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Orbital mechanics and formation flying : a digital control perspective /
Aimed at students, faculty and professionals in the aerospace field, this book provides practical information on the development, analysis, and control of a single and/or multiple spacecraft in space. This book is divided into two major sections: single and multiple satellite motion. The first secti...
| Clasificación: | Libro Electrónico |
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| Autor principal: | |
| Otros Autores: | |
| Formato: | Electrónico eBook |
| Idioma: | Inglés |
| Publicado: |
Cambridge ; Philadelphia :
Woodhead Pub.,
2011.
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| Colección: | Woodhead Publishing in mechanical engineering.
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| Temas: | |
| Acceso en línea: | Texto completo |
Tabla de Contenidos:
- Cover; Orbital mechanics and formation flying: A digital control approach; Copyright; Dedication; Contents; List of figures; List of tables; List of symbols; Acknowledgements; Preface; About the authors; 1 Introduction; 1.1 Introduction to the book; 1.2 Book division; 1.3 References; 2 Two body orbital motion; 2.1 Introduction to orbital motion; 2.2 Constraints and generalized coordinates; 2.3 Lagrange's equation; 2.4 System of particles; 2.5 Two body orbital motion problem; 2.6 Orbital equations of motion; 2.7 Energy and velocity of orbiting bodies; 2.8 Escape velocity.
- 2.9 Earth Coordinate Inertial (ECI) system2.10 Period of an orbit; 2.11 Development of Kepler's equation; 2.12 Suggested problems; 2.13 References; 3 Orbital perturbations in the two body motion; 3.1 Introduction to disturbance effects; 3.2 Lagrange planetary equations; 3.3 Perturbation due to the earth oblateness; 3.4 The near-Earth atmosphere effects; 3.5 Solar radiation pressure force; 3.6 Other disturbance effects; 3.7 Suggested problems; 3.8 References; 4 Frame rotations and quaternions; 4.1 Introduction to rotations and quaternions; 4.2 Two-dimensional frame rotations.
- 4.3 Three-dimensional frame rotations4.4 Example of frame rotations; 4.5 Quaternion defi nition and rotations; 4.6 Quaternion to Euler angle relations; 4.7 Suggested problems; 4.8 References; 5 Rigid body motion; 5.1 Introduction to attitude dynamics; 5.2 Rate of change of a vector; 5.3 Moment of inertia; 5.4 Principal moments of inertia; 5.5 Energy formulation; 5.6 Rate of change of a quaternion; 5.7 Ares V equations of motion; 5.8 Suggested problems; 5.9 References; 6 Environmental and actuator torques; 6.1 Introduction to torque formulation; 6.2 Environmental torques.
- 6.3 Actuator (or control) torques6.4 Suggested problems; 6.5 References; 7 Continuous and digital control systems; 7.1 Introduction to methods of designing continuous and discrete control systems; 7.2 Ares V equations of motion for first stage flight; 7.3 Continuous control formulation; 7.4 Discrete control formulation; 7.5 Adaptive and intelligent controls; 7.6 Suggested problems; 7.7 References; 8 Example; 8.1 Introduction to examples in spacecraft attitude dynamics and control; 8.2 Nanosatellite problem definition; 8.3 B-dot controller for fast corrections.
- 8.4 Linear quadratic regulator for attitude correction8.5 Linear quadratic regulator control weight design; 8.6 Suggested problems; 8.7 References; 9 Formation flying; 9.1 Introduction to formation flying; 9.2 Tschauner-Hempel formulation; 9.3 Clohessy-Wiltshire formulation; 9.4 Earth oblateness and solar effects in formation flying; 9.5 Lawden solution; 9.6 Discrete optimal control problem for formation flying; 9.7 Formation flying controller implementation; 9.8 Suggested problems; 9.9 References; 10 Deployment procedure for a constellation; 10.1 Introductory comments.