Artificial Neural Networks for Control and Propagation of Low-Thrust Trajectories

被引:0
|
作者
Sorokin, A. V. [1 ]
Shirobokov, M. G. [2 ]
Trofimov, S. P. [2 ]
机构
[1] Moscow Inst Phys & Technol, Moscow, Russia
[2] Keldysh Inst Appl Math, Moscow, Russia
基金
俄罗斯基础研究基金会;
关键词
OPTIMIZATION; SPACECRAFT;
D O I
10.1063/1.5133368
中图分类号
P1 [天文学];
学科分类号
0704 ;
摘要
The work is devoted to the design of artificial neural networks which can be used for the orbital control of a spacecraft equipped with a low-thrust engine. The problem of energy-optimal transfer between two points is considered. Two neural networks are constructed: the predictive one and the controlling one. Their architecture, learning algorithms, and the performance in the presence of unaccounted disturbances are given.
引用
收藏
页数:7
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