DocumentCode
2254876
Title
Three dimensional motions control simulation for radial in vertical-type PM LSM rocket launcher
Author
Yoshida, Kinjiro ; Cao, Yi
Author_Institution
Dept. of Electr. & Electron. Syst. Eng., Kyushu Univ., Fukuoka, Japan
Volume
2
fYear
2004
fDate
14-16 Aug. 2004
Firstpage
761
Abstract
In our previous papers, we proposed a vertical-type permanent magnet (PM) linear synchronous motor (LSM) rocket launcher system of which four acceleration guide-ways with armature-windings are arranged symmetrically along a shaft of about 3.8 m. We analyzed the characteristics of propulsion, levitation and guidance forces of PM LSM in the derived vertical-type PM LSM rocket launcher system by using two-dimensional interpolation method. This paper presents the three dimensional motions control simulation for radial displacements in vertical-type PM LSM rocket launcher. We derived the three dimensional motions equation of launcher and simulated three dimensional motions control of launcher when it starts with radial displacements. The stability of three dimensional motions control and the effectiveness of two-dimensional interpolation method have been verified numerically by the simulation results.
Keywords
aerospace propulsion; interpolation; linear synchronous motors; machine control; motion control; permanent magnet motors; rockets; stability; three-term control; PID control method; armature-winding; guidance forces characteristic; levitation characteristic; permanent magnet linear synchronous motor rocket launcher; propulsion characteristic; radial displacement; three dimensional motions control simulation; two-dimensional interpolation method;
fLanguage
English
Publisher
ieee
Conference_Titel
Power Electronics and Motion Control Conference, 2004. IPEMC 2004. The 4th International
Conference_Location
Xi´an
Print_ISBN
7-5605-1869-9
Type
conf
Filename
1375812
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