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Fault-tolerant Flight Control and Guidance Systems: Practical Methods for Small Unmanned Aerial Vehicles (Advances in Industrial Control)
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This book offers a complete overview of fault-tolerant flight control techniques. Discussion covers the necessary equations for the modeling of small UAVs, a complete system based on extended Kalman filters, and a nonlinear flight control and guidance system.
- Sales Rank: #9826392 in Books
- Published on: 2010-10-21
- Released on: 2010-10-21
- Original language: English
- Number of items: 1
- Dimensions: 9.25" h x .66" w x 6.10" l, .91 pounds
- Binding: Paperback
- 268 pages
From the Back Cover
Unmanned aerial vehicles (UAVs) offer an incomparable means of gathering intelligence and carrying out missions without needing an onboard human pilot. The benefits are considerable in terms of cost, efficiency, and reduced pilot risk.
In order to complete a mission efficiently and with a high level of safety and security, the following key design points must be met:
• the flight control system must be robust against the aircraft’s model uncertainties and external disturbances;
• an efficient fault detection and isolation (FDI) system should be capable of monitoring the health of the aircraft; and
• the flight control and guidance system should be reconfigurable depending on actuator fault occurrence or aircraft damage, and should be able to avoid obstacles.
Fault-tolerant Flight Control and Guidance Systems addresses all of these aspects with a practical approach following three main requirements: being applicable in real-time; highly computationally efficient; and modular. The text provides:
• an overview of fault-tolerant flight control techniques;
• the necessary equations for the modeling of small UAVs;
• a complete nonlinear FDI system based on extended Kalman filters; and
• a nonlinear flight control and guidance system.
The book is written in a didactic style with many figures and diagrams making it suitable not only for academic researchers and practicing engineers but also graduate students working in the fields of fault detection techniques and the automatic control of UAVs.
About the Author
Between 2002 and 2004, Guillaum Ducard worked with the team designing the Pac-Car 2, designing hardware and control software for embedded fuel cell systems. The vehicle holds the world record for fuel economy. Since 2004, Doctor Ducard has been interested in hardware and software for unmanned aerial vehicles including fixed-wing aeroplanes, high-altitude atmospheric air ships and quadricopters. He received his Dr.Sc. degree from ETH in 2007. His current research involves the design of navigation algorithms, flight control and guidance systems for quadricopters. Guillaume Ducard is a member of the IEEE and of the AIAA.
Most helpful customer reviews
1 of 1 people found the following review helpful.
Monograph Main Contributions
By SIMANI SILVIO
The monograph is very interesting, well written and well organised. It is of interest to a wide range of readers from the industrial and the control communities. Academic researchers and graduate students working in the mobile autonomous vehicle field may find transferable knowledge in this well-structured monograph and it will obviously appeal to aerospace researchers and engineers.
Regarding the book structure, Chapter 1 provides the main motivations of the monograph. Chapter 2 focuses on a literature review about the fault-tolerant flight control systems already developed for aircraft. Chapter 3 presents the nonlinear model used for simulation and control design. Chapter 4 describes a new system for the detection and isolation of actuator faults in an aircraft. Chapter 5 details the design and the implementation of a reconfigurable control allocation module. Chapter 6 describes the technique known as nonlinear dynamic inversion and presents the architecture and the design procedure of the controllers used in the aircraft autopilot. Chapter 7 is dedicated to the analysis and control of the longitudinal axis of the aircraft and presents architecture for the altitude controller that uses robust NDI in all the control loops. Chapter 8 is dedicated to the analysis and control of the lateral-directional motion of the aircraft. It describes the controllers for the roll and yaw rates, for the roll angle, and for the sideslip angle. Chapter 9 presents a new adaptive path-planning algorithm, which reconfigures the aircraft's trajectory based on its flying performance after the occurrence of an actuator failure. Chapter 10 focuses on an aileron failure and shows how the degraded flying performance can be evaluated and used to reconfigure the guidance system. Finally, the book concludes with an outlook and summarizes the methods presented.
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