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Alternative TitleGlobal optimization of low thrust gravity assist trajectory for Jupiter exploration
李小玉; 郑建华; lixiaoyu@nssc.ac.cn
Source Publication中国科学院大学学报
Keyword深空探测 借力飞行 轨道 小推力
Other AbstractThe low thrust gravity assist (LTGA) trajectory to Jupiter is studied and a novel LTGA model is proposed based on impulsive gravity assist and low thrust exponential sinusoid method. A brief description of this method is presented and the solution to the related low thrust Lambert problem is summarized. LTGA schemes of EMJ, EVEJ, and EMEJ are optimized by differential evolution algorithm and then discussed in detail. Simulation results show that EMJ is the best and the proposed model is efficient for the initial design of LTGA trajectory.
Indexed ByCSCD
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Document Type期刊论文
Corresponding Authorlixiaoyu@nssc.ac.cn
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GB/T 7714
李小玉,郑建华,lixiaoyu@nssc.ac.cn. 木星探测小推力借力飞行轨道的全局优化[J]. 中国科学院大学学报,2013,30(5):603-607.
APA 李小玉,郑建华,&lixiaoyu@nssc.ac.cn.(2013).木星探测小推力借力飞行轨道的全局优化.中国科学院大学学报,30(5),603-607.
MLA 李小玉,et al."木星探测小推力借力飞行轨道的全局优化".中国科学院大学学报 30.5(2013):603-607.
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