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Adaptive Sliding Control of Six-DOF Flight Simulator Motion Platform
Authors:Wu Dongsu  Gu Hongbin
Affiliation:College of Civil Aviation, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
Abstract:
There is proposed an adaptive sliding controller in task space on the base of the linear Newton-Euler dynamic equation of motion platform in a six-DOF flight simulator. The uncertain parameters are divided into two groups: the constant and the time-varying. The controller identifies constant uncertain parameters using nonlinear adaptive controller associated with elimination of the influences of time-varying uncertain parameters and compensation of the external disturbance using sliding control. The results of numerical simulation attest to the capability of this control scheme not only to, with deadly accuracy, identify parameters of motion platform such as load,inertia moments and mass center, but also effectively improve the robustness of the system.
Keywords:motion platform  nonlinear adaptive control  sliding control  flight simulator  Stewart platform  Platform  Motion  Flight Simulator  Control  Sliding  improve  robustness  system  inertia  moments  mass  center  identify  parameters  motion  load  accuracy  results  numerical simulation  capability
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