作者: J. Davila , A. Monsivais , A. Mosqueda
DOI: 10.1007/978-3-319-09858-6_26
关键词: Autopilot 、 Control theory 、 Compensation (engineering) 、 Linear system 、 Bounded function 、 Computer science 、 Control engineering 、 Missile 、 Nonlinear system 、 Control theory 、 Linearization
摘要: The high-order sliding modes are applied for system linearization of a class nonlinear systems. nonlinearites the treated as bounded external disturbances acting on linear system. A standard controller is designed linearized robust composed by two terms: first, controller, that provides desired performance in absence perturbations; second, compensation term, using sliding-modes techniques, used to compensate perturbations affect workability proposed illustrated with design roll autopilot missile.