单通道旋转弹一体化制导控制系统设计

Design of Integrated Guidance and Control for a Spinning Missile with one Pair of Canards

采用一对鸭舵同时完成俯仰和偏航通道的一体化控制,避免了传统设计方法的不稳定性。以一类单通道旋转弹为研究对象,在其运动模型的基础上,设计一体化反演滑模制导控制系统并进行了数值仿真验证,证明了一体化反演滑模制导控制系统的有效性。

This paper adopts one pair of duck rudders accomplishes control of pitching and jaw channel effective to avoid the inherent instability of traditional system. This paper takes a kind of single-channel controlled spinning＇ missile as research object. The simulation of integrated back-stepping sliding mode guidance control system is designed and verified by numerical simulation on the basis of it＇ s pitching motion model. The results verify the effectiveness of the integrated back-stepping sliding mode guidance control system.