Convex Low-Thrust Trajectory Optimization with No-Thrust Constraints and Moving Target

被引：0
|
作者：
Hofmann, Christian [1 ,2 ]
Topputo, Francesco [1 ]
机构：
[1] Polytech Univ Milan, Dept Aerosp Sci & Technol, Via La Masa 34, I-20156 Milan, Italy
[2] MIT, Dept Aeronaut & Astronaut, Cambridge, MA 02139 USA
来源：
JOURNAL OF SPACECRAFT AND ROCKETS | 2024年 / 61卷 / 03期
基金：
欧盟地平线“2020”; 欧洲研究理事会;
关键词：
Orbit Determination; Astrodynamics; Optimal Control; Trajectory Optimization; Low Thrust Trajectory; Low-Thrust Maneuvers; Sequential Convex Programming; Convex Optimization; Spacecraft Guidance; Guidance; Navigation; and Control; POWERED-DESCENT GUIDANCE; PROPULSION; DESIGN; SYSTEM;
D O I：
10.2514/1.A35877
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
[No abstract available]
引用
收藏
页码：889 / 899
页数：11
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