Rama K. Yedavalli

Flight Dynamics and Control of Aero and Space Vehicles (eBook, PDF)

• Format: PDF

Produktbeschreibung

Flight Vehicle Dynamics and Control Rama K. Yedavalli, The Ohio State University, USA A comprehensive textbook which presents flight vehicle dynamics and control in a unified framework Flight Vehicle Dynamics and Control presents the dynamics and control of various flight vehicles, including aircraft, spacecraft, helicopter, missiles, etc, in a unified framework. It covers the fundamental topics in the dynamics and control of these flight vehicles, highlighting shared points as well as differences in dynamics and control issues, making use of the 'systems level' viewpoint. The book begins with the derivation of the equations of motion for a general rigid body and then delineates the differences between the dynamics of various flight vehicles in a fundamental way. It then focuses on the dynamic equations with application to these various flight vehicles, concentrating more on aircraft and spacecraft cases. Then the control systems analysis and design is carried out both from transfer function, classical control, as well as modern, state space control points of view. Illustrative examples of application to atmospheric and space vehicles are presented, emphasizing the 'systems level' viewpoint of control design. Key features: * Provides a comprehensive treatment of dynamics and control of various flight vehicles in a single volume. * Contains worked out examples (including MATLAB examples) and end of chapter homework problems. * Suitable as a single textbook for a sequence of undergraduate courses on flight vehicle dynamics and control. The book is essential reading for undergraduate students in mechanical and aerospace engineering, engineers working on flight vehicle control, and researchers from other engineering backgrounds working on related topics.

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Produktdetails

• Verlag: Wiley-Scrivener
• Seitenzahl: 560
• Erscheinungstermin: 1. November 2019
• Englisch
• ISBN-13: 9781118934425
• Artikelnr.: 58260617

Autorenporträt

Rama K. Yedavalli is a Professor in the Department of Mechanical and Aerospace Engineering at Ohio State University. His research interests include systems level robust stability analysis and control design for uncertain dynamical systems with applications to mechanical and aerospace systems. He also works on robust control, distributed control, adaptive control, hybrid systems control and control of time delay systems with applications to mechanical and aerospace systems.

Inhaltsangabe

Preface xxi

Perspective of the Book xxix

Part I Flight Vehicle Dynamics 1

Roadmap to Part I 2

1 An Overview of the Fundamental Concepts of Modeling of a Dynamic System 5

1.1 Chapter Highlights 5

1.2 Stages of a Dynamic System Investigation and Approximations 5

1.3 Concepts Needed to Derive Equations of Motion 8

1.4 Illustrative Example 15

1.5 Further Insight into Absolute Acceleration 20

1.6 Chapter Summary 20

1.7 Exercises 21

Bibliography 22

2 Basic Nonlinear Equations of Motion in Three Dimensional Space 23

2.1 Chapter Highlights 23

2.2 Derivation of Equations of Motion for a General Rigid Body 23

2.3 Specialization of Equations of Motion to Aero (Atmospheric) Vehicles 32

2.4 Specialization of Equations of Motion to Spacecraft 43

2.5 Flight Vehicle DynamicModels in State Space Representation 52

2.6 Chapter Summary 58

2.7 Exercises 58

Bibliography 60

3 Linearization and Stability of Linear Time Invariant Systems 61

3.1 Chapter Highlights 61

3.2 State Space Representation of Dynamic Systems 61

3.3 Linearizing a Nonlinear State Space Model 63

3.4 Uncontrolled, Natural Dynamic Response and Stability of First and Second Order Linear Dynamic Systems with State Space Representation 66

3.5 Chapter Summary 73

3.6 Exercises 74

Bibliography 75

4 Aircraft Static Stability and Control 77

4.1 Chapter Highlights 77

4.2 Analysis of Equilibrium (Trim) Flight for Aircraft: Static Stability and Control 77

4.3 Static Longitudinal Stability 79

4.4 Stick Fixed Neutral Point and CG Travel Limits 86

4.5 Static Longitudinal Control with Elevator Deflection 92

4.6 Reversible Flight Control Systems: Stick Free, Stick Force Considerations 99

4.7 Static Directional Stability and Control 105

4.8 Engine Out Rudder/Aileron Power Determination: Minimum Control Speed, VMC 107

4.9 Chapter Summary 111

4.10 Exercises 111

Bibliography 114

5 Aircraft Dynamic Stability and Control via Linearized Models 117

5.1 Chapter Highlights 117

5.2 Analysis of Perturbed Flight from Trim: Aircraft Dynamic Stability and Control 117

5.3 Linearized Equations of Motion in Terms of Stability Derivatives For the Steady, Level Equilibrium Condition 122

5.4 State Space Representation for Longitudinal Motion and Modes of Approximation 124

5.5 State Space Representation for Lateral/Directional Motion and Modes of Approximation 131

5.6 Chapter Summary 138

5.7 Exercises 139

Bibliography 140

6 Spacecraft Passive Stabilization and Control 143

6.1 Chapter Highlights 143

6.2 Passive Methods for Satellite Attitude Stabilization and Control 143

6.3 Stability Conditions for Linearized Models of Single Spin Stabilized Satellites 146

6.4 Stability Conditions for a Dual Spin Stabilized Satellite 149

6.5 Chapter Summary 151

6.6 Exercises 152

Bibliography 152

7 Spacecraft Dynamic Stability and Control via Linearized Models 155

7.1 Chapter Highlights 155

7.2 Active Control: Three Axis Stabilization and Control 155

7.3 Linearized Translational Equations of Motion for a Satellite in a Nominal Circular Orbit for Control Design 158

7.4 Linearized Rotational (Attitude) Equations of Motion for a Satellite in a Nominal Circular Orbit for Control Design 160

7.5 Open Loop (Uncontrolled Motion)

Rezensionen

"Different from the most existing books on the subject, this book covers not only aircraft but also spacecraft via the frequency-domain transfer function based control theory as well as the time-domain state space based control theory, thereby providing important concepts of flight dynamics and control in an integral way, which is crucial for students in aerospace engineering who want to know how flight vehicles fly as intended."
Inseok Hwang, PhD, Professor, Aeronautics and Astronautics
School of Aeronautics and Astronautics, Purdue University

"The book is a "must have" for students as well as practicing engineers. I think that the book is unique and it is a complete guideline for two undergraduate courses. It is extremely well written, and it shows the high level scientific background of its author."
Mario Innocenti, PhD, Full Professor of Aerospace Dynamics and Control
Department of Information Engineering, University of Pisa