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Nominal Model-Based Sliding Mode Control with Backstepping for 3-Axis Flight Table 被引量:11
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作者 刘金琨 孙富春 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2006年第1期65-71,共7页
Based on nominal model, a novel global sliding mode controller (GSMC) with a new control scheme is proposed for a practical uncertain servo system. This control scheme consists of two combined controllers, One is th... Based on nominal model, a novel global sliding mode controller (GSMC) with a new control scheme is proposed for a practical uncertain servo system. This control scheme consists of two combined controllers, One is the global sliding mode controller for practical plant, the other is the integral backstepping controller for nominal model. Modeling error between practical plant and nominal model is used to design GSMC. The steady-state control accuracy can be guaranteed by the integral backstepping control law, and the global robustness can be obtained by GSMC. The stability of the proposed controller is proved according to the Lyapunov approach. The simulation results both of sine signal and step signal tracking for 3-axis flight table are investigated to show good position tracking performance and high robustness with respect to large and parameter changes over all the response time. 展开更多
关键词 nominal model sliding mode control backstepping control robust control 3-axis flight table
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QFT Robust Control Design for 3-Axis Flight Table Servo System with Large Friction 被引量:3
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作者 刘金琨 尔联洁 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2004年第1期34-38,共5页
The 3-axis flight table is an important device and a typical high performanceposition and speed servo system used in the hardware-in-the-loop simulation of flight controlsystem. Friction force and uncertainty are the ... The 3-axis flight table is an important device and a typical high performanceposition and speed servo system used in the hardware-in-the-loop simulation of flight controlsystem. Friction force and uncertainty are the main characteristics in the 3-axis flight table servosystem. Based on the description of dynamic and static model of a nonlinear Stribeck frictionmodel, and taking account of the practical uncertainties of 3-axis flight table servo system, theQFT controller is designed. Simulation and realtime results are presented. 展开更多
关键词 quantitative feedback theory 3-axis flight table friction model ROBUSTCONTROL
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