Geomagnetic Field Tracker for Deorbiting a CubeSat Using Electric Thrusters

Morales, JE, Kim, J orcid.org/0000-0002-3456-6614 and Richardson, RR (2019) Geomagnetic Field Tracker for Deorbiting a CubeSat Using Electric Thrusters. Journal of Guidance, Control, and Dynamics, 42 (5). pp. 1157-1165. ISSN 0731-5090

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Authors/Creators:
Copyright, Publisher and Additional Information: © 2019 by Jose Emmanuel Morales Robles. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. This is an author produced version of a paper accepted for publication in Journal of Guidance, Control, and Dynamics. Uploaded in accordance with the publisher's self-archiving policy.
Keywords: CubeSat; De-orbiting; Geomagnetic field tracking; Electric thruster; Satellite
Dates:
  • Accepted: 18 January 2019
  • Published (online): 28 February 2019
  • Published: May 2019
Institution: The University of Leeds
Academic Units: The University of Leeds > Faculty of Engineering & Physical Sciences (Leeds) > School of Mechanical Engineering (Leeds) > Institute of Engineering Systems and Design (iESD) (Leeds)
Depositing User: Symplectic Publications
Date Deposited: 24 Jan 2019 08:52
Last Modified: 04 Jun 2019 05:29
Status: Published
Publisher: American Institute of Aeronautics and Astronautics
Identification Number: https://doi.org/10.2514/1.G003908

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