摘要
研究了推力矢量喷管、升力风扇以及气动舵面共同作用下 ASTOVL升力风扇飞机的飞控问题 ,采用非线性动态逆理论进行控制系统的设计。针对 ASTOVL升力风扇飞机的俯仰控制设计了动态逆控制律 ,并将所设计的控制律进行了仿真。结果表明 ,该方法能够满足控制系统性能的要求 ,具有工程应用前景。
A filght control problem about ASTOVL lift fan aircraft is developed where lift fan, thrust vector nozzles and aerodynamic control surfaces are used together. For pitch control the dynamic inverse control law is designed, then it is applied to the simulation. The results indicate that the method is efficient to control the system, so it provides an extensive prospect of engineering application.[KH4/5D]
出处
《南京航空航天大学学报》
CSCD
北大核心
2000年第5期504-509,共6页
Journal of Nanjing University of Aeronautics & Astronautics
关键词
短矩起落
ASTOVL升力风扇飞机
动态逆控制
thrust vector control
nonlinear dynamic inverse
pesudoinverse
lift fan
control law
