Linearization methods for optimizing the low thrust spacecraft trajectory: Theoretical aspects

被引：4
|
作者：
Kazmerchuk, P. V. [1 ]
机构：
[1] Fed Enterprise Lavochkin Assoc, Chimki, Moscow Oblast, Russia
来源：
SOLAR SYSTEM RESEARCH | 2016年 / 50卷 / 07期
关键词：
low thrust; nonlinear optimization; compound dynamic system; OPTIMIZATION;
D O I：
10.1134/S003809461607008X
中图分类号：
P1 [天文学];
学科分类号：
0704 ;
摘要：
The theoretical aspects of the modified linearization method, which makes it possible to solve a wide class of nonlinear problems on optimizing low-thrust spacecraft trajectories (V. V. Efanov et al., 2009; V. V. Khartov et al., 2010) are examined. The main modifications of the linearization method are connected with its refinement for optimizing the main dynamic systems and design parameters of the spacecraft.
引用
收藏
页码：587 / 592
页数：6
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