DocumentCode :
2856247
Title :
Pulse-compression probing for nonlinear systems with additional hard nonlinearity at the input
Author :
Ruschmann, M. ; Wu, N. Eva
Author_Institution :
Dept. of Electr. & Comput. Eng., Binghamton Univ., Binghamton, NY, USA
fYear :
2011
fDate :
June 29 2011-July 1 2011
Firstpage :
232
Lastpage :
237
Abstract :
The effects of input hard nonlinearities on probing outputs are analyzed with respect to the pulse-compression probing method. The pulse-compression probing method identifies a local, linear model around an operating point of a nonlinear system by processing the system response to a probing input. The outputs of probing systems with one of six common input hard nonlinearities, including deadband, saturation, relay, backlash, and rate limit are derived. Pulse-compression probing is effective for the first five hard nonlinearities listed, where the probing outputs retain the same waveforms as if the probing inputs were scaled and offset. When probing an input with a rate limit, pulse-compression probing is effective when the bit duration of the probing input exceeds some threshold, which is based on the rate limit. As long as the probing input is properly designed with respect to the input nonlinearities present, the shape of the probing output is preserved. As a numerical example, pulse-compression probing method is applied to the NASA generic transport aircraft model with nonlinearities at the probing input.
Keywords :
aircraft control; nonlinear control systems; pulse compression; NASA generic transport aircraft model; backlash; deadband; input hard nonlinearities; nonlinear system; probing outputs; pulse-compression probing method; rate limit; relay; saturation; Atmospheric modeling; Gears; Hysteresis; Monitoring; NASA; Relays; Visualization;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference (ACC), 2011
Conference_Location :
San Francisco, CA
ISSN :
0743-1619
Print_ISBN :
978-1-4577-0080-4
Type :
conf
DOI :
10.1109/ACC.2011.5991345
Filename :
5991345
Link To Document :
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