摘要
首先介绍了一种仿射非线性系统的解耦控制方法 ,然后采用该方法为某机动飞机设计了解耦控制律 ,最后对所设计的飞机飞行控制系统进行了闭环仿真研究。仿真结果表明 ,所设计的控制系统具有良好的解耦性能 ,可以同时完成较精确的纵向和侧向机动 ,并且系统动静态品质良好。
An affine nonlinear system decoupling control method is presented. Using this method, a decoupling control law is designed for a large maneuverable aircraft. Finally, closed loop simulation research is performed for the designed flight control system. The results show that the system, which can accomplish longitudinal and lateral maneuvers simultaneously, not only has excellent decoupling performance, but also has better static and dynamic quality.
出处
《电光与控制》
2001年第4期30-34,共5页
Electronics Optics & Control
