کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
755672 1462561 2006 7 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
Nominal Model-Based Sliding Mode Control with Backstepping for 3-Axis Flight Table
موضوعات مرتبط
مهندسی و علوم پایه سایر رشته های مهندسی مهندسی هوافضا
پیش نمایش صفحه اول مقاله
Nominal Model-Based Sliding Mode Control with Backstepping for 3-Axis Flight Table
چکیده انگلیسی

Based on nominal model, a novel global sliding mode controller (GSMC) with a new control scheme is proposal 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 rcr bustness with respect to large and parameter changes over all the response time.

ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Chinese Journal of Aeronautics - Volume 19, Issue 1, February 2006, Pages 65-71