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：

[No abstract available]

引用

页码：2213 / 2220

页数：8

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