Orbit modeling (English Wikipedia)

Analysis of information sources in references of the Wikipedia article "Orbit modeling" in English language version.

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So named for Philip H. Cowell, who, with A.C.D. Cromellin, used a similar method to predict the return of Halley's comet. Brouwer, Dirk; Clemence, Gerald M. (1961). Methods of Celestial Mechanics. Academic Press, New York and London. p. 186.

books.google.com

Moulton, Forest Ray (1914). "Chapter IX". An Introduction to Celestial Mechanics (Second Revised ed.). Macmillan. ISBN 9780598943972.

doi.org

Peláez, Jesús; José Manuel Hedo; Pedro Rodríguez de Andrés (13 October 2006). "A special perturbation method in orbital dynamics". Celest. Mech. Dyn. Astron. 97 (2): 131–150. Bibcode:2007CeMDA..97..131P. doi:10.1007/s10569-006-9056-3. S2CID 35352081.

harvard.edu

ui.adsabs.harvard.edu

Peláez, Jesús; José Manuel Hedo; Pedro Rodríguez de Andrés (13 October 2006). "A special perturbation method in orbital dynamics". Celest. Mech. Dyn. Astron. 97 (2): 131–150. Bibcode:2007CeMDA..97..131P. doi:10.1007/s10569-006-9056-3. S2CID 35352081.

jhuapl.edu

messenger.jhuapl.edu

"MESSENGER Sails on Sun's Fire for Second Flyby of Mercury". 2008-09-05. Archived from the original on 2013-05-14. On September 4, the MESSENGER team announced that it would not need to implement a scheduled maneuver to adjust the probe's trajectory. This is the fourth time this year that such a maneuver has been called off. The reason? A recently implemented navigational technique that makes use of solar-radiation pressure (SRP) to guide the probe has been extremely successful at maintaining MESSENGER on a trajectory that will carry it over the cratered surface of Mercury for a second time on October 6.

semanticscholar.org

api.semanticscholar.org

Peláez, Jesús; José Manuel Hedo; Pedro Rodríguez de Andrés (13 October 2006). "A special perturbation method in orbital dynamics". Celest. Mech. Dyn. Astron. 97 (2): 131–150. Bibcode:2007CeMDA..97..131P. doi:10.1007/s10569-006-9056-3. S2CID 35352081.

upm.es

oa.upm.es

Peláez, Jesús; José Manuel Hedo; Pedro Rodríguez de Andrés (13 October 2006). "A special perturbation method in orbital dynamics". Celest. Mech. Dyn. Astron. 97 (2): 131–150. Bibcode:2007CeMDA..97..131P. doi:10.1007/s10569-006-9056-3. S2CID 35352081.

ocw.upm.es

Delgado, Manuel. "Third Body Perturbation Modeling the Space Environment" (PDF). European Masters in Aeronautics and Space. Universidad Polit ´ecnica de Madrid. Archived from the original (PDF) on 18 February 2015. Retrieved 27 November 2012.

web.archive.org

Delgado, Manuel. "Third Body Perturbation Modeling the Space Environment" (PDF). European Masters in Aeronautics and Space. Universidad Polit ´ecnica de Madrid. Archived from the original (PDF) on 18 February 2015. Retrieved 27 November 2012.
"MESSENGER Sails on Sun's Fire for Second Flyby of Mercury". 2008-09-05. Archived from the original on 2013-05-14. On September 4, the MESSENGER team announced that it would not need to implement a scheduled maneuver to adjust the probe's trajectory. This is the fourth time this year that such a maneuver has been called off. The reason? A recently implemented navigational technique that makes use of solar-radiation pressure (SRP) to guide the probe has been extremely successful at maintaining MESSENGER on a trajectory that will carry it over the cratered surface of Mercury for a second time on October 6.