Title :
Research on the controlling methods for rudder simulator based on PXI
Author :
Shi, Xianjun ; Lin, Huibo ; Liao, Jian
Author_Institution :
Dept. of Control Eng., Naval Aeronaut. & Astronaut. Univ., Yantai
Abstract :
Missile rudders are executive bodies of missile flight control system. All kinds of attitude motion of missile are depended on the actuator driver fins of rudder. The software designs of the electrical servo system are completed after the hard ware designs are presented in details. Then simulation and analyses of the servo system are carried out.
Keywords :
aerospace engineering; attitude control; missile control; servomechanisms; PXI; actuator driver; attitude motion; controlling methods; electrical servo system; missile flight control system; missile rudders; rudder simulator; software designs; Computational modeling; Computer interfaces; Computer simulation; Control engineering; Control systems; Missiles; Motion control; Position control; Servomechanisms; Servomotors;
Conference_Titel :
System Simulation and Scientific Computing, 2008. ICSC 2008. Asia Simulation Conference - 7th International Conference on
Conference_Location :
Beijing
Print_ISBN :
978-1-4244-1786-5
Electronic_ISBN :
978-1-4244-1787-2
DOI :
10.1109/ASC-ICSC.2008.4675430
