BRIAN L. STEVENS is a retired Senior Research Engineer from the Georgia Institute of Technology Research Institute, where he continues to teach classes in Guidance, Navigation, and Control. FRANK L. LEWIS is a Distinguished Scholar Professor, Distinguished Teaching Professor, and Moncrief-O'Donnell Chair at the University of Texas at Arlington Research Institute. ERIC N. JOHNSON is the Lockheed Martin Associate Professor of Avionics Integration, Daniel Guggenheim School of Aerospace Engineering at Georgia Institute of Technology.

• Preface xi1 The Kinematics and Dynamics of Aircraft Motion 11.1 Introduction 11.2 Vector Operations 31.3 Matrix Operations on Vector Coordinates 71.4 Rotational Kinematics 161.5 Translational Kinematics 201.6 Geodesy, Coordinate Systems, Gravity 231.7 Rigid-Body Dynamics 341.8 Advanced Topics 44References 58Problems 592 Modeling the Aircraft 632.1 Introduction 632.2 Basic Aerodynamics 642.3 Aircraft Forces And Moments 752.4 Static Analysis 1012.5 The Nonlinear Aircraft Model 1082.6 Linear Models And The Stability Derivatives 1162.7 Summary 137References 138Problems 1393 Modeling, Design, and Simulation Tools 1423.1 Introduction 1423.2 State-Space Models 1443.3 Transfer Function Models 1553.4 Numerical Solution of The State Equations 1703.5 Aircraft Models For Simulation 1793.6 Steady-State Flight 1853.7 Numerical Linearization 1993.8 Aircraft Dynamic Behavior 2053.9 Feedback Control 2133.10 Summary 241References 241Problems 2434 Aircraft Dynamics and Classical Control Design 2504.1 Introduction 2504.2 Aircraft Rigid-Body Modes 2574.3 The Handling-Qualities Requirements 2744.4 Stability Augmentation 2874.5 Control Augmentation Systems 3034.6 Autopilots 3224.7 Nonlinear Simulation 3444.8 Summary 371References 372Problems 3745 Modern Design Techniques 3775.1 Introduction 3775.2 Assignment of Closed-Loop Dynamics 3815.3 Linear Quadratic Regulator With Output Feedback 3975.4 Tracking A Command 4135.5 Modifying The Performance Index 4285.6 Model-Following Design 4555.7 Linear Quadratic Design with Full State Feedback 4705.8 Dynamic Inversion Design 4775.9 Summary 492References 492Problems 4956 Robustness and Multivariable Frequency-Domain Techniques 5006.1 Introduction 5006.2 Multivariable Frequency-Domain Analysis 5026.3 Robust Output-Feedback Design 5256.4 Observers and The Kalman Filter 5296.5 Linear Quadratic Gaussian/Loop Transfer Recovery 5546.6 Summary 577References 578Problems 5807 Digital Control 5847.1 Introduction 5847.2 Simulation of Digital Controllers 5857.3 Discretization of Continuous Controllers 5887.4 Modified Continuous Design 5987.5 Implementation Considerations 6117.6 Summary 619References 620Problems 6208 Modeling and Simulation of Miniature Aerial Vehicles 6238.1 Introduction 6238.2 Propeller/Rotor Forces and Moments 6308.3 Modeling Rotor Flapping 6408.4 Motor Modeling 6458.5 Small Aerobatic Airplane Model 6488.6 Quadrotor Model 6548.7 Small Helicopter Model 6558.8 Summary 660References 661Problems 6619 Adaptive Control with Application to Miniature Aerial Vehicles 6649.1 Introduction 6649.2 Model Reference Adaptive Control Based On Dynamic Inversion 6659.3 Neural Network Adaptive Control 6689.4 Limited Authority Adaptive Control 6749.5 Neural Network Adaptive Control Example 6809.6 Summary 709References 709Problems 711Appendix A F-16 Model 714Appendix B Software 723Index 733

The book retains its original chapter subject skeleton with the titles slightly changed and as mentioned has two new chapters added, in total it is some 150 pages longer than the original. This is not however a simple graft of new material onto the original book. Many of the chapters have been rewritten so that even where much the same material is covered, it is more detailed and augmented, whilst at the same time maintaining a consistent uniform style across the whole book....In conclusion this new edition is a significant update of a popular text...(The Aeronautical Journal- January 2017)