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Research Article

Orbit design and mission planning for global observation of Jupiter

An-Yi Huang1,2Bing Yan1Zhen-Yu Li1Peng Shu1Ya-Zhong Luo1( )Zhen Yang1
National University of Defense Technology, Changsha 410073, China
State Key Laboratory of Astronautic Dynamics, Xi’an 710043, China
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Abstract

This paper presents the method created by the National University of Defense Technology (NUDT) team in the 10th China Trajectory Optimization Competition, which entails a 3-year observation mission of 180 regions on Jupiter. The proposed method can be divided into three steps. First, a preliminary analysis and evaluation via an analytical method is undertaken to decide whether the third subtask of the mission, i.e., exploring the Galilean moons, should be ignored. Second, a near-optimal orbit for magnetic field observation is designed by solving an analytical equation. Third, a set of observation windows and their sequence are optimized using a customized genetic algorithm. The final index obtained is 354.505, ranking second out of all teams partaking in the competition.

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Astrodynamics
Pages 39-48
Cite this article:
Huang A-Y, Yan B, Li Z-Y, et al. Orbit design and mission planning for global observation of Jupiter. Astrodynamics, 2021, 5(1): 39-48. https://doi.org/10.1007/s42064-020-0090-9

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Received: 15 June 2020
Accepted: 11 July 2020
Published: 03 December 2020
© Tsinghua University Press 2020
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