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Jupiter system exploration trajectory design: Summary of the winning solution at CTOC10 被引量:2
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作者 Haiyang Zhang Yabo Hu +5 位作者 Zichen Fan Jie Lv Huidong Ma Ze Yu Mingying Huo Gang Zhang 《Astrodynamics》 CSCD 2021年第1期13-26,共14页
This paper presents the methods and results submitted by the winning team from Harbin Institute of Technology of the 10th China Trajectory Optimization Competition(CTOC10).The problem posed by CTOC10 requires explorin... This paper presents the methods and results submitted by the winning team from Harbin Institute of Technology of the 10th China Trajectory Optimization Competition(CTOC10).The problem posed by CTOC10 requires exploring the Jupiter system using a combined spacecraft.The exploration mission consists of the detection of Jupiter’s magnetic field and an exploration of the Galilean moons.The mission is completed through three steps:problem analysis,orbital design process,and data processing.The orbital design process is mainly divided into four parts,namely,repeating groundtrack orbit design,gravity-assisted orbit design,initial orbit parameter selection,and local optimization adjustment.The designed orbit is then evaluated using a heuristic optimization algorithm applied during the data processing.Finally,six full-coverage observations of Jupiter’s magnetic field are realized under the constraints of fuel and time.The final index of the submitted result is 357.8067. 展开更多
关键词 China Trajectory Optimization Competition jupiter exploration repeating ground-track orbit gravity assist
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Orbit design and mission planning for global observation of Jupiter 被引量:1
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作者 An-Yi Huang Bing Yan +3 位作者 Zhen-Yu Li Peng Shu Ya-Zhong Luo Zhen Yang 《Astrodynamics》 CSCD 2021年第1期39-48,共10页
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 Jupi... 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. 展开更多
关键词 jupiter exploration resonance orbit repeating orbit design observation planning
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