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

页码：900 / 907

页数：8