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New methods in celestial mechanics and mission design

Authors: Jerrold E. Marsden and Shane D. Ross
Journal: Bull. Amer. Math. Soc. 43 (2006), 43-73
MSC (2000): Primary 70F07, 70F15; Secondary 37J45, 70H33
Published electronically: November 22, 2005
MathSciNet review: 2188175
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Abstract: The title of this paper is inspired by the work of Poincaré [1890, 1892], who introduced many key dynamical systems methods during his research on celestial mechanics and especially the three-body problem. Since then, many researchers have contributed to his legacy by developing and applying these methods to problems in celestial mechanics and, more recently, with the design of space missions. This paper will give a survey of some of these exciting ideas, and we would especially like to acknowledge the work of Michael Dellnitz, Frederic Gabern, Katalin Grubits, Oliver Junge, Wang-Sang Koon, François Lekien, Martin Lo, Sina Ober-Blöbaum, Kathrin Padberg, Robert Preis, and Bianca Thiere. One of the purposes of the AMS Current Events session is to discuss work of others. Even though we were involved in the research reported on here, this short paper is intended to survey many ideas due to our collaborators and others. This survey is by no means complete, and we apologize for not having time or space to do justice to many important and fundamental works. In fact, the results reported on here rely on and were inspired by important preceding work of many others in celestial mechanics, mission design and in dynamical systems. We mention just a few whose work had a positive influence on what is reported here: Brian Barden, Ed Belbruno, Robert Farquhar, Gerard Gómez, George Haller, Charles Jaffé, Kathleen Howell, Linda Petzold, Josep Masdemont, Vered Rom-Kedar, Radu Serban, Carles Simó, Turgay Uzer, Steve Wiggins, and Roby Wilson. In an upcoming monograph (see Koon, Lo, Marsden, and Ross [2005]), the dynamical systems and computational approach and its application to mission design are discussed in detail. One of the key ideas is that the competing gravitational pull between celestial bodies creates a vast array of passageways that wind around the Sun, planets and moons. The boundaries of these passageways are realized geometrically as invariant manifolds attached to equilibrium points and periodic orbits in interlinked three-body problems. In particular, tube-like structures form an interplanetary transport network which will facilitate the exploration of Mercury, the Moon, the asteroids, and the outer solar system, including a mission to assess the possibility of life on Jupiter’s icy moons. The use of these methods in problems in molecular dynamics of interest in chemistry is also briefly discussed.

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Additional Information

Jerrold E. Marsden
Affiliation: Control and Dynamical Systems, California Institute of Technology 107-81, Pasa- dena, California 91125

Shane D. Ross
Affiliation: Department of Aerospace and Mechanical Engineering, University of Southern California, RRB 217, Los Angeles, California 90089-1191

Keywords: Three-body problem, mission design, transport, celestial mechanics
Received by editor(s): May 3, 2005
Received by editor(s) in revised form: July 19, 2005
Published electronically: November 22, 2005
Additional Notes: The first author’s research was supported in part by a Max Planck Research Award and NSF-ITR Grant ACI-0204932.
The second author’s research was supported by an NSF Postdoctoral Fellowship, DMS 0402842.
This article is based on a lecture presented January 7, 2005, at the AMS Special Session on Current Events, Joint Mathematics Meetings, Atlanta, GA
Dedicated: To Henri Poincaré on the 150th anniversary of his birth.
Article copyright: © Copyright 2005 American Mathematical Society
The copyright for this article reverts to public domain 28 years after publication.