DocumentCode
3390752
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
fYear
2008
fDate
10-12 Oct. 2008
Firstpage
598
Lastpage
600
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;
fLanguage
English
Publisher
ieee
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
Type
conf
DOI
10.1109/ASC-ICSC.2008.4675430
Filename
4675430
Link To Document