Controller Design for Variable Maneuverability and Disturbance Rejection for Vehicles:
نویسندگان
چکیده
منابع مشابه
Disturbance Rejection Controller Design Based on Sensitivity Function Notching
This paper presents a feed-forward control scheme for rejecting stochastic narrow band disturbances. The effect of this scheme manifests itself as a tunable notch on the sensitivity transfer function frequency response, where the target frequency, width, and depth of the notch can be set by prescribed design parameters. This approach is based on employing least mean square adaptive control that...
متن کاملDesign of Diesel Engine Adaptive Active Disturbance Rejection Speed Controller
The ship main engine speed control system is a typical nonlinear system and it is uncertain characteristics, It is influenced by the wind, wave, flow etc. So it is difficulted to designed the diesel engine mathematical model. This paper presents a nonlinear mathematical model of ship main engine. Because the active disturbance rejection controller does not depend on the mathematical model of th...
متن کاملCDM Controller Order and Disturbance Rejection Ability
algebraic control design method whose objective is to easily obtain a good controller with minimum user effort. As a matter of fact, if a system model, in the form of linear differential equations, is known, the user only need to define a time-constant and the controller order. The later can be established regarding the expected disturbance type via a lookup table first published by Koksal and ...
متن کاملAn Adaptive Internal Model-based Controller for Periodic Disturbance Rejection
This paper details the design of an adaptive internal model-based controller to attenuate periodic disturbances in the presence of random noise. The internal model-based controller is designed in two steps, making use of the separation principle to design a controller with the desired properties that stabilizes the closed-loop system. Periodic disturbances appear as harmonics of a fundamental f...
متن کاملH∞ Controller for Disturbance Rejection in a Fixed Wing Uav
This paper presents a nonlinear H∞ controller for the rejection of input disturbances in a fixed wing Unmanned Aerial Vehicle (UAV). The controller acts in all states of a complete nonlinear dynamic model. Simulation results shows that the aircraft is successfully maintained in the desired stable condition after a finite pulse disturbance. Keywords— Nonlinear H∞ Control, Fixed Wing UAV. Resumo—...
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: Transactions of the Society of Instrument and Control Engineers
سال: 2007
ISSN: 0453-4654
DOI: 10.9746/ve.sicetr1965.43.632