DocumentCode
1866593
Title
On-line robust aeroservoelastic stability margin analysis from wavelet-processed flight testing data
Author
Li, Hongchao ; Shi, Zhongke ; Tang, Wei
Author_Institution
Coll. of Autom., Northwestern Polytech. Univ., Xi´´an
fYear
2006
fDate
19-21 Jan. 2006
Lastpage
757
Abstract
An on-line method based on robust mu analysis is presented to evaluate the stability margin of multi-loop aeroservoelastic system from flight testing data. The flight data is preprocessed to remove noise by wavelet filter in time-frequency domain. The method for stability analysis is described and the classical stability margin used for single-input-single-output (SISO) system has been extended to multi-loop system. With the present definition for uncertainty, the guaranteed bounds on gain and phase margin can been calculated for a specified mu value. A nonparametric identification is applied to determine the open-loop transfer function from testing data. This method enables us to implement on-line stability evaluation without theory model. Finally, the analysis results are compared with return difference matrix method to illustrate the efficiency of the new method
Keywords
aerospace control; aerospace testing; identification; multivariable control systems; robust control; time-frequency analysis; transfer functions; wavelet transforms; SISO system; aeroservoelastic stability margin analysis; flight testing data; multi-loop aeroservoelastic system; multi-loop system; nonparametric identification; on-line method; on-line stability evaluation; open-loop transfer function; return difference matrix method; single-input-single-output system; stability analysis; time-frequency domain; wavelet filter; wavelet processing; Filters; Noise robustness; Robust stability; Stability analysis; System testing; Time frequency analysis; Transfer functions; Uncertainty; Wavelet analysis; Wavelet domain;
fLanguage
English
Publisher
ieee
Conference_Titel
Systems and Control in Aerospace and Astronautics, 2006. ISSCAA 2006. 1st International Symposium on
Conference_Location
Harbin
Print_ISBN
0-7803-9395-3
Type
conf
DOI
10.1109/ISSCAA.2006.1627440
Filename
1627440
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