基于非线性动态逆的飞机控制规律仿真

Design and simulation of aircraft control law based on the nonlinear dynamic inversion

介绍了采用非线性动态逆方法对常规飞机的各回路进行的控制规律解算,并以某型飞机为模型进行仿真,结果表明,该控制规律解算能提供精确的纵向和横向控制,具有良好的指令跟踪性能.

Nonlinear dynamic inversion methods are adopted to design control law of each loop for general aircraft. And taking a fighter plane for example, simulation according to relevant theory is accomplished. The result shows that this law has a good performance of command tracing.