碟形飞行器李雅普诺夫优化控制器设计

Design of Controllers for Flying Saucer Based on Lyapunov Optimization

针对一类简单控制器实现的碟形飞行器变质量矩/推力矢量复合控制系统,通过转换,建立了关联控制系统,并基于李雅普诺夫优化设计方法,对碟形飞行器的控制器进行了设计。最后,将此控制方法应用于碟形飞行器全弹道飞行试验进行仿真。仿真研究表明,与传统的静态控制器设计方法相比,这种方法显示了巨大的优越性。

For moving-mass/thrust-vectoring compound control over a flying saucer based on simple controllers, a model of interconnected control system is established by transition, and based on the designing method of Lyapunov optimization, the controllers of the flying saucer are designed. Finally, the control method is used to the simulation of the flying saucer＇ s full trajectory flying examination, and the result shows that, compared to the designing method of conventional static-state controllers, this method shows great advantages.