Fault-tolerant Flight Control and Guidance Systems: Practical Methods for Small Unmanned Aerial Vehicles [Paperback]

Review.- Nonlinear Aircraft Model.- Nonlinear Fault Detection and Isolation System.- Control Allocation.- Nonlinear Control Design.- Autopilot for the Longitudinal Motion.- Autopilot for the Lateral Motion.- Reconfigurable Guidance System.- Evaluation of the Reduction in the Performance of a UAV.- Conclusions and Outlook.

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.

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 aircrafts 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: bls