This chapter provides a technical overview and the necessary background for existing controller synthesis methods that have been applied for navigation and control of UAVs. These include linear controllers (PID, LQR, LQG, etc.), backstepping, sliding mode, nonlinear model predictive, adaptive, dynamic inversion, fuzzy logic and neural networks, gain scheduling, \documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$$H_\infty $$\end{document} and \documentclass[12pt]{minimal} \usepackage{amsmath} \usepackage{wasysym} \usepackage{amsfonts} \usepackage{amssymb} \usepackage{amsbsy} \usepackage{mathrsfs} \usepackage{upgreek} \setlength{\oddsidemargin}{-69pt} \begin{document}$$\mu $$\end{document}-synthesis [1, 2]. The distinctive advantages and drawbacks for each technique are investigated with respect to applicability to the family of new generation UAVs with time-varying aerodynamic characteristics.
Literature Review
Springer Tracts in Autonomous Systems
Nonlinear Control of Fixed-Wing UAVs with Time-Varying and Unstructured Uncertainties ; Kapitel : 2 ; 9-28
2020-02-22
20 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
Springer Verlag | 2022
|Online Contents | 1996
Online Contents | 1996
Online Contents | 1997
Online Contents | 1997