Dynamics of Tethered Satellites and Space Elevators
- 1 Edición - 1 de febrero de 2027
- Última edición
- Autores: Arun K. Misra, Stephen Cohen
- Idioma: Inglés
Dynamics of Tethered Satellites and Space Elevators provides a comprehensive overview of the current state of knowledge of tethered space systems, including their potential applic… Leer más
Descripción
Descripción
An entire section of chapters on the dynamics of partial and full space elevators concludes the volume.
Puntos claves
Puntos claves
- Builds on from basic fundamentals to advanced, in-depth coverage of tethered space systems
- Includes mathematical modeling in each chapter
- Considers several applications – from attitude stabilization, momentum exchange, to in-orbit maintenance (such as fueling service, orbit maneuvering, and space debris removal), and many more
- Discusses past missions in detail and broaches future ones, including zero-emission lift of cargo to space
De interès para
De interès para
Índice
Índice
1.1 Motivation for Space Tethers and Space Elevators
1.2 History of the Tether Concept
1.3 Description of the Tether Missions Flown
1.4 Conclusions
Part I: Space Tethers and Tethered Satellites
2. Dynamics of Rigid Tethered Satellite Systems
2.1 Constant Length Case
2.2 Variable Length Case
2.3 State Space Trajectories
2.4 Conclusions
3. Elastic Oscillations of Space Tethers
3.1 Longitudinal Oscillations of a Vertical Fixed Length Tether
3.2 Transverse Oscillations of a Vertical Fixed Length Tether
3.3 Transverse Oscillations of Variable Length Tethers
3.4 Conclusions
4. Control of Tethered Satellite Systems
4.1 Tension Control
4.2 Length Rate Control
4.3 Thruster Control and Offset Control
4.4 Conclusions
5. Tethered Multibody Systems
5.1 Three-Body Tethered Systems
5.2 N-Body Tethered Systems
5.3 Control of Librations
5.4 Tethered Formations in Space
5.5 Conclusions
6. Tether Propulsion
6.1 Motion of System Before Payload Release (consider condensing?)
6.2 Determination of Payload Orbit After Release
6.3 Special Cases
6.4 Conclusions
7. Removal of Space Debris
7.1 Dynamics Model of a Tethered Debris Removal System
7.2 Low Thrust Case
7.3 Planar Librational Motion of the Debris Removal System in a Circular Orbit
7.4 Conclusions
Part II: Space Elevators
8. Very Long Tethers
8.1 Steady State Equilibrium Analysis of a Very Long Tether
8.2 Description of the Partial Elevator System
8.3 Dynamics Model
8.4 Conclusions
9. Space Elevator Description
9.1 Design of the Nominal System
9.2 Comparison with Space Tethers
9.3 Orbits Available via Payload Release
9.4 Sizing of Components
9.5 Conclusions
10. Elastic Oscillations of Space Elevator
10.1 Wave Speed of Tether
10.2 Equations of Motion of the System
10.3 Analysis of the Equations of Motion
10.4 Conclusions
11. Climber Effects on Space Elevator Tether
11.1 Stationary Climber Effects
11.2 Dynamic Climber Effects
11.3 Dynamic Response to Payload Release
11.4 Conclusions
12. Conclusions
12.1 Space Tethers
12.2 Space Elevators
Detalles del producto
Detalles del producto
- Edición: 1
- Última edición
- Publicado: 1 de febrero de 2027
- Idioma: Inglés
Sobre los autores
Sobre los autores
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Arun K. Misra
Arun K. Misra is the Thomas Workman Professor in the Department of Mechanical Engineering at McGill University in Montreal, Canada. He has made extensive research contributions in the areas of dynamics and control of tethered satellites, space debris, space robotics, space structures, and space elevators. He is a Fellow of the American Institute of Aeronautics and Astronautics as well as of the American Astronautical Society. He has been elected to the Canadian Academy of Engineering and to the International Academy of Astronautics. He has received numerous awards including the Dirk Brouwer Award from the American Astronautical Society. He is a Co-Editor of the journal Acta Astronautica published by Elsevier.
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