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航天器轨道追逃动力学与控制问题研究综述
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作者 朱彦伟 张乘铭 +1 位作者 杨傅云翔 杨乐平 《国防科技大学学报》 EI CAS CSCD 北大核心 2024年第3期1-11,共11页
随着航天器交会与接近操作技术的快速发展,轨道追逃问题逐渐成为航天领域的研究热点。从动力学与控制视角,对航天器轨道追逃问题的研究现状进行综述。给出了基于定量微分对策的轨道追逃问题模型的一般形式,系统梳理了各种类型的轨道追... 随着航天器交会与接近操作技术的快速发展,轨道追逃问题逐渐成为航天领域的研究热点。从动力学与控制视角,对航天器轨道追逃问题的研究现状进行综述。给出了基于定量微分对策的轨道追逃问题模型的一般形式,系统梳理了各种类型的轨道追逃问题;对于追逃策略求解,分别针对闭环策略和开环策略,分析了各种方法的优缺点;围绕人工智能算法与轨道追逃问题的结合,阐述了基于深度神经网络和强化学习的轨道追逃策略的研究现状。关于未来展望,提出了追逃博弈态势分析、多航天器博弈控制、三体条件下博弈动力学与控制等发展方向。 展开更多
关键词 航天器追逃博弈 微分对策 深度神经网络 强化学习
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航天器轨道追逃态势分析的水平集方法
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作者 杨傅云翔 杨乐平 +1 位作者 朱彦伟 张乘铭 《国防科技大学学报》 EI CAS CSCD 北大核心 2024年第3期30-38,共9页
航天器轨道追逃是当前航天动力学与控制领域的研究热点。针对轨道追逃定性问题开展研究,提出了一种综合运用降维动力学模型和后向可达集的航天器近距离轨道追逃态势分析方法,以支撑任务可行性分析;通过在视线旋转坐标系下推导博弈系统... 航天器轨道追逃是当前航天动力学与控制领域的研究热点。针对轨道追逃定性问题开展研究,提出了一种综合运用降维动力学模型和后向可达集的航天器近距离轨道追逃态势分析方法,以支撑任务可行性分析;通过在视线旋转坐标系下推导博弈系统降维动力学模型,建立近距离追逃定性问题模型,减少了状态空间维度;使用目标集的后向可达集描述捕获区并划分追逃状态空间,基于水平集方法建立可达集在降维动力学模型中演化的动态HJI(Hamilton-Jacobi-Isaacs)偏微分方程,并设计WENO-TVD求解器数值计算HJI方程终值问题粘性解,完成了追逃目标集的准确描述并避免了可能出现的终端奇异现象。通过不同推力构型的追逃场景数值仿真验证了方法的有效性,展现了一次计算批量化处理初始态势的功能。 展开更多
关键词 航天器追逃博弈 可行性分析 水平集方法
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An AutoML based trajectory optimization method for long-distance spacecraft pursuit-evasion game
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作者 yang fuyunxiang yang Leping ZHU Yanwei 《Journal of Systems Engineering and Electronics》 SCIE EI CSCD 2023年第3期754-765,共12页
Current successes in artificial intelligence domain have revitalized interest in spacecraft pursuit-evasion game,which is an interception problem with a non-cooperative maneuvering target.The paper presents an automat... Current successes in artificial intelligence domain have revitalized interest in spacecraft pursuit-evasion game,which is an interception problem with a non-cooperative maneuvering target.The paper presents an automated machine learning(AutoML)based method to generate optimal trajectories in long-distance scenarios.Compared with conventional deep neural network(DNN)methods,the proposed method dramatically reduces the reliance on manual intervention and machine learning expertise.Firstly,based on differential game theory and costate normalization technique,the trajectory optimization problem is formulated under the assumption of continuous thrust.Secondly,the AutoML technique based on sequential model-based optimization(SMBO)framework is introduced to automate DNN design in deep learning process.If recommended DNN architecture exists,the tree-structured Parzen estimator(TPE)is used,otherwise the efficient neural architecture search(NAS)with network morphism is used.Thus,a novel trajectory optimization method with high computational efficiency is achieved.Finally,numerical results demonstrate the feasibility and efficiency of the proposed method. 展开更多
关键词 PURSUIT-EVASION different game trajectory optimization automated machine learning(AutoML)
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A DNN based trajectory optimization method for intercepting non-cooperative maneuvering spacecraft 被引量:4
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作者 yang fuyunxiang yang Leping +1 位作者 ZHU Yanwei ZENG Xin 《Journal of Systems Engineering and Electronics》 SCIE EI CSCD 2022年第2期438-446,共9页
Current successes in artificial intelligence domain have revitalized interest in neural networks and demonstrated their potential in solving spacecraft trajectory optimization problems. This paper presents a data-free... Current successes in artificial intelligence domain have revitalized interest in neural networks and demonstrated their potential in solving spacecraft trajectory optimization problems. This paper presents a data-free deep neural network(DNN) based trajectory optimization method for intercepting noncooperative maneuvering spacecraft, in a continuous low-thrust scenario. Firstly, the problem is formulated as a standard constrained optimization problem through differential game theory and minimax principle. Secondly, a new DNN is designed to integrate interception dynamic model into the network and involve it in the process of gradient descent, which makes the network endowed with the knowledge of physical constraints and reduces the learning burden of the network. Thus, a DNN based method is proposed, which completely eliminates the demand of training datasets and improves the generalization capacity. Finally, numerical results demonstrate the feasibility and efficiency of our proposed method. 展开更多
关键词 non-cooperative maneuvering spacecraft neural network differential game trajectory optimization
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