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Design of Control Laws and State Observers for Fixed-Wing UAVs
Simulation and Experimental Approaches
Presents fixed-wing UAV modeling techniques, simulations, and results from real-time experiments using linear and nonlinear controllers and state observers
Arturo Tadeo Espinoza-Fraire (Author), Alejandro Enrique Dzul López (Author), Ricardo Pavel Parada Morado (Author), José Armando Sáenz Esqueda (Author)
9780323954051, Elsevier Science
Paperback / softback, published 6 October 2022
290 pages
27 x 18 x 1.9 cm, 0.45 kg
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.
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
Subject Areas: Mechanical engineering [TGB]
