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
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;
Conference_Titel :
Industrial Electronics and Applications (ICIEA), 2012 7th IEEE Conference on
Conference_Location :
Singapore
Print_ISBN :
978-1-4577-2118-2
DOI :
10.1109/ICIEA.2012.6360747
