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