Authors:
- Provides an analytical approach for continuous low-thrust trajectory design
- Presents a general, two-maneuver transfer procedure from a libration point orbit in the Earth–Moon system to a lunar orbit
- Offers a detailed description of the relative motion of a charged spacecraft around a spacecraft with a magnetic field
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Table of contents (6 chapters)
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Front Matter
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Back Matter
About this book
Given its breadth of coverage, the book offers a valuable reference guide for allengineers and researchers interested in the potential applications of low-energy space missions.
Authors and Affiliations
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School of Astronautics, Northwestern Polytechnical University, Xi'an, China
Jianping Yuan, Yu Cheng, Chong Sun
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Nanjing University, Nanjing, China
Jinglang Feng
About the authors
Jian-ping Yuan received the B.S. and Ph.D.degrees from Northwestern Polytechnical University, Xi’an, China, in 1982 and 1985, respectively. He is currently a Professor in the School of Astronautics, Northwestern Polytechnical University. His research interests are spacecraft flight dynamics and control.
Yu Cheng
Research topic: transfer trajectory design in the three-body problem; relative dynamics of a charged spacecraft under a magnetic field and the potential application in formation flying, stability analysis of the critical points and periodic orbits of the Hamiltonian system, and computation of invariant tori using parameterization method.
Jinglang Feng
Research topic: orbital dynamics around irregular gravitational field, e.g. contact binary asteroid systems, in terms of equilibrium points, periodic orbits and their stability, resonant dynamics, etc. Moreover, the perturbation of solar radiation pressure on the secular dynamics oforbital motion around asteroid are also investigated for mission analysis.
Chong Sun
Research topic: continuous low thrust trajectory design and optimization, including the solar sail low thrust trajectory design, the solar electrical propulsion low thrust trajectory design, and hybrid low thrust trajectory design and its application. For example, the near earth asteroid exploration, the period orbit mission in three body system.
Bibliographic Information
Book Title: Low Energy Flight: Orbital Dynamics and Mission Trajectory Design
Authors: Jianping Yuan, Yu Cheng, Jinglang Feng, Chong Sun
DOI: https://doi.org/10.1007/978-981-13-6130-2
Publisher: Springer Singapore
eBook Packages: Engineering, Engineering (R0)
Copyright Information: Science Press and Springer Nature Singapore Pte Ltd. 2019
Hardcover ISBN: 978-981-13-6129-6Published: 27 March 2019
eBook ISBN: 978-981-13-6130-2Published: 19 March 2019
Edition Number: 1
Number of Pages: X, 209
Number of Illustrations: 28 b/w illustrations, 108 illustrations in colour
Topics: Aerospace Technology and Astronautics, Mathematical Applications in the Physical Sciences
Industry Sectors: Aerospace, Electronics, Energy, Utilities & Environment, Engineering, IT & Software, Materials & Steel, Oil, Gas & Geosciences