Nonlinear state feedback synthesis by global input/output linearization
نویسندگان
چکیده
منابع مشابه
Distributed control of nonlinear diffusion systems by inputoutput linearization
This paper addresses the distributed control by input–output linearization of a nonlinear diffusion equation that describes a particular but important class of distributed parameter systems. Both manipulated and controlled variables are assumed to be distributed in space. The control law is designed using the concept of characteristic index from geometric control by using directly the PDE model...
متن کاملNonlinear State Feedback Synthesis
This paper studies the design of feedback controllers for trajectory tracking in single-inputlsingle-output nonlinear systems X = f (x ) + g(x) u, y = h(x). A nonlinear transformation of the form z, = K ( X ) + X(x) u that transforms this nonlinear input/output system into a linear system is first constructed. On the basis of this transformation, an approach for designing control laws for traje...
متن کاملOn Global Transverse Feedback Linearization
Necessary and sufficient conditions for global transverse feedback linearization are presented, together with easy-to-check sufficient conditions.
متن کاملOn the Recoverability of Nonlinear State Feedback Laws by Extended Linearization Control Techniques
Extended linearization is the process of factoring a nonlinear system into a linear-like structure x = A(x)x + B(x)u which contains state-dependent coefficient (SDC) matrices. An extended linearization control technique is any technique which (a) treats the SDC matrices A(z) and B(x ) as being constant and (b) uses a linear control synthesis method on the linear-like structure to produce a clos...
متن کاملNonlinear Attitude Control for a Rigid Spacecraft by Feedback Linearization
Attitude control law design for spacecraft large angle maneuvers is investigated in this paper. The feedback linearization technique is applied to the design of a nonlinear tracking control law. The output function to be tracked is the quaternion attitude parameter. The designed control law turns out to be a combination of attitude and attitude rate tracking command. The attitude-only output fu...
متن کاملذخیره در منابع من
با ذخیره ی این منبع در منابع من، دسترسی به آن را برای استفاده های بعدی آسان تر کنید
ژورنال
عنوان ژورنال: AIChE Journal
سال: 1987
ISSN: 0001-1541,1547-5905
DOI: 10.1002/aic.690330408