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Stable periodic orbits for spacecraft around minor celestial bodies

Stable periodic orbits for spacecraft around minor celestial bodies Astrodynamics Vol. 2, No. 1, 69{86, 2018 https://doi.org/10.1007/s42064-017-0014-5 1;2 3 1 3 4 Yu Jiang (B), Jurgen  Arno Schmidt , Hengnian Li , Xiaodong Liu , and Yue Yang 1. State Key Laboratory of Astronautic Dynamics, Xi'an Satellite Control Center, Xi'an 710043, China 2. School of Aerospace Engineering, Tsinghua University, Beijing 100084, China 3. Astronomy Research Unit, University of Oulu, Finland 4. School of Software Engineering, Xi'an Jiaotong University, Xi'an 710049, China ABSTRACT KEYWORDS We are interested in stable periodic orbits for spacecraft in the gravitational eld of minor asteroid celestial bodies. The stable periodic orbits around minor celestial bodies are useful not only comet for the mission design of the deep space exploration, but also for studying the long-time deep space exploration stability of small satellites in the large-size-ratio binary asteroids. The irregular shapes periodic orbits and gravitational elds of the minor celestial bodies are modeled by the polyhedral model. stability Using the topological classi cations of periodic orbits and the grid search method, the stable orbit design periodic orbits can be calculated and the topological cases can be determined. Furthermore, we nd ve di erent types of stable periodic orbits around minor celestial bodies: (1) stable http://www.deepdyve.com/assets/images/DeepDyve-Logo-lg.png Astrodynamics Springer Journals

Stable periodic orbits for spacecraft around minor celestial bodies

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Publisher
Springer Journals
Copyright
2017 Chinese Society of Theoretical and Applied Mechanics and Tsinghua University Press and Springer Nature Singapore Pte Ltd.
ISSN
2522-008X
eISSN
2522-0098
DOI
10.1007/s42064-017-0014-5
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Abstract

Astrodynamics Vol. 2, No. 1, 69{86, 2018 https://doi.org/10.1007/s42064-017-0014-5 1;2 3 1 3 4 Yu Jiang (B), Jurgen  Arno Schmidt , Hengnian Li , Xiaodong Liu , and Yue Yang 1. State Key Laboratory of Astronautic Dynamics, Xi'an Satellite Control Center, Xi'an 710043, China 2. School of Aerospace Engineering, Tsinghua University, Beijing 100084, China 3. Astronomy Research Unit, University of Oulu, Finland 4. School of Software Engineering, Xi'an Jiaotong University, Xi'an 710049, China ABSTRACT KEYWORDS We are interested in stable periodic orbits for spacecraft in the gravitational eld of minor asteroid celestial bodies. The stable periodic orbits around minor celestial bodies are useful not only comet for the mission design of the deep space exploration, but also for studying the long-time deep space exploration stability of small satellites in the large-size-ratio binary asteroids. The irregular shapes periodic orbits and gravitational elds of the minor celestial bodies are modeled by the polyhedral model. stability Using the topological classi cations of periodic orbits and the grid search method, the stable orbit design periodic orbits can be calculated and the topological cases can be determined. Furthermore, we nd ve di erent types of stable periodic orbits around minor celestial bodies: (1) stable

Journal

Astrodynamics – Springer Journals

Published: Mar 1, 2018

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