|
|
|||
|
||||
OverviewThis book considers global solutions to the restricted three-body problem from a geometric point of view. The authors seek dynamical channels in the phase space which wind around the planets and moons and naturally connect them. These low energy passageways could slash the amount of fuel spacecraft need to explore and develop our solar system. In order to effectively exploit these passageways, the book addresses the global transport. It goes beyond the traditional scope of libration point mission design, developing tools for the design of trajectories which take full advantage of natural three or more body dynamics, thereby saving precious fuel and gaining flexibility in mission planning. This is the key for the development of some NASA mission trajectories, such as low energy libration point orbit missions (e.g., the sample return Genesis Discovery Mission), low energy lunar missions and low energy tours of outer planet moon systems, such as a mission to tour and explore in detail the icy moons of Jupiter. This book can serve as a valuable resource for graduate students and advanced undergraduates in applied mathematics and aerospace engineering, as well as a manual for practitioners who work on libration point and deep space missions in industry and at government laboratories. The authors include a wealth of background material, but also bring the reader up to a portion of the research frontier. Full Product DetailsAuthor: Wang Sang Koon , Martin W. Lo , Jerrold Marsden , Shane D. RossPublisher: Springer-Verlag New York Inc. Imprint: Springer-Verlag New York Inc. Volume: v. 332 ISBN: 9780387495156ISBN 10: 0387495150 Pages: 335 Publication Date: 01 June 2009 Audience: College/higher education , Professional and scholarly , Undergraduate , Postgraduate, Research & Scholarly Format: Hardback Publisher's Status: Out of Stock Indefinitely Availability: Awaiting stock Table of ContentsAcknowledgments.- Preface.- Related Literature.- Introduction.- Motion near the Collinear Equilibrium Points.- Heteroclinic Connection and Global Orbit Structure.- Construction of Trajectories with Prescribed Itineraries.- Trajectories in the Four-Body Problem.- Extension to the Spatial Problem: Halo Orbits and Their Computation.- Invariant Manifolds and End-to-End Transfer.- Transfer CorrectionManeuvers and Station-Keeping Strategies.- Invariant Manifolds and Complex Mission Designs.- Multi-Moon Orbiters and Low Thrust Trajectories.ReviewsAuthor InformationTab Content 6Author Website:Countries AvailableAll regions |
||||