为满足导弹编队协同作战中队形变换的需求,研究可实现队形拆分重构与领弹继任的队形控制器设计问题。以3枚导弹组成的楔形编队为研究对象,提出基于队形的编队飞行控制系统结构;建立导弹在惯性坐标系下的运动模型;从领弹和跟随弹的相对位置出发,设计基于自适应控制的队形控制器。仿真结果表明,该控制方法能够在领弹机动的前提下,在避障过程中实现编队队形拆分重构与领弹继任,具有较强的鲁棒性和稳定性,方法简单,易于实现。

To meet the requirement of formation transformation in missile coordinated combat, the problem of missile formation controller design to realize formation split, reconstruction and leader missile succession was studied. A wedge-shaped formation including three missiles was taken as study object, formation flying control system structure based on formation was proposed; the missile motion model in the inertial coordinate was established: According to the relative position between the leader and follower missiles, formation controller based on adaptive control was designed. Simulation results show the control method achieves formation split, reconstruction and leader missile succession in the process of obstacle avoidance under the premise of collar missile maneuver, and the method has strong robustness and stability, which is simple and easy to implement.