基于迎角恒定的进场功率补偿控制律研究

The research of approach power compensation control law with the attack of angle regulator

主要论述了舰载机速度恒定和迎角恒定两种进场功率补偿系统的基本原理,并对其控制律进行研究设计,通过Matlab/Simulink分别进行仿真得到航迹角对俯仰角的时域动态响应曲线,并分析比较,说明了迎角恒定的进场功率补偿系统比速度恒定的进场功率补偿系统具有更好的操纵性和轨迹跟踪性能。在实际面向工程应用时,更加易于设计,且符合舰载机的发展要求。

This paper mainly discusses the rational of the aircraft approach power compensation system with the speed regulator and with the attack of angle regulator,and designed the approach power compensation control law.The dynamic response of track angle to pitch angle is simulated,analyzed and compared,which indicates that approach power compensation system with the attack of angle regulator has better control performance and track response performance,and is easier to design for development request of aircraft.