General Integral Control Design via Feedback Linearization
نویسندگان
چکیده
منابع مشابه
Aircraft trajectory control with feedback linearization for general nonlinear system
1. China Aerodynamics Research and Development Center, Mianyang, 621000 2. China State Key Laboratory of Aerodynamics, Mianyang, 621000 E-mail: [email protected] Abstract: The feedback linearization method is further developed for the controller design on general nonlinear systems. Through the Lyapunov stability theory, the intractable nonlinear implicit algebraic control equations are...
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ژورنال
عنوان ژورنال: Intelligent Control and Automation
سال: 2014
ISSN: 2153-0653,2153-0661
DOI: 10.4236/ica.2014.51003