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Dynamics of tethered satellite systems

Author: V S Aslanov; Alexander S Ledkov
Publisher: Cambridge, UK ; Philadelphia, PA : Woodhead, 2012.
Series: Woodhead Publishing in mechanical engineering.
Edition/Format:   Print book : EnglishView all editions and formats
Database:WorldCat
Summary:
Aimed at engineering students and professionals working in the field of mechanics of space flight, this book examines space tether systems - one of the most forward thinking directions of modern astronautics. It presents the mathematical models and the methods used for the analysis and prediction of space tether systems' motion.
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Document Type: Book
All Authors / Contributors: V S Aslanov; Alexander S Ledkov
ISBN: 9780857091567 0857091565 9780857096005 0857096001
OCLC Number: 820530313
Description: xxiv, 331 pages : illustrations ; 25 cm.
Contents: Machine generated contents note: 1. Space tether systems: review of the problem --
1.1. Application of space tether systems --
1.2. Chronology of experiments with the use of space tethers --
1.3. Materials for tether production --
1.4. Study of space tether dynamics: state of the problem --
1.5. References --
2. Mathematical models of space tether systems --
2.1. Simple models of space tether system consisting of two point masses connected by a massless tether --
2.2. Simple model of a space tether system consisting of two point masses connected by a heavy tether --
2.3. Model of a space tether system with a heavy flexible tether --
2.4. Model of a space tether system consisting of a point mass connected by a heavy tether with a rigid body --
2.5. Model of a space tether system consisting of two rigid bodies connected by a heavy elastic multipoint tether --
2.6. References --
3. Motion of a spacecraft with a tethered payload --
3.1. Mathematical model of a base spacecraft with a tethered payload --
3.2. Analytical solution in case of a slow changing of the parameters --
3.3. The approximate analytical solutions in the variables of the amplitude-phase --
3.4. Analytical solutions for small oscillations --
3.5. Estimation of the microaccelerations level on board the spacecraft --
3.6. Motion of the spacecraft with a propulsion system --
3.7. Motion of a spacecraft around its centre of mass in a circular orbit with a vertically deployed elastic tether --
3.8. References --
4. Delivery of a payload from an orbit by means of a space tether --
4.1. Tether deployment schemes --
4.2. Project YES2 --
4.3. Modelling of the YES2 tether deployment --
4.4. Abnormal situations during tether deployment --
4.5. References --
5. Use of methods of chaotic dynamics for the analysis of tether system motion --
5.1. Some elements of chaotic dynamics --
5.2. The chaotic approach in STS dynamics --
5.3. References.
Series Title: Woodhead Publishing in mechanical engineering.
Responsibility: Vladinir S. Aslanov and Alexander S. Ledkov.

Abstract:

Aimed at engineering students and professionals working in the field of mechanics of space flight, this book examines space tether systems - one of the most forward thinking directions of modern  Read more...

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