DocumentCode
2734950
Title
The LDCM actuator for vibration suppression
Author
Ide, Eric N. ; Lindner, Douglas K.
Author_Institution
Bradley Dept. of Electr. Eng., Virginia Polytech. Inst., Blacksburg, VA, USA
fYear
1988
fDate
0-0 1988
Firstpage
667
Lastpage
670
Abstract
A linear DC motor (LDCM) has been proposed as an actuator for the COFS I Mast and the COFS program ground test Mini-Mast. The basic principles of operation of the LDCM as an actuator for vibration suppression in large flexible structures are reviewed. Because of force and stroke limitations, control loops are required to stabilize the actuator, which results in a nonstandard actuator-plant configuration. A simulation model that includes LDCM actuator control loops and a definite-element model of the Mast is described, with simulation results showing the excitation capability of the actuator.<>
Keywords
DC motors; aerospace control; electric actuators; vibration control; COFS I Mast; Mini-Mast; aerospace control; control loops; electric actuator; large flexible structures; linear DC motor; simulation model; vibration suppression; Coils; DC motors; Equations; Finite element methods; Flexible structures; Force control; Frequency; Hydraulic actuators; Position measurement; Testing;
fLanguage
English
Publisher
ieee
Conference_Titel
System Theory, 1988., Proceedings of the Twentieth Southeastern Symposium on
Conference_Location
Charlotte, NC, USA
ISSN
0094-2898
Print_ISBN
0-8186-0847-1
Type
conf
DOI
10.1109/SSST.1988.17132
Filename
17132
Link To Document