DocumentCode :
3246452
Title :
Based on coupled modal arithmetic active control experimental study for space structures
Author :
Sheliang, Wang ; Binbin, Li ; Bo, Zhang
Author_Institution :
Coll. of Civil Eng., XAUAT, Xi´´an, China
fYear :
2011
fDate :
22-24 April 2011
Firstpage :
143
Lastpage :
146
Abstract :
When the system equation is transformed under mode frame of reference, the system of equations is coupled and shown by mode frame of reference. It is known as the method of modal space control Real-time control is achieved because of mode control force according to the control algorithm. The active control experiment is operated for the three layers truss space structure. Meanwhile the theory of coupled mode control and control algorithm are introduced, and the operating principle is stated. The optimal layout of piezoelectric derive bar is obtained according to Riccati equation. After processing and analyzing the experimental data by using the five-point moving average smoothing method, the result is shown that the efficiently active control can be greatly inhibitive effects. Meanwhile the corresponding modal damping co-efficiency can be improved in different degrees.
Keywords :
Riccati equations; aerospace components; aerospace control; force control; intelligent structures; piezoelectric materials; supports; Riccati equation; coupled modal arithmetic active control; five point moving average smoothing method; modal space control; mode control force; mode reference frame; piezoelectric derive bar; space structures; truss space structure; Acceleration; Actuators; Aerospace electronics; Damping; Equations; Force; Mathematical model; active control; coupled mode control; intelligence space structure; piezoelectric stack;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Electric Technology and Civil Engineering (ICETCE), 2011 International Conference on
Conference_Location :
Lushan
Print_ISBN :
978-1-4577-0289-1
Type :
conf
DOI :
10.1109/ICETCE.2011.5775729
Filename :
5775729
Link To Document :
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