火箭助飞鱼雷程序弹道自适应控制系统设计

Adaptive Controller System Design for Rocket-assisted Torpedo Program Trajectory

针对火箭助飞鱼雷空中段飞行过程中随机干扰大、动力学参数变化剧烈等特点,将自适应控制方法引入火箭助飞鱼雷空中段控制系统,并根据Narendra提出的只利用系统输入输出量的模型参考自适应控制理论设计了其自适应控制规律,仿真结果证明该控制系统能够克服动力学特性的变化并有较高的制导精度及较强的抗干扰能力。

Aiming to solve the great random interfere and acuity change of dynamics parameters when the Rocket-assisted Torpedo（RT） flight in the air,a design method of adaptive control for RT control system was introduced in this paper.The Model Reference Adaptive Control theory of using the import and export quantum which is brought forward by Narendra was applied in the RT control system.Computer simulation results demonstrate the effectiveness of the system for overcoming the change of dynamic characteristic.The system achieves the higher control and guide precision and better anti-jamming capability.