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Bombardelli, Claudio, Urrutxua, Hodei, Merino Martínez, Mario, Ahedo Galilea, Eduardo and Peláez Álvarez, Jesús (2012). Relative Dynamics and Control of an Ion Beam Shepherd Satellite. In: "22nd AAS/AIAA Space Flight Mechanics Meeting", 29/01/2012 - 02/02/2012, Charleston, South Carolina, USA. ISBN 978-0-87703-581-7. pp. 2145-2157.
Title: | Relative Dynamics and Control of an Ion Beam Shepherd Satellite |
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Author/s: |
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Item Type: | Presentation at Congress or Conference (Article) |
Event Title: | 22nd AAS/AIAA Space Flight Mechanics Meeting |
Event Dates: | 29/01/2012 - 02/02/2012 |
Event Location: | Charleston, South Carolina, USA |
Title of Book: | Advances in the Astronautical Sciences |
Date: | 2012 |
ISBN: | 978-0-87703-581-7 |
Volume: | 143 |
Subjects: | |
Faculty: | E.T.S.I. Aeronáuticos (UPM) |
Department: | Física Aplicada a la Ingeniería Aeronáutica [hasta 2014] |
Creative Commons Licenses: | Recognition - No derivative works - Non commercial |
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The ion beam shepherd (IBS) is a recently proposed concept for modifying the orbit and/or attitude of a generic orbiting body in a contactless manner, which makes it a candidate technology for active space debris removal. In this paper we deal with the problem of controlling the relative position of a shepherd satellite coorbiting at small separation distance with a target debris. After deriving the orbit relative motion equations including the effect of the ion beam perturbation we study the system stability and propose different control strategies.
Item ID: | 22872 |
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DC Identifier: | https://oa.upm.es/22872/ |
OAI Identifier: | oai:oa.upm.es:22872 |
Official URL: | http://www.univelt.com/book=3597 |
Deposited by: | Memoria Investigacion |
Deposited on: | 14 Nov 2014 17:46 |
Last Modified: | 14 Nov 2014 17:46 |