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Spacecraft Dynamics and Control: An Introduction presents the fundamentals of classical control in the context of spacecraft attitude control. This approach is particularly beneficial for the training of students in both of the subjects of classical control as well as its application to spacecraft attitude control. By using a physical system (a spacecraft) that the reader can visualize (rather than arbitrary transfer functions), it is easier to grasp the motivation for why topics in control theory are important, as well as the theory behind them. The entire treatment of both orbital and attitude dynamics makes use of vectrix notation, which is a tool that allows the user to write down any vector equation of motion without consideration of a reference frame. This is particularly suited to the treatment of multiple reference frames. Vectrix notation also makes a very clear distinction between a physical vector and its coordinate representation in a reference frame. This is very important in spacecraft dynamics and control problems, where often multiple coordinate representations are used (in different reference frames) for the same physical vector.
* Provides an accessible, practical aid for teaching and self-study with a layout enabling a fundamental understanding of the subject
* Fills a gap in the existing literature by providing an analytical toolbox offering the reader a lasting, rigorous methodology for approaching vector mechanics, a key element vital to new graduates and practicing engineers alike
* Delivers an outstanding resource for aerospace engineering students, and all those involved in the technical aspects of design and engineering in the space sector
* Contains numerous illustrations to accompany the written text. Problems are included to apply and extend the material in each chapter
Essential reading for graduate level aerospace engineering students, aerospace professionals, researchers and engineers.
Spacecraft Dynamics and Control: An Introduction presents the fundamentals of classical control in the context of spacecraft attitude control. This approach is particularly beneficial for the training of students in both of the subjects of classical control as well as its application to spacecraft attitude control. By using a physical system (a spacecraft) that the reader can visualize (rather than arbitrary transfer functions), it is easier to grasp the motivation for why topics in control theory are important, as well as the theory behind them. The entire treatment of both orbital and attitude dynamics makes use of vectrix notation, which is a tool that allows the user to write down any vector equation of motion without consideration of a reference frame. This is particularly suited to the treatment of multiple reference frames. Vectrix notation also makes a very clear distinction between a physical vector and its coordinate representation in a reference frame. This is very important in spacecraft dynamics and control problems, where often multiple coordinate representations are used (in different reference frames) for the same physical vector.
* Provides an accessible, practical aid for teaching and self-study with a layout enabling a fundamental understanding of the subject
* Fills a gap in the existing literature by providing an analytical toolbox offering the reader a lasting, rigorous methodology for approaching vector mechanics, a key element vital to new graduates and practicing engineers alike
* Delivers an outstanding resource for aerospace engineering students, and all those involved in the technical aspects of design and engineering in the space sector
* Contains numerous illustrations to accompany the written text. Problems are included to apply and extend the material in each chapter
Essential reading for graduate level aerospace engineering students, aerospace professionals, researchers and engineers.
1 Kinematics 1
Notes 44
References 45
2 Rigid Body Dynamics 47
Notes 63
References 63
3 The Keplerian Two-Body Problem 65
Notes 98
References 98
4 Preliminary Orbit Determination 99
Notes 114
References 114
5 Orbital Maneuvers 115
Notes 128
Reference 128
6 Interplanetary Trajectories 129
Notes 146
References 147
7 Orbital Perturbations 149
Notes 180
References 181
8 Low Thrust Trajectory Analysis and Design 183
Notes 188
References 188
9 Spacecraft Formation Flying 189
Notes 207
Reference 207
10 The Restricted Three-Body Problem 209
Notes 218
References 218
11 Introduction to Spacecraft Attitude Stabilization 219
12 Disturbance Torques on a Spacecraft 227
Notes 234
Reference 234
13 Torque-Free Attitude Motion 235
Notes 245
References 245
14 Spin Stabilization 247
Notes 253
References 253
15 Dual-Spin Stabilization 255
Notes 266
References 266
16 Gravity-Gradient Stabilization 267
Notes 277
References 277
17 Active Spacecraft Attitude Control 279
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viii
Contents
57
58
59
Notes
63
References 63
3 The Keplerian Two-Body Problem 65
67
67
68
72
83
84
88
89
89
90
Notes
98
References 98
4 Preliminary Orbit Determination 99
Problem) 109
110
Notes
114
References 114
5 Orbital Maneuvers 115
118
120
FOR SCREEN VIEWING IN DART ONLY
JWST251-FM JWST251-De-Ruiter Printer: Yet to Come November 2, 2012 14:18 Trim: 244mm
×
168mm
Contents
ix
Notes
128
Reference 128
6 Interplanetary Trajectories 129
139
141
Notes
146
References 147
7 Orbital Perturbations 149
151
151
2
163
J
2
on the Orbital Elements 164
168
169
Notes
180
References 181
8 Low Thrust Trajectory Analysis and Design 183
Notes
188
References 188
9 Spacecraft Formation Flying 189
195
195
FOR SCREEN VIEWING IN DART ONLY
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×
168mm
x
Contents
198
200
202
203
204
207
Notes
207
Reference 207
10 The Restricted Three-Body Problem 209
211
212
213
215
216
218
Notes
218
References 218
11 Introduction to Spacecraft Attitude Stabilization 219
220
221
224
<
| Erscheinungsjahr: | 2013 |
|---|---|
| Fachbereich: | Fertigungstechnik |
| Genre: | Technik |
| Rubrik: | Naturwissenschaften & Technik |
| Medium: | Buch |
| Inhalt: | 588 S. |
| ISBN-13: | 9781118342367 |
| ISBN-10: | 1118342364 |
| Sprache: | Englisch |
| Herstellernummer: | 1W118342360 |
| Autor: |
de Ruiter, Anton H.
Damaren, Christopher Forbes, James R. |
| Auflage: | 1. Auflage |
| Hersteller: |
Wiley
Wiley & Sons |
| Maße: | 245 x 173 x 32 mm |
| Von/Mit: | Anton H. de Ruiter (u. a.) |
| Erscheinungsdatum: | 04.01.2013 |
| Gewicht: | 1,028 kg |
1 Kinematics 1
Notes 44
References 45
2 Rigid Body Dynamics 47
Notes 63
References 63
3 The Keplerian Two-Body Problem 65
Notes 98
References 98
4 Preliminary Orbit Determination 99
Notes 114
References 114
5 Orbital Maneuvers 115
Notes 128
Reference 128
6 Interplanetary Trajectories 129
Notes 146
References 147
7 Orbital Perturbations 149
Notes 180
References 181
8 Low Thrust Trajectory Analysis and Design 183
Notes 188
References 188
9 Spacecraft Formation Flying 189
Notes 207
Reference 207
10 The Restricted Three-Body Problem 209
Notes 218
References 218
11 Introduction to Spacecraft Attitude Stabilization 219
12 Disturbance Torques on a Spacecraft 227
Notes 234
Reference 234
13 Torque-Free Attitude Motion 235
Notes 245
References 245
14 Spin Stabilization 247
Notes 253
References 253
15 Dual-Spin Stabilization 255
Notes 266
References 266
16 Gravity-Gradient Stabilization 267
Notes 277
References 277
17 Active Spacecraft Attitude Control 279
JWST251-FM JWST251-De-Ruiter Printer: Yet to Come November 2, 2012 14:18 Trim: 244mm
×
168mm
viii
Contents
57
58
59
Notes
63
References 63
3 The Keplerian Two-Body Problem 65
67
67
68
72
83
84
88
89
89
90
Notes
98
References 98
4 Preliminary Orbit Determination 99
Problem) 109
110
Notes
114
References 114
5 Orbital Maneuvers 115
118
120
FOR SCREEN VIEWING IN DART ONLY
JWST251-FM JWST251-De-Ruiter Printer: Yet to Come November 2, 2012 14:18 Trim: 244mm
×
168mm
Contents
ix
Notes
128
Reference 128
6 Interplanetary Trajectories 129
139
141
Notes
146
References 147
7 Orbital Perturbations 149
151
151
2
163
J
2
on the Orbital Elements 164
168
169
Notes
180
References 181
8 Low Thrust Trajectory Analysis and Design 183
Notes
188
References 188
9 Spacecraft Formation Flying 189
195
195
FOR SCREEN VIEWING IN DART ONLY
JWST251-FM JWST251-De-Ruiter Printer: Yet to Come November 2, 2012 14:18 Trim: 244mm
×
168mm
x
Contents
198
200
202
203
204
207
Notes
207
Reference 207
10 The Restricted Three-Body Problem 209
211
212
213
215
216
218
Notes
218
References 218
11 Introduction to Spacecraft Attitude Stabilization 219
220
221
224
<
| Erscheinungsjahr: | 2013 |
|---|---|
| Fachbereich: | Fertigungstechnik |
| Genre: | Technik |
| Rubrik: | Naturwissenschaften & Technik |
| Medium: | Buch |
| Inhalt: | 588 S. |
| ISBN-13: | 9781118342367 |
| ISBN-10: | 1118342364 |
| Sprache: | Englisch |
| Herstellernummer: | 1W118342360 |
| Autor: |
de Ruiter, Anton H.
Damaren, Christopher Forbes, James R. |
| Auflage: | 1. Auflage |
| Hersteller: |
Wiley
Wiley & Sons |
| Maße: | 245 x 173 x 32 mm |
| Von/Mit: | Anton H. de Ruiter (u. a.) |
| Erscheinungsdatum: | 04.01.2013 |
| Gewicht: | 1,028 kg |
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