Design of Control Laws and State Observers for Fixed-Wing UAVs - Simulation and Experimental Approaches

Design of Control Laws and State Observers for Fixed-Wing UAVs: Simulation and Experimental Approaches provides readers with modeling techniques, simulations, and results from real-time experiments using linear and nonlinear controllers and state observers. The book starts with an overview of the history of UAVs and the equations of motion applied to them. Following chapters analyze linear and nonlinear controllers, state observers, and the book concludes with a chapter discussing testbed development and experimental results, equipping readers with the knowledge they need to conduct their own stable UAV flights whether in simulation or real-time.

List of contents

1. Introduction
2. Aerodynamic principles
3. Equations of Motion of a fixed-wing UAV
4. Linear controllers
5. Nonlinear controllers
6. State observers
7. Testbed and experimental results
A Mathematical review
B Kinematics and dynamics background
C Stability in the Lyapunov sense
D Fundamentals of linear and nonlinear controllers
E Discrete-time Kalman filter
F Linear and nonlinear controllers: programs for the embedded system
G Linear and nonlinear state observers: programs for the embedded system
H MATLAB® program to graph
I Altimeter program

Product details

• Authors: Alejandro Enrique Dzul López, Arturo Tadeo Espinoza-Fraire, Alejandro Enrique Dzul López, Arturo Tadeo Espinoza-Fraire, José Armando Sáenz Esqueda, Ricardo Pavel Parada Morado, Ricardo Pavel Parada Morado, José Armando Sáenz Esqueda
• Publisher: Elsevier Science & Technology
• Languages: English
• Product format: Paperback / Softback
• Released: 06.10.2022
• EAN: 9780323954051
• ISBN: 978-0-323-95405-1
• Dimensions: 152 mm x 14 mm x 229 mm
• Weight: 450 g
• Subjects: Natural sciences, medicine, IT, technology > Technology > Mechanical engineering, production engineering; TECHNOLOGY & ENGINEERING / Mechanical, Aerospace & aviation technology, Aerospace and aviation technology