Adaptive-Mesh Sequential Convex Programming for Space Trajectory Optimization

被引：2
|
作者：
Kumagai, Naoya [1 ]
Oguri, Kenshiro [1 ]
机构：
[1] Purdue Univ, Sch Aeronaut & Astronaut, W Lafayette, IN 47907 USA
来源：
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 2024年 / 47卷 / 10期
关键词：
Mission Planning and Design; Trajectory Optimization; Interplanetary Spaceflight; Low-Thrust Interplanetary Spaceflight; Sequential Convex Programming; Pontryagin's Minimum Principle; LOW-THRUST; REFINEMENT METHOD;
D O I：
10.2514/1.G008107
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
引用
收藏
页码：2213 / 2220
页数：8
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