Recent advances in celestial and space mechanics
Author(s)
Bibliographic Information
Recent advances in celestial and space mechanics
(Mathematics for industry / editor in chief, Masato Wakayama, v. 23)
Springer, c2016
Available at 2 libraries
  Aomori
  Iwate
  Miyagi
  Akita
  Yamagata
  Fukushima
  Ibaraki
  Tochigi
  Gunma
  Saitama
  Chiba
  Tokyo
  Kanagawa
  Niigata
  Toyama
  Ishikawa
  Fukui
  Yamanashi
  Nagano
  Gifu
  Shizuoka
  Aichi
  Mie
  Shiga
  Kyoto
  Osaka
  Hyogo
  Nara
  Wakayama
  Tottori
  Shimane
  Okayama
  Hiroshima
  Yamaguchi
  Tokushima
  Kagawa
  Ehime
  Kochi
  Fukuoka
  Saga
  Nagasaki
  Kumamoto
  Oita
  Miyazaki
  Kagoshima
  Okinawa
  Korea
  China
  Thailand
  United Kingdom
  Germany
  Switzerland
  France
  Belgium
  Netherlands
  Sweden
  Norway
  United States of America
Note
Includes bibliographical references
Description and Table of Contents
Description
This book presents recent advances in space and
celestial mechanics, with a focus on the N-body
problem and astrodynamics, and explores the development and application of computational techniques in both
areas. It highlights the design of space transfers with various modes of
propulsion, like solar sailing and low-thrust transfers between libration point
orbits, as well as a broad range of targets and applications, like rendezvous
with near Earth objects. Additionally, it includes contributions on the
non-integrability properties of the collinear three- and four-body problem, and
on general conditions for the existence of stable, minimum energy
configurations in the full N-body problem.
A valuable resource for physicists and mathematicians with research interests in celestial
mechanics, astrodynamics and optimal control as applied to space
transfers, as well as for professionals and companies in the industry.
Table of Contents
Preface.- List of Contributors.- Integrability and Non-Integrability of N-Body Problems.- Relative Equilibria in the Full N-Body Problem with Applications to the Equal Mass Problem.- Station Keeping Strategies for a Solar Sail in the Solar System.- Minimum Fuel Trip from a L2 Earth-Moon Halo Orbit to Asteroid 2006 RH120.- Low-Thrust Transfers Between Libration Point Orbits Without Explicit Use of Manifolds.- Time-Minimum Control of the Elliptic Restricted Three-Body Problem Applied to Space Transfer.- On Local Optima in Minimum Time Control of the Restricted Three-Body Problem.
by "Nielsen BookData"