DocumentCode
578946
Title
Design of TV-guided system based on control loop of rudder pitch attitude
Author
Wang, Xin ; Yao, Jun ; Qiao, Xiangxin
Author_Institution
Shenyang Ligong Univ., Shenyang, China
fYear
2012
fDate
18-20 July 2012
Firstpage
334
Lastpage
337
Abstract
TV-guided system model is difficult to establish and the parameters are not easy to calculate. This paper uses the missile kinematics equations to simplify the transfer function of actuator systematic in the dynamic equations. The guidance system is designed based on three-point guidance law and the model of TV-guided system is established using Simulink. The simulation analysis shows that the simplified controller can improve system´s rapidity, veracity and stability.
Keywords
actuators; attitude control; control engineering computing; digital simulation; military computing; missile guidance; television equipment; transfer functions; Simulink; TV-guided system design; actuator systematic; dynamic equations; missile kinematics equations; rudder pitch attitude control loop; three-point guidance law; transfer function; Attitude control; Control systems; Mathematical model; Missiles; TV; Target tracking; Transfer functions; TV-guided; actuator systematic; guidance law;
fLanguage
English
Publisher
ieee
Conference_Titel
Industrial Electronics and Applications (ICIEA), 2012 7th IEEE Conference on
Conference_Location
Singapore
Print_ISBN
978-1-4577-2118-2
Type
conf
DOI
10.1109/ICIEA.2012.6360747
Filename
6360747
Link To Document