DocumentCode
3028183
Title
Application of Adaptive Inverse Control in Control Loading System of Flight Simulator based on rapid prototyping of RT_LAB
Author
Jingsong, Zhao ; Gang, Shen ; Jun-wei, Han
Author_Institution
Sch. of Electromech. Eng., Harbin Inst. of Technol., Harbin, China
fYear
2010
fDate
8-10 June 2010
Firstpage
649
Lastpage
653
Abstract
Adaptive Inverse Control (AIC) based on Recursive Least Square (RLS) is applied in Control Loading System (CLS) of Flight Simulator (FS) .The algorithm was used to improve position tracking accuracy as an inner loop of CLS. This paper presents the implementation of a rapid prototyping control system based on RAT-LAB simulation environment, which involves the design of AIC and RLS algorithms using MATLAB/Simulink blocksets. The effectiveness of AIC was verified by mean of the analysis of the experiment results such as the comparison of reference signal and position output response signal, the change of frequency bandwidth. Finally, the accuracy of identification was pointed out via experiment that is a critical factor of the AIC.
Keywords
adaptive control; aerospace simulation; aircraft control; least squares approximations; mathematics computing; position control; software prototyping; MATLAB/Simulink blocksets; RT-LAB; adaptive inverse control; control loading system; flight simulator; position tracking; rapid prototyping; recursive least squares; Accuracy; Adaptation model; Atmospheric modeling; Bandwidth; Control systems; Load modeling; Loading;
fLanguage
English
Publisher
ieee
Conference_Titel
Systems and Control in Aeronautics and Astronautics (ISSCAA), 2010 3rd International Symposium on
Conference_Location
Harbin
Print_ISBN
978-1-4244-6043-4
Electronic_ISBN
978-1-4244-7505-6
Type
conf
DOI
10.1109/ISSCAA.2010.5632322
Filename
5632322
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