飞机γ角姿态控制系统方案设计及仿真

Design and Simulation of Aero γ Angle Attitude Control System

摘要:

在简要分析飞机侧向控制系统运动模态基础上,对飞机? 角姿态控制系统结构方案进行设计并进行仿真验证。仿真结果显示,所设计的飞机? 角姿态控制系统结构方案及其控制规律具有良好抗干扰能力,是合理有效的,从而提出对飞行状态变化剧烈的飞机,应采用控制规律调参措施。

Abstract:

On the basis of synopsis analysis airplane the sport molds of the lateral side control system, the structure control project of aero angle attitude control system was designed and verified by simulation was done. Simulation results show that designed aero angle attitude control system structure project and it's control law had good anti-interference ability, and were feasible. Lastly, it was put forward the control law should adopt adjusting parameters measures with flying state violent variety airplane.