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Low energy flightorbital dynamics an...

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Low energy flightorbital dynamics and mission trajectory design /

紀錄類型:	書目-電子資源 : Monograph/item
正題名/作者:	Low energy flightby Jianping Yuan ... [et al.].
其他題名:	orbital dynamics and mission trajectory design /
其他作者:	Yuan, Jianping.
出版者:	Singapore :Springer Singapore :2019.
面頁冊數:	x, 209 p. :ill., digital ;24 cm.
Contained By:	Springer eBooks
標題:	Gravity assist (Astrodynamics)
電子資源:	https://doi.org/10.1007/978-981-13-6130-2
ISBN:	9789811361302$q(electronic bk.)

Low energy flightorbital dynamics and mission trajectory design /
Low energy flightorbital dynamics and mission trajectory design /[electronic resource] :by Jianping Yuan ... [et al.]. - Singapore :Springer Singapore :2019. - x, 209 p. :ill., digital ;24 cm.

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$q(electronic bk.)

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

836335
Gravity assist (Astrodynamics)

LC Class. No.: TL1075

Dewey Class. No.: 629.411

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505 0 $a 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 $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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