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Author by : Vladimir Vasilʹevich Belet︠s︡kiĭ
Languange Used : en
Release Date : 1993
Publisher by : Univelt Incorporated
ISBN : 9780877033707
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Author by : Vladimir Aslanov
Languange Used : en
Release Date : 2012-10-16
Publisher by : Elsevier
ISBN : 9780857096005
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. The main advantage of this technology is the simplicity, profitability and ecological compatibility: space tethers allow the execution of various manoeuvers in orbit without costs of jet fuel due to the use of gravitational and electromagnetic fields of the Earth. This book will acquaint the reader with the modern state of the space tether’s dynamics, with specific attention on the research projects of the nearest decades. This book presents the most effective mathematical models and the methods used for the analysis and prediction of space tether systems’ motion; attention is also given to the influence of the tether on spacecraft’s motion, to emergencies and chaotic modes. Written by highly qualified experts with practical experience in both the fields of mechanics of space flight, and in the teaching Contains detailed descriptions of mathematical models and methods, and their features, that allow the application of the material of the book to the decision of concrete practical tasks New approaches to the decision of problems of space flight mechanics are offered, and new problems are posed...
Dynamics Of Space Tether Systems
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Author by : Vladimir Vasilʹevich Belet︠s︡kiĭ
Languange Used : en
Release Date : 1993-01-01
Publisher by : Amer Astronautical Society
ISBN : 0877033714
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The Impact Of Atmospheric Models On The Dynamics Of Space Tether Systems
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Author by : Vishal Siewnarine
Languange Used : en
Release Date : 2015
Publisher by :
ISBN : OCLC:1362901732
Space debris has become an increasingly larger concern for aerospace travel and exploration. One idea to control the space debris population is to de-orbit defunct satellites using a space tether system. A space tether system is often made up of three parts: the main satellite, the tether and the sub-satellite. The tether connects the main satellite and the sub-satellite. Space tether systems make use of the Lorentz force as an electrodynamic drag for de-orbit. We use an established model of a space tether system to observe how satellites de-orbit. This model was constructed in MATLAB (Simulink) and uses the 1976 U.S. Standard Atmosphere. However, we wish to investigate how the model behaves using newer and more accurate atmospheric models, namely, the Jacchia-Bowman 2008 model and the Drag Temperature Model 2013. We also investigate the effect of controlling the tether's libration energy under the three aforementioned atmospheric models....
Dynamics Of Space Tether Systems
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Author by : Vladimir Vasilevič Beleckij (Mathématicien, Russie)
Languange Used : en
Release Date : 1993
Publisher by :
ISBN : 0877033714
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Dynamics Of Tethered Space Systems
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Author by : Hans Troger
Languange Used : en
Release Date : 2010-04-29
Publisher by : CRC Press
ISBN : 9781439836866
During many of the earliest American and Russian space missions, experiments were performed using cables to connect people and objects to spacecraft in orbit. These attempts generated considerable information about the formation of tethered systems and basic problems with tether orientation and gravity-gradient stabilization. During the 1970s, inte...
Deployment Dynamic Of Space Tether Systems
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Author by :
Languange Used : en
Release Date : 2004
Publisher by :
ISBN : OCLC:656419252
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Dynamics And Stability Of Spinning Flexible Space Tether Systems
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Author by : George Tyc
Languange Used : en
Release Date : 1998
Publisher by :
ISBN : OCLC:184805532
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Dynamics And Stability Of Spinning Flexible Space Tether Systems
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Author by :
Languange Used : en
Release Date : 1998
Publisher by :
ISBN : OCLC:654193307
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