Low Energy Flight: Orbital Dynamics and Mission Trajectory Design (Record no. 76137)

000 -LEADER
fixed length control field 03532nam a22005535i 4500
001 - CONTROL NUMBER
control field 978-981-13-6130-2
005 - DATE AND TIME OF LATEST TRANSACTION
control field 20220801214243.0
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION
fixed length control field 190319s2019 si | s |||| 0|eng d
020 ## - INTERNATIONAL STANDARD BOOK NUMBER
ISBN 9789811361302
-- 978-981-13-6130-2
082 04 - CLASSIFICATION NUMBER
Call Number 629.1
100 1# - AUTHOR NAME
Author Yuan, Jianping.
245 10 - TITLE STATEMENT
Title Low Energy Flight: Orbital Dynamics and Mission Trajectory Design
250 ## - EDITION STATEMENT
Edition statement 1st ed. 2019.
300 ## - PHYSICAL DESCRIPTION
Number of Pages X, 209 p. 136 illus., 108 illus. in color.
505 0# - FORMATTED CONTENTS NOTE
Remark 2 Introduction -- Continuous Low Thrust Trajectory Design and optimization -- Study of the Transfer Between Libration Point Orbits and Lunar Orbits in Earth-Moon System -- Lorentz Force Formation Flying in Earth-Moon System -- Orbital Dynamics in the Irregular Gravitational Field - Resonance -- Orbital Dynamics in the Vicinity of Contact Binary Asteroid Systems -- Appendices.
520 ## - SUMMARY, ETC.
Summary, etc The book focuses on the orbital dynamics and mission trajectory (transfer or target trajectory) design of low-energy flight in the context of modern astrodynamics. It investigates various topics that either offer new methods for solving classical problems or address emerging problems that have yet to be studied, including low-thrust transfer trajectory design using the virtual gravity field method; transfer in the three-body system using invariant manifolds; formation flying under space-borne artificial magnetic fields; and the orbital dynamics of highly irregular asteroids. It also features an extensive study of the orbital dynamics in the vicinity of contact binary asteroids, including the 1:1 ground-track resonance, the equilibrium points and their stability, and the third-order analytical solution of orbital motion in the vicinity of the non-collinear equilibrium point. Given its breadth of coverage, the book offers a valuable reference guide for all engineers and researchers interested in the potential applications of low-energy space missions. .
700 1# - AUTHOR 2
Author 2 Cheng, Yu.
700 1# - AUTHOR 2
Author 2 Feng, Jinglang.
700 1# - AUTHOR 2
Author 2 Sun, Chong.
856 40 - ELECTRONIC LOCATION AND ACCESS
Uniform Resource Identifier https://doi.org/10.1007/978-981-13-6130-2
942 ## - ADDED ENTRY ELEMENTS (KOHA)
Koha item type eBooks
264 #1 -
-- Singapore :
-- Springer Nature Singapore :
-- Imprint: Springer,
-- 2019.
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-- text
-- txt
-- rdacontent
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-- computer
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-- rdamedia
338 ## -
-- online resource
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347 ## -
-- text file
-- PDF
-- rda
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Aerospace engineering.
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Astronautics.
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Mathematical physics.
650 14 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Aerospace Technology and Astronautics.
650 24 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Mathematical Physics.
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-- ZDB-2-ENG
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-- ZDB-2-SXE

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