DocumentCode
2271473
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
fYear
2015
fDate
28-30 July 2015
Firstpage
8760
Lastpage
8763
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;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Conference (CCC), 2015 34th Chinese
Conference_Location
Hangzhou, China
Type
conf
DOI
10.1109/ChiCC.2015.7261023
Filename
7261023
Link To Document