DocumentCode
3048666
Title
The robust and perfect tracking control for flight simulator
Author
Zheng, Lianqiang ; Wang, Weihong ; Yao, Zhichao
Author_Institution
Sch. of Autom. Sci. & Electr. Eng., Beijing Univ. of Aeronaut. & Astronaut., Beijing, China
fYear
2010
fDate
20-23 June 2010
Firstpage
1033
Lastpage
1039
Abstract
Due to requirements of engineering application, introduce some additional information besides the reference signal, i.e., the derivative of reference signal and the second derivative of reference signal, as additional controller inputs, the robust and perfect tracking control (RPT) strategy is imported into the design of a perfect tracking controller for the flight simulator. By choosing appropriate state variables and controlled output, the time domain design method, RPT control method, can utilize all possible information from the reference signal and the integration of dynamic error. As a result, our problem formulation and design algorithms are capable of tracking any polynomial signals with an arbitrarily fast settling time without actually augmenting any additional integrator to the given plant. Furthermore, the simulation results show the validity of the design.
Keywords
aerospace simulation; systems analysis; tracking; flight simulator; requirements engineering; robust and perfect tracking control; time domain design; Aerodynamics; Aerospace simulation; Deformable models; Design methodology; Error correction; Frequency domain analysis; Frequency response; Missiles; Robust control; Servomechanisms; dynamic tracking error; flight simulator; robust and perfect tracking control; special coordinate basis; time domain design;
fLanguage
English
Publisher
ieee
Conference_Titel
Information and Automation (ICIA), 2010 IEEE International Conference on
Conference_Location
Harbin
Print_ISBN
978-1-4244-5701-4
Type
conf
DOI
10.1109/ICINFA.2010.5512298
Filename
5512298
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