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Low Energy Flight: Orbital Dynamics and Mission Trajectory Design

Record Type:	Language materials, printed : Monograph/item
Title/Author:	Low Energy Flight: Orbital Dynamics and Mission Trajectory Design/ by Jianping Yuan, Yu Cheng, Jinglang Feng, Chong Sun.
Author:	Yuan, Jianping.
other author:	Cheng, Yu.
Description:	X, 209 p. 136 illus., 108 illus. in color.online resource. :
Contained By:	Springer Nature eBook
Subject:	Aerospace engineering. -
Online resource:	https://doi.org/10.1007/978-981-13-6130-2
ISBN:	9789811361302

Low Energy Flight: Orbital Dynamics and Mission Trajectory Design
Yuan, Jianping.

Low Energy Flight: Orbital Dynamics and Mission Trajectory Design[electronic resource] /by Jianping Yuan, Yu Cheng, Jinglang Feng, Chong Sun. - 1st ed. 2019. - X, 209 p. 136 illus., 108 illus. in color.online resource.

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.

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. .

ISBN: 9789811361302

Standard No.: 10.1007/978-981-13-6130-2doiSubjects--Topical Terms:

686400
Aerospace engineering.

LC Class. No.: TL787-4050.22

Dewey Class. No.: 629.1

Low Energy Flight: Orbital Dynamics and Mission Trajectory Design
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520 $a 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. .
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