航天器
运动规划
强化学习
计算机科学
过程(计算)
随机树
控制理论(社会学)
人工智能
航空航天工程
工程类
控制(管理)
机器人
操作系统
作者
Shulei Jiang,Fanyu Zhao,Y Chen,Zhonghe Jin
标识
DOI:10.1109/iccsse59359.2023.10245260
摘要
During the execution process of the spacecraft mission, a large number of attitude maneuvers are required. When the external environment and the spacecraft's dynamic constraints are coupled, it will cause certain difficulties in solving the spacecraft's attitude maneuver path planning. Therefore, the spacecraft attitude maneuver planning must be improved. However, traditional methods often have the problems of low solution efficiency and strong model dependence. We propose the Deep Q-network (DQN) method to solve these problems and directly perform end-to-end inference. Finally, by comparing with the Rapid-exploration Random Tree (RRT) algorithm, the results show that the planning results meet all constraints and energy consumption of the DQN method is reduced by about 62% compared to the RRT method, and the planning time is also reduced by about 81 %.
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