Spacecraft Dynamics and Control - An Introduction

Klappentext "This unique volume is unmatched in breadth and depth, providing detailed coverage of topics ranging from orbital dynamics to formation flight to attitude dynamics to control and navigation. The authors bring a fresh, unified perspective to the field with a groundbreaking textbook that is destined to become the favorite of students at all levels."--Dennis S. Bernstein, Aerospace Engineering Department, The University of Michigan, USAThis textbook presents a rigorous, yet practical and accessible introduction to the fundamentals of spacecraft dynamics and control. Written for engineering students and practicing engineers with a basic background in mathematics and mechanics, it is suitable for both upper-year undergraduate courses and first graduate courses, as well as self study. The material covered is comprehensive; all the pertinent aspects of a spacecraft mission including orbital dynamics, attitude dynamics, and control are discussed. Additionally, advanced topics such as low-thrust trajectory analysis, nonlinear spacecraft attitude control, and navigation techniques are introduced. A unique feature of this textbook is the presentation of classical control systems design techniques using spacecraft attitude control as the motivating control design objective.Key features:* A comprehensive reference on the fundamentals of orbital dynamics, attitude dynamics, and control* Classical control systems design is explained and motivated by the control of a spacecraft's attitude* Practical aspects of spacecraft dynamics and control are discussed, included sensor and actuator operation, digital implementation of controllers, and the effects of unmodelled dynamics* Numerous illustrations accompany the text, helping the reader to better understand the material Zusammenfassung Provides the basics of spacecraft orbital dynamics plus attitude dynamics and control, using vectrix notation Spacecraft Dynamics and Control: An Introduction presents the fundamentals of classical control in the context of spacecraft attitude control. Inhaltsverzeichnis Preface xvii1 Kinematics 1Notes 44References 452 Rigid Body Dynamics 47Notes 63References 633 The Keplerian Two-Body Problem 65Notes 98References 984 Preliminary Orbit Determination 99Notes 114References 1145 Orbital Maneuvers 115Notes 128Reference 1286 Interplanetary Trajectories 129Notes 146References 1477 Orbital Perturbations 149Notes 180References 1818 Low Thrust Trajectory Analysis and Design 183Notes 188References 1889 Spacecraft Formation Flying 189Notes 207Reference 20710 The Restricted Three-Body Problem 209Notes 218References 21811 Introduction to Spacecraft Attitude Stabilization 21912 Disturbance Torques on a Spacecraft 227Notes 234Reference 23413 Torque-Free Attitude Motion 235Notes 245References 24514 Spin Stabilization 247Notes 253References 25315 Dual-Spin Stabilization 255Notes 266References 26616 Gravity-Gradient Stabilization 267Notes 277References 27717 Active Spacecraft Attitude Control 279JWST251-FM JWST251-De-Ruiter Printer: Yet to Come November 2, 2012 14:18 Trim: 244mm×168mmviiiContents575859Notes63References 633 The Keplerian Two-Body Problem 6567676872838488898990Notes98References 984 Preliminary Orbit Determination 99Problem) 109110Notes114References 1145 Orbital Maneuvers 115118120FOR SCREEN VIEWING IN DART ONLYJWST251-FM JWST251-De-Ruiter Printer: Yet to Come November 2, 2012 14:18 Trim: 244mm×168mmContentsixNotes128Reference 1286 Interplanetary Trajectories 129139141Notes146References 1477 Orbital Perturbations 1491511512163J2on the Orbital Elements 164168169Notes180References 1818 Low Thrust Trajectory Analysis and Design 183Notes188References 1889 Spacecraft Formation Flying 1891951...

Sommario

Preface xvii
 
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
 
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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
 
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198
 
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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
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Relazione

"In conclusion, this book covers a broad range of areas - including some more in-depth content (stabilisation techniques, practical design issues) - and is best used as an introductory text to the field for latter year undergraduates." ( The Aeronautical Journal , 1 November 2014)

"Overall, this book provides a good, comprehensive examination of the fundamentals of translational and rotational dynamics, determination, and control of spacecraft. Summing Up: Recommended. All academic and professional aerospace engineering collections." ( Choice , 1 September 2013)

Dettagli sul prodotto

• Autori: Christopher Damaren, Damaren Christopher, Anton H. de Ruiter, Anton H. (Ryerson University De Ruiter, de Ruiter Anton H., James R. Forbes, Forbes James R.
• Editore: Wiley, John and Sons Ltd
• Lingue: Inglese
• Formato: Copertina rigida
• Pubblicazione: 04.01.2013
• EAN: 9781118342367
• ISBN: 978-1-118-34236-7
• Pagine: 592
• Categorie: Scienze naturali, medicina, informatica, tecnica > Tecnica > Tecnica aerospaziale; Maschinenbau, Regelungstechnik, Raumfahrttechnik, Mechanical Engineering, Electrical & Electronics Engineering, Elektrotechnik u. Elektronik, Aeronautic & Aerospace Engineering, Luft- u. Raumfahrttechnik, Control Systems Technology