Spacecraft Dynamics and Control

Anton H. de Ruiter 지음

Wiley 2012년 12월 05일 출간

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Provides the basics of spacecraft orbital dynamics plus attitude dynamics and control, using vectrix notationSpacecraft 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 subjectFills 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 alikeDelivers an outstanding resource for aerospace engineering students, and all those involved in the technical aspects of design and engineering in the space sectorContains numerous illustrations to accompany the written text. Problems are included to apply and extend the material in each chapt

목차

Preface xvii1 Kinematics 11.1 Physical Vectors 11.2 Reference Frames and Physical Vector Coordinates 61.3 Rotation Matrices 111.4 Derivatives of Vectors 321.5 Velocity and Acceleration 411.6 More Rigorous Definition of Angular Velocity 42Notes 44References 452 Rigid Body Dynamics 472.1 Dynamics of a Single Particle 472.2 Dynamics of a System of Particles 492.3 Rigid Body Dynamics 522.4 The Inertia Matrix 562.5 Kinetic Energy of a Rigid Body 60Notes 63References 633 The Keplerian Two-Body Problem 653.1 Equations of Motion 653.2 Constants of the Motion 673.3 Shape of a Keplerian Orbit 693.4 Kepler&'s Laws 803.5 Time of Flight 833.6 Orbital Elements 893.7 Orbital Elements given Position and Velocity 923.8 Position and Velocity given Orbital Elements 94Notes 98References 984 Preliminary Orbit Determination 994.1 Orbit Determination from Three Position Vectors 994.2 Orbit Determination from Three Line-of-Sight Vectors 1034.3 Orbit Determination from Two Position Vectors and Time (Lambert&'s Problem) 109Notes 114References 1145 Orbital Maneuvers 1155.1 Simple Impulsive Maneuvers 1155.2 Coplanar Maneuvers 1165.3 Plane Change Maneuvers 1235.4 Combined Maneuvers 1255.5 Rendezvous 127Notes 128Reference 1286 Interplanetary Trajectories 1296.1 Sphere of Influence 1296.2 Interplanetary Hohmann Transfers 1336.3 Patched Conics 1376.4 Planetary Flyby 1436.5 Planetary Capture 145Notes 146References 1477 Orbital Perturbations 1497.1 Special Perturbations 1507.1.1 Cowell&'s Method 1517.2 General Perturbations 1547.3 Gravitational Perturbatio

출판사 서평

“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)

작가정보

저자(글) Anton H. de Ruiter