Aircraft Control and Simulation: Dynamics, Controls Design, and Autonomous Systems

Get a complete understanding of aircraft control and simulation Aircraft Control and Simulation: Dynamics, Controls Design, and Autonomous Systems, Third Edition is a comprehensive guide to aircraft control and simulation. This updated text covers flight control systems, flight dynamics, aircraft modeling, and flight simulation from both classical design and modern perspectives, as well as two new chapters on the modeling, simulation, and adaptive control of unmanned aerial vehicles. With detailed examples, including relevant MATLAB calculations and FORTRAN codes, this approachable yet detailed reference also provides access to supplementary materials, including chapter problems and an instructor?s solution manual. Aircraft control, as a subject area, combines an understanding of aerodynamics with knowledge of the physical systems of an aircraft. The ability to analyze the performance of an aircraft both in the real world and in computer–simulated flight is essential to maintaining proper control and function of the aircraft. Keeping up with the skills necessary to perform this analysis is critical for you to thrive in the aircraft control field. Explore a steadily progressing list of topics, including equations of motion and aerodynamics, classical controls, and more advanced control methods Consider detailed control design examples using computer numerical tools and simulation examples Understand control design methods as they are applied to aircraft nonlinear math models Access updated content about unmanned aircraft (UAVs) Aircraft Control and Simulation: Dynamics, Controls Design, and Autonomous Systems, Third Edition is an essential reference for engineers and designers involved in the development of aircraft and aerospace systems and computer–based flight simulations, as well as upper–level undergraduate and graduate students studying mechanical and aerospace engineering. INDICE: Preface xi .1 The Kinematics and Dynamics of Aircraft Motion 1 .1.1 Introduction / 1 .1.2 Vector Operations / 3 .1.3 Matrix Operations on Vector Coordinates / 7 .1.4 Rotational Kinematics / 16 .1.5 Translational Kinematics / 20 .1.6 Geodesy, Coordinate Systems, Gravity / 23 .1.7 Rigid–Body Dynamics / 34 .1.8 Advanced Topics / 44 .References / 58 .Problems / 59 .2 Modeling the Aircraft 63 .2.1 Introduction / 63 .2.2 Basic Aerodynamics / 64 .2.3 Aircraft Forces And Moments / 75 .2.4 Static Analysis / 101 .2.5 The Nonlinear Aircraft Model / 108 .2.6 Linear Models And The Stability Derivatives / 116 .2.7 Summary / 137 .References / 138 .Problems / 139 .3 Modeling, Design, and Simulation Tools 142 .3.1 Introduction / 142 .3.2 State–Space Models / 144 .3.3 Transfer Function Models / 155 .3.4 Numerical Solution Of The State Equations / 170 .3.5 Aircraft Models For Simulation / 179 .3.6 Steady–State Flight / 185 .3.7 Numerical Linearization / 199 .3.8 Aircraft Dynamic Behavior / 205 .3.9 Feedback Control / 213 .3.10 Summary / 241 .References / 241 .Problems / 243 .4 Aircraft Dynamics and Classical Control Design 250 .4.1 Introduction / 250 .4.2 Aircraft Rigid–Body Modes / 257 .4.3 The Handling–Qualities Requirements / 274 .4.4 Stability Augmentation / 287 .4.5 Control Augmentation Systems / 303 .4.6 Autopilots / 322 .4.7 Nonlinear Simulation / 344 .4.8 Summary / 371 .References / 372 .Problems / 374 .5 Modern Design Techniques 377 .5.1 Introduction / 377 .5.2 Assignment Of Closed–Loop Dynamics / 381 .5.3 Linear Quadratic Regulator With Output Feedback / 397 .5.4 Tracking A Command / 413 .5.5 Modifying The Performance Index / 428 .5.6 Model–Following Design / 455 .5.7 Linear Quadratic Design With Full State Feedback / 470 .5.8 Dynamic Inversion Design / 477 .5.9 Summary / 492 .References / 492 .Problems / 495 .6 Robustness and Multivariable Frequency–Domain Techniques 500 .6.1 Introduction / 500 .6.2 Multivariable Frequency–Domain Analysis / 502 .6.3 Robust Output–Feedback Design / 525 .6.4 Observers And The Kalman Filter / 529 .6.5 Linear Quadratic Gaussian/Loop Transfer Recovery / 554 .6.6 Summary / 577 .References / 578 .Problems / 580 .7 Digital Control 584 .7.1 Introduction / 584 .7.2 Simulation Of Digital Controllers / 585 .7.3 Discretization Of Continuous Controllers / 588 .7.4 Modified Continuous Design / 598 .7.5 Implementation Considerations / 611 .7.6 Summary / 619 .References / 620 .Problems / 620 .8 Modeling and Simulation of Miniature Aerial Vehicles 623 .8.1 Introduction / 623 .8.2 Propeller/Rotor Forces And Moments / 630 .8.3 Modeling Rotor Flapping / 640 .8.4 Motor Modeling / 645 .8.5 Small Aerobatic Airplane Model / 648 .8.6 Quadrotor Model / 654 .8.7 Small Helicopter Model / 655 .8.8 Summary / 660 .References / 661 .Problems / 661 .9 Adaptive Control With Application to Miniature Aerial Vehicles 664 .9.1 Introduction / 664 .9.2 Model Reference Adaptive Control Based On Dynamic Inversion / 665 .9.3 Neural Network Adaptive Control / 668 .9.4 Limited Authority Adaptive Control / 674 .9.5 Neural Network Adaptive Control Example / 680 .9.6 Summary / 709 .References / 709 .Problems / 711 .Appendix A F–16 Model 714 .Appendix B Software 723 .Index 733

• ISBN: 978-1-118-87098-3
• Editorial: John Wiley & Sons
• Encuadernacion: Rústica
• Páginas: 768
• Fecha Publicación: 25/11/2015
• Nº Volúmenes: 1
• Idioma: Inglés