Comparison of LPM, GPM and RPM for Optimization of Low-Thrust Earth-Mars Rendezvous Trajectories

被引：0
|
作者：
Wang, Yukai [1 ]
Zhu, Yongsheng [2 ]
Jiang, Xiuqiang [1 ]
Li, Shuang [1 ]
机构：
[1] Nanjing Univ Aeronaut & Astronaut, Coll Astronaut, Nanjing 210016, Jiangsu, Peoples R China
[2] Shanghai Engn Ctr Microsatellites, Shanghai 201203, Peoples R China
来源：
2014 IEEE CHINESE GUIDANCE, NAVIGATION AND CONTROL CONFERENCE (CGNCC) | 2014年
关键词：
DESIGN;
D O I：
暂无
中图分类号：
TM [电工技术]; TN [电子技术、通信技术];
学科分类号：
0808 ; 0809 ;
摘要：
The performance comparison is performed among Legendre (LPM), Gauss (GPM), and Radau (RPM) pseudospectral methods, which are utilized to optimize the low-thrust Earth-Mars rendezvous trajectories. In order to provide a fair comparison condition, a shape-based approach is implemented to provide equivalent initial guesses for all the next accurate optimization, and the SQP algorithm is used to solve the resulting nonlinear programming problem for each of the discretization. The behavior and performance of the three pseudospectral methods are compared on the mission of Earth-Mars Rendezvous in 2013.
引用
收藏
页码：2461 / 2467
页数：7
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