导弹三维轨迹跟踪的最佳指导规律设计基于固定增益干扰观察员的三维轨迹跟踪
Ke Zhang1, Zhenlin Zhang1, Zhiguo Han1
1School of Astronautics, Northwestern Polytechnical University, Xi'an 710072, China.
ISA transactions
|October 13, 2023
概括
一项新的最佳干扰拒绝指导法 (ODRGL) 有效地跟踪导弹轨迹,尽管速度和干扰无法控制. 这种方法提高了系统稳定性和3D空间中的能量优化.
科学领域:
- 导弹指导和控制系统是导弹的指导和控制系统.
- 航空航天工程是航空航天工程.
- 非线性控制理论非线性控制理论
背景情况:
- 轨迹跟踪是导弹指导的一个关键挑战.
- 无法控制的速度和外部干扰 (风,建模错误) 复杂化了指导规律的设计.
- 现有的方法可能无法充分解决3D空间中的联合不确定性.
研究的目的:
- 提出一个新的三维最佳干扰排斥指导法 (ODRGL).
- 为了解决不可控制速度的导弹的轨迹跟踪问题.
- 为了有效地拒绝风和建模错误等干扰.
主要方法:
- 开发曲率和曲率通道的错误模型,包括曲率通道的建模错误.
- 基于分离定理的控制器和观察者的设计.
- 关于固定增益干扰观察员 (FGDO) 的建议,用于干扰估计和前补偿.
- 使用微分几何线性化理论进行名义错误模型的线性化.
- 对于线性化模型的线性二次调节器 (LQR) 控制器的设计.
主要成果:
- 拟议的ODRGL在干扰下成功稳定了非线性导弹系统.
- 指导法确保在轨迹跟踪过程中优化能源.
- 模拟结果验证了对风力干扰和建模错误的有效性.
- 机关准确地估计和补偿干扰.
结论:
- 开发的ODRGL为3D导弹轨迹跟踪提供了强大的解决方案.
- 集成FGDO和LQR控制器提高了指导性能.
- 该方法有效地处理系统的非线性和外部不确定性.
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