海军航空工程学院学报2012，Vol.27Issue(2)：138-142,5.
基于升降舵控制的飞机飞行速度控制系统仿真
Simulation Researches on Aero Airspeed Control System Based on Elevator Control
摘要
Abstract
For assurance airplane to land（or to warship） at request accuracy,it is very important for airspeed control system to have good control capability.Firstly,main function of airspeed control system was brief analyzed,and a few kinds structure schemes of airspeed control system were brief introduced.Secondly,airspeed control system structure principle diagram based on elevator bottom control and Simulink structure diagram were established.Using simulation method,simulation researches on the inside and outside control loops of the speed control system were done.Finally transmission ratio with good control performance corresponded speed control system was obtained.Simulation results showed that the designed control scheme of the airplane airspeed control system based on elevator control and the control laws were reasonable and feasible and good control performance.关键词
飞行速度控制/升降舵控制/传动比/仿真Key words
aero airspeed control/elevator bottom control/transmission ratio/simulation分类
航空航天引用本文复制引用
曲东才,曹栋,刘爱元,杨晓龙..基于升降舵控制的飞机飞行速度控制系统仿真[J].海军航空工程学院学报,2012,27(2):138-142,5.基金项目
国家自然科学基金资助项目 （）
