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Bau, Giulio and Bombardelli, Claudio and Peláez Álvarez, Jesús and Lorenzini, Enrico C. and Francesconi, Alessandro (2010). A Variational Method for the Propagation of Spacecraft Relative Motion.. In: "20th AAS/AIAA Space Flight Mechanics Meeting 2010", 14/02/2010 - 17/02/2010, San Diego, California, EE.UU:. ISBN 9780877035602.
Title: | A Variational Method for the Propagation of Spacecraft Relative Motion. |
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Author/s: |
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Item Type: | Presentation at Congress or Conference (Article) |
Event Title: | 20th AAS/AIAA Space Flight Mechanics Meeting 2010 |
Event Dates: | 14/02/2010 - 17/02/2010 |
Event Location: | San Diego, California, EE.UU: |
Title of Book: | Advances in the Astronautical Sciences Series. Proceedings of 20th AAS/AIAA Space Flight Mechanics Meeting |
Date: | 2010 |
ISBN: | 9780877035602 |
Volume: | 136 |
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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A new formulation of the spacecraft relative motion for a generic orbit is presented based on the orbital propagation method proposed by Peláez et al. in 2006 [1]. Two models have been developed. In the first model the method is applied to each spacecraft using a time synchronization of the system dynamical states. In the second model we employ a local orbital reference frame with a linearization of gravitational terms, apply the method to the formation center of mass and propagate the relative dynamics with respect to the center of mass reference orbit. The models are compared in terms of computational speed for the case of a bounded triangular formation
Item ID: | 9571 |
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DC Identifier: | https://oa.upm.es/9571/ |
OAI Identifier: | oai:oa.upm.es:9571 |
Official URL: | http://www.space-flight.org/AAS_meetings/2010_winter/2010%20winter.html |
Deposited by: | Memoria Investigacion |
Deposited on: | 04 Nov 2011 09:16 |
Last Modified: | 25 May 2015 13:50 |