Angle penetration attack ability plays a more and more important role for missiles in modern warfare, and the traditional separate guidance and control system design problem is the key to restrict the improvement of time-sensitive attack and cooperative attack ability of multimissiles. Firstly, the deviation control strategy of line-of-sight angle and attack angle is put forward in this paper, and the integrated guidance and control system model with impact angle constraint is established, according to the characteristics of angle penetration attack. Then, an integrated guidance and control controller for angle penetration attack is designed by using adaptive dynamic surface control, with the dynamic constraints, nonlinear input saturation, and terminal line-of-sight and attack angle constraints concerned. In order to ensure the robustness of the system, nonlinear disturbance observers are introduced to estimate the uncertainty of the system model. Finally, the stability of the integrated design method is proven based on the Lyapunov theory. Simulation results verify the effectiveness of the integrated guidance and control design method proposed in this paper in multimissile angle penetration attack.

中文翻译：

---

多导弹角侵彻攻击鲁棒综合制导控制设计

角度突防攻击能力对导弹在现代战争中的作用越来越重要，而传统的分离制导和控制系统设计问题是制约多导弹时敏攻击和协同攻击能力提高的关键。首先，针对角突突攻击的特点，提出了视距角和攻角偏差控制策略，并建立了具有冲击角约束的综合制导控制系统模型。然后，结合动态约束、非线性输入饱和、末端视距和攻角约束，采用自适应动态面控制设计了角突攻击综合制导控制控制器。为了保证系统的鲁棒性，引入了非线性扰动观测器来估计系统模型的不确定性。最后，基于李雅普诺夫理论证明了集成设计方法的稳定性。仿真结果验证了本文提出的综合制导与控制设计方法在多导弹角度突防攻击中的有效性。