collision avoidance methodology for CubeSats lacking propulsion. The approach involves altering the satellite’s orientation to modify its cross-sectional area and, subsequently, the drag force. Examining altitudes within low Earth orbit (LEO) across 2U, 3U, and 6U CubeSat formats, maneuvers are considered two days before the Time to Closest Approach (TCA). Evaluation against the Conjunction Data Messages (CDMs) threshold miss distances reveals a minimum 7% and maximum 106% deviation in Vertical Distance Difference (VDD), and 68% to 1045% in Horizontal Distance Difference (HDD) concerning the notification threshold. These findings strongly endorse the practicality of the proposed collision avoidance methodology, utilizing CubeSat Attitude Determination and Control Systems (ADCS). Ongoing research focuses on assessing ADCS maneuver execution rates and implementation times, advancing our understanding and applicability of this innovative CubeSat collision avoidance approach.

Publisher

MDPI AG

Subject

Fluid Flow and Transfer Processes,Computer Science Applications,Process Chemistry and Technology,General Engineering,Instrumentation,General Materials Science

Reference25 articles.

1. (2022, July 25). NASA Website: Space Debris and Human Spacecraft, Available online: https://www.nasa.gov/mission_pages/station/news/orbital_debris.html.

2. O’Reilly, D. (2023, February 11). Scopus. Available online: https://www.scopus.com/record/display.uri?eid=2-s2.0-85099955214&origin=resultslist&sort=plf-f&src=s&st1=collision+avoidance+cubesat&sid=b08453557fa8a10a6244f7da8f05a4dc&sot=b&sdt=b&sl=42&s=TITLE-ABS-KEY%28collision+avoidance+cubesat%29&relpos=5&citeCnt=3.

3. S.D. Office (2022). ESA’s Annual Space Environment Report, The European Space Agency.

4. (2022, May 09). ESA’s Space Debris Office. Available online: https://www.esa.int/Safety_Security/Space_Debris/Space_debris_by_the_numbers.

5. Orbital Debris Threat for Space Sustainability and Way Forward;Murtaza;IEEE Access,2020

Cited by 1 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3