Eclipse-Conscious Low-Thrust Trajectory Optimization Using Pseudospectral Methods and Control Smoothing Techniques

被引：0
|
作者：
Sowell, Samuel [1 ]
Taheri, Ehsan [1 ]
机构：
[1] Auburn Univ, Dept Aerosp Engn, Auburn, AL 36849 USA
来源：
JOURNAL OF SPACECRAFT AND ROCKETS | 2024年 / 61卷 / 03期
关键词：
Astronomical Events; Pontryagin's Minimum Principle; Pseudospectral Methods; Geostationary Transfer Orbit; Planets; Earth Centered Inertial; Satellite Constellations; Propulsion and Power; Adaptive Mesh Refinement; Boundary Element Method; MESH REFINEMENT METHOD; MINIMUM-TIME; SATELLITE FORMATION; COSTATE ESTIMATION; ORBIT TRANSFERS; EARTH; FUEL; DESIGN;
D O I：
10.2514/1.A35789
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：900 / 907
页数：8
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