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
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
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页码:900 / 907
页数:8
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