DocumentCode :
3514257
Title :
Simulation research of MIMO vibration control in aircraft store test
Author :
Wang, Guanglu ; Xu, Ming
Author_Institution :
CAPE, Beijing, China
fYear :
2009
fDate :
20-24 July 2009
Firstpage :
339
Lastpage :
344
Abstract :
The paper expounds the main content of simulation of multiple-input-multi-output (MIMO) vibration which includes the purpose, the model and the procedure. The simulation technology has been used to some aircraft store reliability qualification test. Many control projects were simulated. According to the simulation result, the best control project was ensured. According to the best control project, some store reliability qualification test was successfully finished.
Keywords :
MIMO systems; aircraft control; aircraft testing; optimal control; reliability; vibration control; MIMO vibration control; aircraft store reliability qualification test; multiple-input-multi-output vibration; optimal control project simulation technology; Acceleration; Aerospace control; Aircraft; MIMO; Missiles; Open loop systems; Optimal control; Qualifications; Testing; Vibration control; MIMO; limit control; response control; simulation; store;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Reliability, Maintainability and Safety, 2009. ICRMS 2009. 8th International Conference on
Conference_Location :
Chengdu
Print_ISBN :
978-1-4244-4903-3
Electronic_ISBN :
978-1-4244-4905-7
Type :
conf
DOI :
10.1109/ICRMS.2009.5270177
Filename :
5270177
Link To Document :
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