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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.
* Accompanied by a website that includes additional problems and a solutions manual.
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.
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.
* Accompanied by a website that includes additional problems and a solutions manual.
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.
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.
* Accompanied by a website that includes additional problems and a solutions manual.
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.
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.
* Accompanied by a website that includes additional problems and a solutions manual.
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.
Inhaltsverzeichnis
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)
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)
Details
| Erscheinungsjahr: | 2019 |
|---|---|
| Fachbereich: | Fertigungstechnik |
| Genre: | Technik |
| Rubrik: | Naturwissenschaften & Technik |
| Medium: | Buch |
| Seiten: | 560 |
| Inhalt: | 560 S. |
| ISBN-13: | 9781118934456 |
| ISBN-10: | 1118934458 |
| Sprache: | Englisch |
| Herstellernummer: | 1W118934450 |
| Autor: | Yedavalli, Rama K. |
| Auflage: | 1. Auflage |
| Hersteller: |
Wiley
Wiley & Sons |
| Maße: | 251 x 170 x 45 mm |
| Von/Mit: | Rama K. Yedavalli |
| Erscheinungsdatum: | 05.12.2019 |
| Gewicht: | 1,127 kg |
Inhaltsverzeichnis
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)
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)
Details
| Erscheinungsjahr: | 2019 |
|---|---|
| Fachbereich: | Fertigungstechnik |
| Genre: | Technik |
| Rubrik: | Naturwissenschaften & Technik |
| Medium: | Buch |
| Seiten: | 560 |
| Inhalt: | 560 S. |
| ISBN-13: | 9781118934456 |
| ISBN-10: | 1118934458 |
| Sprache: | Englisch |
| Herstellernummer: | 1W118934450 |
| Autor: | Yedavalli, Rama K. |
| Auflage: | 1. Auflage |
| Hersteller: |
Wiley
Wiley & Sons |
| Maße: | 251 x 170 x 45 mm |
| Von/Mit: | Rama K. Yedavalli |
| Erscheinungsdatum: | 05.12.2019 |
| Gewicht: | 1,127 kg |
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