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
Link To Document :
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