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
来源：
XLIII ACADEMIC SPACE CONFERENCE, DEDICATED TO THE MEMORY OF ACADEMICIAN S P KOROLEV AND OTHER OUTSTANDING RUSSIAN SCIENTISTS - PIONEERS OF SPACE EXPLORATION | 2019年 / 2171卷
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
相关论文
共 50 条
[21]   Fast preliminary design of low-thrust trajectories for multi-asteroid exploration [J].
Fan, Zichen ;
Huo, Mingying ;
Qi, Naiming ;
Xu, Ye ;
Song, Zhiguo .
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 93
[22]   Artificial equilibrium points in binary asteroid systems with continuous low-thrust [J].
Bu, Shichao ;
Li, Shuang ;
Yang, Hongwei .
ASTROPHYSICS AND SPACE SCIENCE, 2017, 362 (08)
[23]   Low-Thrust Nonlinear Orbit Control for Very Low Lunar Orbits [J].
Leonardi, Edoardo Maria ;
Pontani, Mauro ;
Carletta, Stefano ;
Teofilatto, Paolo .
APPLIED SCIENCES-BASEL, 2024, 14 (05)
[24]   Optimal low-thrust trajectories to asteroids through an algorithm based on differential dynamic programming [J].
Colombo, Camilla ;
Vasile, Massimiliano ;
Radice, Gianmarco .
CELESTIAL MECHANICS & DYNAMICAL ASTRONOMY, 2009, 105 (1-3) :75-112
[25]   Nonlinear Earth orbit control using low-thrust propulsion [J].
Pontani, Mauro ;
Pustorino, Marco .
ACTA ASTRONAUTICA, 2021, 179 :296-310
[26]   Optimal strategy for low-thrust spiral trajectories using Lyapunov-based guidance [J].
Yang Dalin ;
Xu Bo ;
Gao Youtao .
ADVANCES IN SPACE RESEARCH, 2015, 56 (05) :865-878
[27]   Optimal combined impulsive/low-thrust trajectories for asteroid deflection via kinetic impact [J].
Conway, Bruce A. ;
Speziale, Alessia ;
Malagni, Ludovica .
ACTA ASTRONAUTICA, 2024, 220 :516-524
[28]   Automated Design of Propellant-Optimal, Low-Thrust Trajectories for Trojan Asteroid Tours [J].
Stuart, Jeffrey R. ;
Howell, Kathleen C. ;
Wilson, Roby S. .
JOURNAL OF SPACECRAFT AND ROCKETS, 2014, 51 (05) :1631-1647
[29]   A SURVEY OF THE METHODS AVAILABLE FOR THE DESIGN OF MANY-REVOLUTION LOW-THRUST PLANETOCENTRIC TRAJECTORIES [J].
Ghosh, Pradipto .
SPACEFLIGHT MECHANICS 2019, VOL 168, PTS I-IV, 2019, 168 :395-414
[30]   Loosely displaced formation-keeping control for satellite swarm with continuous low-thrust [J].
Zhao, Lin ;
Zhao, Kun ;
Li, Hui ;
Huang, Weiquan ;
Zhang, Xinyu ;
Zeng, Xiangxi .
INTERNATIONAL JOURNAL OF ADVANCED ROBOTIC SYSTEMS, 2020, 17 (05)
12345