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Quasi-satellite system for leader-follower spacecraft formation


Citation

Mohd Harithuddin, Ahmad Salahuddin (2016) Quasi-satellite system for leader-follower spacecraft formation. In: AEROTECH VI - Innovation in Aerospace Engineering and Technology, 8–9 Nov 2016 , Kuala Lumpur, Malaysia. (pp. 1-9).

Abstract

The quasi-satellite motion is where a celestial body appears to orbit around another body that is also orbiting a common focus. The recent discoveries of asteroids in quasi-satellite motion around the Earth inspired this work. This paper attempts to look into exploiting the quasi-satellite dynamics in nature to provide a new perspective in spacecraft formation flight. We consider a two-spacecraft formation flight in which the follower appears to orbit of the leader in its reference frame. We perform a parametric analysis by varying the orbital elements of leader and follower examine the initial conditions needed to simulate a quasi-satellite formation system. We illustrate the trajectories of the follower spacecraft. This serves two purposes: firstly, to demonstrate formation flight based on the idea of quasi-satellite; and secondly, to gain some insights on the shapes of the resultant "quasi-orbits".


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Additional Metadata

Item Type: Conference or Workshop Item (Paper)
Divisions: Faculty of Engineering
DOI Number: https://doi.org/10.1088/1757-899X/152/1/012034
Publisher: Institute of Physics Publishing
Keywords: Quasi-satellite system; Leader-follower; Spacecraft formation
Depositing User: Nurul Ainie Mokhtar
Date Deposited: 11 Jan 2018 05:43
Last Modified: 11 Jan 2018 05:43
Altmetrics: http://www.altmetric.com/details.php?domain=psasir.upm.edu.my&doi=10.1088/1757-899X/152/1/012034
URI: http://psasir.upm.edu.my/id/eprint/53717
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