摘要
小型飞行器独特的气动外形、复杂的作战使命对飞行控制系统提出了苛刻的要求。近年来,动态逆控制方法在工程界获得了普遍应用,并成功用于多种飞行器的控制系统设计中。文中就动态逆方法作了论述。研究了应用动态逆控制方法的设计途径。分析了用于神经网络动态逆控制的几种神经网络模型,提出了用于小型飞行器的动态逆控制方案。最后,指出了未来飞行控制系统动态逆设计的发展方向。
The aerodynamic shape and complicated battle task of the miniature aircraft request good capability for control system. In recent years, the method of control with dynamic inversion has been widely applied in the engineering field. Many aircraft control systems have been designed successfully by the method. The method of Control with dynamic inversion was discussed. How to apply this method was researched. Some models of neural network used in dynamic inversion were analyzed. The architecture of control system with dynamic inversion of the miniature aircraft was developed. At last, the developing direction for designing flight control system with dynamic inversion in the future was forecast.
出处
《弹箭与制导学报》
CSCD
北大核心
2008年第3期1-4,共4页
Journal of Projectiles,Rockets,Missiles and Guidance
基金
总装预研基金资助
关键词
飞行器
飞行控制
神经网络
动态逆
aircraft
flight control
neural network
dynamic inversion
