具有多输入和扰动作用的空空导弹滚动通道的前馈/反馈自适应控制器

中程空空导弹的参数处于激烈、大范围的时变中，采用古典控制器很难满足不同高度弹道的性能规范。为了使导弹在飞行高度和速度大范围变化时均能保持优良性能，采用数字自适应控制方法是合适的。本文提出了一种基于超稳定性理论的飞行控制系统方案，其性能明显优于不采用自适应控制器的古典系统。

FEEDFORWARD AND FEEDBACK ADAPTIVE CONTROLLER FOR ROLLING CHANNEL OF AIR-TO-AIR MISSILE WITH MULTI-INPUT AND DISTURBANCES

The parameters of midcourse air-air missile is very widely and significantly.It is diffcult to satisfy performance specifications for different altitudes trajetories using pure classical controller. However, to maintain good performance over a wide range of the altitudes and speeds of the missile,digital adaptive control methods may prove suitable.Adaptive flight control system schemes based on hyperstability theory are presented in this paper, the new schemes performance is superior to that without adaptive controller.