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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。
The flight control of ASTOVL lift fan with thrust vector nozzle, lift fan and air-driven rudder is studied. The nonlinear dynamic inverse theory is used to design the control system. Aiming at the pitch control of ASTOVL lift fan aircraft, a dynamic inverse control law is designed and the designed control law is simulated. The results show that this method can meet the requirements of control system performance and has the prospect of engineering application.