State Estimation and Control for Low-cost Unmanned Aerial Vehicles
Autor Chingiz Hajiyev, Halil Ersin Soken, Sıtkı Yenal Vuralen Limba Engleză Hardback – 27 iun 2015
State Estimation and Control of Low-Cost Unmanned Aerial Vehicles covers all the important issues for designing a guidance, navigation and control (GNC) system of a low-cost UAV. It proposes significant new approaches that can be exploited by GNC system designers in the future and also reviews the current literature. The state estimation, control and FDI methods are illustrated by examples and MATLAB® simulations.
State Estimation and Control of Low-Cost Unmanned Aerial Vehicles will be of interest to both researchers in academia and professional engineers in the aerospace industry. Graduate students may also find it useful, and some sections are suitable for an undergraduate readership.
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Specificații
ISBN-13: 9783319164168
ISBN-10: 3319164163
Pagini: 242
Ilustrații: XII, 232 p. 156 illus., 38 illus. in color.
Dimensiuni: 155 x 235 x 17 mm
Greutate: 0.52 kg
Ediția:2015
Editura: Springer International Publishing
Colecția Springer
Locul publicării:Cham, Switzerland
ISBN-10: 3319164163
Pagini: 242
Ilustrații: XII, 232 p. 156 illus., 38 illus. in color.
Dimensiuni: 155 x 235 x 17 mm
Greutate: 0.52 kg
Ediția:2015
Editura: Springer International Publishing
Colecția Springer
Locul publicării:Cham, Switzerland
Public țintă
ResearchCuprins
Introduction to Unmanned Aerial Vehicles.- Equations of Motion for the UAV.- Navigation Systems for UAV.- Estimation of the UAV Dynamics.- Estimation of the UAV Dynamics.- Estimation of the UAV Dynamics in the Presence of Sensor Faults.- Estimation of the UAV Dynamics in the Presence of Sensor/Actuator Faults.- Fault Detection, Isolation and Data Fusion for the UAV Air Data System.- Stability Analysis for the UAV.- Classical Controller Design for the UAV.- LQR Controller Design.- Fuzzy Logic Based Controller Design.
Textul de pe ultima copertă
This book discusses state estimation and control procedures for a low-cost unmanned aerial vehicle (UAV). The authors consider the use of robust adaptive Kalman filter algorithms and demonstrate their advantages over the optimal Kalman filter in the context of the difficult and varied environments in which UAVs may be employed. Fault detection and isolation (FDI) and data fusion for UAV air-data systems are also investigated, and control algorithms, including the classical, optimal, and fuzzy controllers, are given for the UAV. The performance of different control methods is investigated and the results compared.
State Estimation and Control of Low-Cost Unmanned Aerial Vehicles covers all the important issues for designing a guidance, navigation and control (GNC) system of a low-cost UAV. It proposes significant new approaches that can be exploited by GNC system designers in the future and also reviews the current literature. The state estimation, control and FDI methods are illustrated by examples and MATLAB® simulations.
State Estimation and Control of Low-Cost Unmanned Aerial Vehicles will be of interest to both researchers in academia and professional engineers in the aerospace industry. Graduate students may also find it useful, and some sections are suitable for an undergraduate readership.
State Estimation and Control of Low-Cost Unmanned Aerial Vehicles covers all the important issues for designing a guidance, navigation and control (GNC) system of a low-cost UAV. It proposes significant new approaches that can be exploited by GNC system designers in the future and also reviews the current literature. The state estimation, control and FDI methods are illustrated by examples and MATLAB® simulations.
State Estimation and Control of Low-Cost Unmanned Aerial Vehicles will be of interest to both researchers in academia and professional engineers in the aerospace industry. Graduate students may also find it useful, and some sections are suitable for an undergraduate readership.
Caracteristici
Includes key issues in designing guidance navigation and control system of an UAV The theory presented is supported with and illustrated by simulation results, for ease of comprehension The novel approach will be of interest to engineers in diverse fields, such as aerospace, control engineering and signal processing