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对于非接触环状电磁稳定型航天器的初始合作对齐控制
Haoxiang Yuan1, He Liao1, Yuantian Qin1
1Institute of Astronautics, Nanjing University of Aeronautics and Astronautics, Nanjing 211106, China.
ISA transactions
|November 11, 2025
概括
这项研究引入了一种用于非接触式航天器对齐的新控制方法,确保避免碰撞和快速稳定,即使初始角度和速度很大. 先进的算法使预测控制能够实现更安全的轨道操作.
科学领域:
- 航空航天工程 航空航天工程
- 控制系统理论 控制系统理论
- 机器人技术 机器人技术 机器人技术
背景情况:
- 无接触环形电磁稳定航天器 (NCAESS) 提供了改进的姿态控制.
- 在模块在太空释放期间,初始对齐控制是一个关键的挑战.
- 传统的方法仅限于小的初始角度和速度.
研究的目的:
- 为NCAESS提出一个合作性调整控制方法.
- 在初始对齐过程中解决避免碰撞和快速稳定问题.
- 为了处理具有挑战性的释放状态,具有大角度和角速度.
主要方法:
- 制定了一个由两个模块组成的合作调整控制战略.
- 使用非线性干扰拒绝模型预测控制 (NDRMPC) 算法.
- 未来状态轨迹预测和规划是为了避免碰撞而集成的.
主要成果:
- 提出的方法有效地处理四个释放状态,具有很大的角度和速度.
- 模拟成功地证明了模块之间避免碰撞.
- 实现了快速的非对称收和精确的预测控制.
结论:
- 基于NDRMPC的方法有效地解决了NCAESS的初始对齐控制问题.
- 这种方法通过保证避免碰撞来确保安全.
- 该方法增强了具有挑战性的释放条件的航天器的操作能力.
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