摘要
文中主要是根据建立的飞机小扰动线性化方程,利用经典控制理论中的根轨迹法,分析设计了某无人机飞行控制系统中纵向运动的两个通道:俯仰通道和高度通道的控制律,并利用Matlab进行了数字仿真,给出了仿真结果。
This paper is mainly according to the plane＇s little perturbation linearization equations, using the root locus method of the classical control theory to analyse and design a UAV＇s（unmaned air vehicles） flight control system. The pitching ,altitude holding channels＇ control laws of the portrait control system are designed with the root locus method. Digital simulation is carried out in Matlab environment.
出处
《弹箭与制导学报》
CSCD
北大核心
2007年第2期91-93,共3页
Journal of Projectiles,Rockets,Missiles and Guidance
关键词
飞行控制
控制律
数字仿真
flight control
control law
digital simulation
