# 基于微分对策的航天器轨道追逃最优控制策略

**Repository Path**: hai_zhu/master_thesis_code

## Basic Information

- **Project Name**: 基于微分对策的航天器轨道追逃最优控制策略
- **Description**: 硕士学位论文《基于微分对策的航天器轨道追逃最优控制策略》相关源代码
- **Primary Language**: Matlab
- **License**: GPL-3.0
- **Default Branch**: master
- **Homepage**: None
- **GVP Project**: No

## Statistics

- **Stars**: 9
- **Forks**: 1
- **Created**: 2022-04-22
- **Last Updated**: 2025-06-25

## Categories & Tags

**Categories**: Uncategorized

**Tags**: None

## README

# 基于微分对策的航天器轨道追逃最优控制策略

#### 介绍
硕士学位论文[《基于微分对策的航天器轨道追逃最优控制策略》](https://cdmd.cnki.com.cn/Article/CDMD-91002-1020701376.htm)相关源代码，包含论文第三、四、五章的程序源码、图片原图和一些原始数据。

#### 使用说明
程序均使用MATLAB编写，如果您在研究中使用到相关代码，请引用我们的相关工作，谢谢！

```
@mastersthesis{Zhu2017Thesis,
  title={基于微分对策的航天器轨道追逃最优控制策略},
  author={祝海},
  school={国防科学技术大学},
  year={2017}
}

@article{Luo2020Survey,
  title={航天器轨道追逃微分对策研究综述},
  author={罗亚中 and 李振瑜 and 祝海},
  journal={中国科学：技术科学},
  volume={50},
  number={12},
  pages={1533--1545},
  year={2020}
}

@article{Li2019Acta,
    author = {Zhen-yu Li and Hai Zhu and Zhen Yang and Ya-zhong Luo},
    title = {A dimension-reduction solution of free-time differential games for spacecraft pursuit-evasion},
    journal = {Acta Astronautica},
    volume = {163},
    pages = {201-210},
    year = {2019}    
}

@article{Li2020JGCD,
    author = {Zhen-yu Li and Hai Zhu and Zhen Yang and Ya-zhong Luo},
    title = {Saddle point of orbital pursuit-evasion game under J2-perturbed dynamics},
    journal = {Journal of Guidance, Control, and Dynamics},
    volume = {43},
    number = {9},
    pages = {1733-1739},
    year = {2020}
}

@article{Li2021SCTS,
    author = {Zhen-yu Li and Hai Zhu and Ya-zhong Luo},
    title = {An escape strategy in orbital pursuit-evasion games with incomplete information},
    journal = {Science China Technological Sciences },
    volume = {64},
    pages = {559-570},
    year = {2021}
}
```