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Aircraft control and simulation : dynamics, controls design, and autonomous systems
Stevens, Brian L.,
- ISBN:9781119174882
- ISBN:1119174880
- ISBN:9781118870990
- ISBN:1118870999
- ISBN:9781118870983
- ISBN:1118870980
- Call Number : TL 678 .S74 2015
- Main Entry: Stevens, Brian L., 1939-
- Title:Aircraft control and simulation : dynamics, controls design, and autonomous systems [electronic resource] / Brian L. Stevens, Frank L. Lewis, Eric N. Johnson.
- Edition:3rd ed.
- Publisher:New Jersey : John Wiley & Sons, 2015.
- Physical Description:xii, 749p.: ill
- Notes:Includes bibliographical references and index
- Subject:Airplanes -- Control systems.
- Added Entry:Lewis, Frank L.
- Added Entry:Johnson, Eric N., 1970-
Aircraft control and simulation : dynamics, controls design
- Cover
- Title Page
- Copyright
- Contents
- Preface
- Chapter 1 The Kinematics and Dynamics of Aircraft Motion
- 1.1 Introduction
- 1.2 Vector Operations
- 1.3 Matrix Operations on Vector Coordinates
- 1.4 Rotational Kinematics
- 1.5 Translational Kinematics
- 1.6 Geodesy, Coordinate Systems,~Gravity
- Introduction
- The Shape of the Earth, WGS-84
- Frames, Earth-Centered Coordinates, Latitude and Longitude
- Local Coordinate Systems
- Radii of Curvature
- Trigonometric Relationships for the Spheroid
- Cartesian/Polar Coordinate Conversions
- Earth-Related Coordinate Transformations
- Gravitation and Gravity
- Gravitation and Accelerometers
- 1.7 Rigid-Body Dynamics
- 1.8 Advanced Topics
- References
- Problems
- Chapter 2 Modeling the Aircraft
- 2.1 Introduction
- 2.2 Basic Aerodynamics
- 2.3 Aircraft Forces And Moments
- Definition of Axes and Angles
- Definition of Forces and Moments
- Force and Moment Coefficients
- The Aerodynamic Derivatives
- Aerodynamic Coefficient Measurement and Estimation
- Component Buildup
- Drag Coefficient, CD
- Lift Coefficient, CL
- Sideforce Coefficient, CY
- Rolling Moment
- Control Effects on Rolling Moment
- Pitching Moment
- Control Effects on Pitching Moment
- Yawing Moment
- Control Effects on Yawing Moment
- Data Handling
- 2.4 Static Analysis
- 2.5 The Nonlinear Aircraft Model
- 2.6 Linear Models And The Stability Derivatives
- 2.7 Summary
- References
- Problems
- Chapter 3 Modeling, Design, and Simulation Tools
- Chapter 4 Aircraft Dynamics and Classical Control Design
- 4.1 Introduction
- 4.2 Aircraft Rigid-Body Modes
- Algebraic Derivation of Longitudinal Transfer Functions and Modes
- The Short-Period Approximation
- The Phugoid Approximation
- Accuracy of the Short-Period and Phugoid Approximations
- Pitch Stability
- Algebraic Derivation of Lateral-Directional Transfer Functions
- The Dutch Roll Approximation
- The Spiral and Roll Subsidence Approximations
- Spiral Stability
- Accuracy of the Lateral-Mode Approximations
- Mode Variation from the Nonlinear Model
- 4.3 The Handling-Qualities Requirements
- 4.4 Stability Augmentation
- 4.5 Control Augmentation Systems
- 4.6 Autopilots
- 4.7 Nonlinear Simulation
- 4.8 Summary
- References
- Problems
- Chapter 5 Modern Design Techniques
- Chapter 6 Robustness and Multivariable Frequency-Domain Techniques
- Chapter 7 Digital Control
- Chapter 8 Modeling and Simulation of Miniature Aerial Vehicles
- Chapter 9 Adaptive Control With Application to Miniature Aerial Vehicles
- Appendix A F-16 Model
- Appendix B Software
- Index
- EULA