Delta-V and ground metric investigations for responsive satellite formation flying

This paper studies a responsive mission involving a dual spacecraft flying formation system. A graphical solution based on the selective dependent variables for acquiring the local and global optimum impulsive velocities is proposed to obtain the minimum orbital transfer velocity changes as well as...

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Main Authors: Yahya, Nor Affendy, Varatharajoo, Renuganth, Harithuddin, A. S. M., Razoumny, Yury
Format: Article
Published: Elsevier 2022
Online Access:http://psasir.upm.edu.my/id/eprint/100888/
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author Yahya, Nor Affendy
Varatharajoo, Renuganth
Harithuddin, A. S. M.
Razoumny, Yury
author_facet Yahya, Nor Affendy
Varatharajoo, Renuganth
Harithuddin, A. S. M.
Razoumny, Yury
author_sort Yahya, Nor Affendy
building UPM Institutional Repository
collection Online Access
description This paper studies a responsive mission involving a dual spacecraft flying formation system. A graphical solution based on the selective dependent variables for acquiring the local and global optimum impulsive velocities is proposed to obtain the minimum orbital transfer velocity changes as well as improving its nadir ground coverage. These studies are conducted using finite thrust of single, dual and three-impulse modes under the condition of unperturbed environment. Based on the obtained results, the relationship between the number of impulses applied and the amount of fuel consumed to retain the leader-follower formation separation is inversely proportional. Whereas, in all cases of the ground metric studies, the formation inclination has shown a dominant influence over other parameters for maximizing the total nadir ground coverage and the swath length.
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institution Universiti Putra Malaysia
institution_category Local University
last_indexed 2025-11-15T13:32:57Z
publishDate 2022
publisher Elsevier
recordtype eprints
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spelling upm-1008882023-07-26T03:06:24Z http://psasir.upm.edu.my/id/eprint/100888/ Delta-V and ground metric investigations for responsive satellite formation flying Yahya, Nor Affendy Varatharajoo, Renuganth Harithuddin, A. S. M. Razoumny, Yury This paper studies a responsive mission involving a dual spacecraft flying formation system. A graphical solution based on the selective dependent variables for acquiring the local and global optimum impulsive velocities is proposed to obtain the minimum orbital transfer velocity changes as well as improving its nadir ground coverage. These studies are conducted using finite thrust of single, dual and three-impulse modes under the condition of unperturbed environment. Based on the obtained results, the relationship between the number of impulses applied and the amount of fuel consumed to retain the leader-follower formation separation is inversely proportional. Whereas, in all cases of the ground metric studies, the formation inclination has shown a dominant influence over other parameters for maximizing the total nadir ground coverage and the swath length. Elsevier 2022-04 Article PeerReviewed Yahya, Nor Affendy and Varatharajoo, Renuganth and Harithuddin, A. S. M. and Razoumny, Yury (2022) Delta-V and ground metric investigations for responsive satellite formation flying. Acta Astronautica, 193. 20 - 34. ISSN 0094-5765 https://www.sciencedirect.com/science/article/pii/S0094576521006688 10.1016/j.actaastro.2021.12.033
spellingShingle Yahya, Nor Affendy
Varatharajoo, Renuganth
Harithuddin, A. S. M.
Razoumny, Yury
Delta-V and ground metric investigations for responsive satellite formation flying
title Delta-V and ground metric investigations for responsive satellite formation flying
title_full Delta-V and ground metric investigations for responsive satellite formation flying
title_fullStr Delta-V and ground metric investigations for responsive satellite formation flying
title_full_unstemmed Delta-V and ground metric investigations for responsive satellite formation flying
title_short Delta-V and ground metric investigations for responsive satellite formation flying
title_sort delta-v and ground metric investigations for responsive satellite formation flying
url http://psasir.upm.edu.my/id/eprint/100888/
http://psasir.upm.edu.my/id/eprint/100888/
http://psasir.upm.edu.my/id/eprint/100888/