带落角约束的导弹制导与控制一体化设计

摘要

对带有落角约束的导弹制导与控制一体化设计进行了研究。首先建立了俯仰通道的制导与控制一体化模型，利用自适应RBF神经网络对干扰进行在线估计，运用反演递推方法和滑模控制的方法设计了控制器，并且分析了闭环系统的稳定性。数字仿真表明所设计的控制器满足导弹打击精度和落角限制要求。%In this paper, the problem of integrated design of missile＂ s guidance aria control wltn terminal angular constraint is discussed. Based on the integrated model in pitch plane, the adaptive RBF neural network sliding-mode controller is designed using the methods of stepback design and sliding-mode control, and the close loop system stability is analyzed. The numerical simulation results show that the controller meets the requirements of missile＇ s attacking precision and the limitation of terminal angular constraint.