DocumentCode :
871445
Title :
Electrostatic suspension system with sliding mode control
Author :
Yang, W.Q. ; Zhang, Y.S.
Author_Institution :
Dept. of Precision Instrum., Tsinghua Univ., Beijing, China
Volume :
28
Issue :
2
fYear :
1992
fDate :
4/1/1992 12:00:00 AM
Firstpage :
605
Lastpage :
609
Abstract :
Two aspects must be considered in selecting the preload of electrostatic suspension system (ESS) for the electrostatic gyroscope (ESG), both the required load capacity and the tolerable electrical disturbing torques exerted on the rotor. By means of sliding mode control (SMC), ESS may operate in three modes: (1) two-sided linear suspension (2) single-sided nonlinear suspension, and (3) single-sided suspension with nonlinearity compensation. Therefore a low preload can be selected for reducing both the electrical disturbing torques and the power consumption, meanwhile ensuring the required load capacity. It has been proven by experiments that the ESS with 2 g preload can bear overload acceleration up to 6 g successfully
Keywords :
aerospace instrumentation; electrostatic devices; gyroscopes; variable structure systems; electrical disturbing torques; electrostatic gyroscope; electrostatic suspension; flight control; load capacity; nonlinearity compensation; overload acceleration; power consumption; preload; rotor; single-sided nonlinear suspension; sliding mode control; two-sided linear suspension; Acceleration; Circuits; Electrodes; Electronic switching systems; Electrostatics; Force control; Force measurement; Sliding mode control; Variable structure systems; Voltage control;
fLanguage :
English
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9251
Type :
jour
DOI :
10.1109/7.144586
Filename :
144586
Link To Document :
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