"Advances in Flight Control Systems" ed. by Agneta Balint
ITexLi | 2017 | ISBN: 9533072180 9789533072180 | 309 pages | PDF | 17 MB
ITexLi | 2017 | ISBN: 9533072180 9789533072180 | 309 pages | PDF | 17 MB
The aim of the book is to bring together reputable researchers from different countries in order to provide a comprehensive coverage of advanced and modern topics in flight control not yet reflected by other books. This book covers most of the currents main streams of flight control researches, ranging from adaptive flight control mechanism, fault tolerant flight control, acceleration based flight control, helicopter flight control, comparison of flight control systems and fundamentals.
Nonlinear problems in flight control have stimulated cooperation among engineers and scientists from a range of disciplines. Developments in computer technology allowed for numerical solutions of nonlinear control problems, while industrial recognition and applications of nonlinear mathematical models in solving technological problems is increasing.
Contents
Preface
1 Adaptive Fight Control Actuators and Mechanisms for Missiles, Munitions and Uninhabited Aerial Vehicles (UAVs)
2 Adaptive Backstepping Flight Control for Modern Fighter Aircraft
3 Hybrid Adaptive Flight Control with Model Inversion Adaptation
4 Application of Evolutionary Computing in Control Allocation
5 Fault Tolerant Flight Control, a Physical Model Approach
6 Design of Intelligent Fault-Tolerant Flight Control System for Unmanned Aerial Vehicles
7 Active Fault Diagnosis and Major Actuator Failure Accommodation: Application to a UAV
8 Fault-Tolerance of a Transport Aircraft with Adaptive Control and Optimal Command Allocation
9 Acceleration-based 3D Flight Control for UAVs: Strategy and Longitudinal Design
10 Autonomous Flight Control System for Longitudinal Motion of a Helicopter
11 Autonomous Flight Control for RC Helicopter Using a Wireless Camera
12 Hierarchical Control Design of a UAV Helicopter
13 Comparison of Flight Control System Design Methods in Landing
14 Oscillation Susceptibility of an Unmanned Aircraft whose Automatic Flight Control System Fails
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