Title :
On aero glide downwards beam guidance control system
Author :
Qu, Dongcai ; Pingyuan, Ma ; Shi, Xianjun
Author_Institution :
Department of Control Engineering Naval Aeronautical and Astronautical University, Yantai, Shandong, China, 264001
Abstract :
The aero glide downwards beam guidance control system is an important control system. Based on the basic work principle been brief discussed, kinematic link and glide coupler in the glide downwards beam guidance control system were analyzed. The aero glide downwards beam guidance system structure was designed, and a great deal of simulation researches was done under MATLAB platform. Simulation results manifestation: the designed structure for aero glide downwards beam guidance control system is reasonable and stability, and its steady state performance was also gotten better.
Keywords :
Aerospace control; Aircraft; Control systems; Couplers; Kinematics; MATLAB; Mathematical model; Beam Deviation Angle; Coupler; Glide Downwards Beam Guidance Control; Transmission Ratio;
Conference_Titel :
Control Conference (CCC), 2015 34th Chinese
Conference_Location :
Hangzhou, China
DOI :
10.1109/ChiCC.2015.7261023
