基于配置文件跟踪的增强变化后退指导法用于操作目标拦截与输入和的目标拦截
Jingliang Sun1, Mengmeng Wang2, Zihan Wang2
1School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China; Key Laboratory of Dynamics and Control of Flight Vehicle, Ministry of Education, Beijing 100081, China; Beijing Institute of Technology Chongqing Innovation Center, Chongqing 401135, China.
ISA transactions
|November 18, 2025
概括
这项研究引入了导弹拦截机动目标的新型指导法则,即使在系统限制的情况下,也确保了精确的撞击角度. 开发的方法提供了有效的轨迹控制和保证的稳定性.
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:
- 导航系统面临的挑战是机动目标和输入和.
- 实现精确的撞击角度控制对于拦截效率至关重要.
研究的目的:
- 制定一个基于个人资料跟踪的,收益变化的倒退指导法.
- 为了解决与输入和的机动目标的冲击角限制.
主要方法:
- 制定了一个基于距离跨度的多项式函数,用于参考视线角度配置.
- 开发了一个收益变化的有限时间受约束的倒退指导法.
- 设计了一个基于跟踪错误的可变增益来抵制目标机动.
主要成果:
- 可以在没有数值优化的情况下通过分析来确定参考配置文件.
- 拟议的指导法有效地追踪了设计的个人资料.
- 建立了封闭循环系统稳定的理论保证.
结论:
- 开发的指导法对受到冲击角度限制的指导有效.
- 对比模拟证实了该方法对现有方法的优势.
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