Image from Google Jackets

Low Energy Flight : Orbital Dynamics and Mission Trajectory Design / by Jianping Yuan, Yu Cheng, Jinglang Feng, Chong Sun

By: Yuan, Jianping., autor
Contributor(s): SpringerLink (Online service) | Cheng, Yu., autor | Feng, Jinglang., autor | Sun, Chong., autor
Series: (Engineering (Springer-11647)).Publisher: Singapore : Springer Singapore : Imprint: Springer, 2019Description: 1 recurso en línea (X, 209 páginas) : 136 ilustraciones, 108 ilustraciones a color.ISBN: 9789811361302.Subject: AstrodinámicaOnline resources: Acceso a este recurso digital (usuarios Universidad Europea de Madrid)Digital Resources
Contents:
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.
Abstract: 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. .
Tags from this library: No tags from this library for this title. Log in to add tags.
Star ratings
    Average rating: 0.0 (0 votes)
Holdings
Item type Current library Collection Call number Status Date due Barcode Item holds
LIBRO-E NO PRÉSTAMO LIBRO-E NO PRÉSTAMO Madrid Digital Acceso Electrónico (UEM) Ciencias e Ingeniería TL1050 2019 EB (Browse shelf(Opens below)) Acceso electrónico eBooks24062735
Total holds: 0

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. .

There are no comments on this title.

to post a comment.