Derivative-Free Adaptive Control, デリバティブフリー適応制御, 9781624107016, 978-1-62410-701-6

Derivative-Free Adaptive Control

学術書籍  >  理工学  >  AIAAタイトル  > 




Derivative-Free Adaptive Control

24,200(税込)

数量

書名

Derivative-Free Adaptive Control
デリバティブフリー適応制御
著者・編者 Yucelen, T. & Calise, A.
発行元 AIAA (American Institute of Aeronautics and Astronautics)
発行年/月 2023年9月
装丁 Hardcover
ISBN 978-1-62410-701-6
発送予定 海外倉庫よりお取り寄せ 6-10週間以内に発送します
 

Description

Derivative-Free Adaptive Control serves as a compendium of the authors' scholarship on the development of and theory for adaptive control, referred to herein as Derivative-Free Model Reference Adaptive Control (DF-MRAC).
Previous methods of Model Reference Adaptive Control (MRAC) were based on the underlying assumption that plant model uncertainty can be approximated by a set of state dependent basis functions that are parameterized by an unknown but constant set of weights.
In DF-MRAC, the viewpoint taken is that ideal weights may be time varying and, in fact, one can do away with the need for choosing a set of basis functions. The book presents a set of reproducible examples that illustrate the important features and advantages of DF-MRAC over conventional MRAC methods, and points out the many circumstances that exist for which a constant parameterization of uncertainty may be difficult or impossible to achieve, particularly in the case of unmodeled dynamics, time varying uncertainties, and exogenous disturbances that may be acting on the system being controlled.
Geared toward graduate students, scholars, and experienced designers in the industry, the book clearly illustrates the benefits offered by DF-MRAC by contrasting it with Derivative-Based MRAC. It includes easy to follow and implementable examples, and collects existing results on this subject in one volume.

 

Contents:

Derivative-Free Adaptive Control
Introduction
Model Reference Adaptive Control
Derivative-Free Model Reference Adaptive Control
Robustness to Unmodeled Dynamics
The Output Feedback Case
Large-Scale Systems
Applications to Flight Control
Conclusions and Some Possible Future Directions
Index
Supporting Materials