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Effects of Time Varying Moments on a Large Tethered Satellite in Orbit: Analysis for Circular and Elliptical Orbits - Softcover
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The purpose of this book is to investigate the effect of a varying moment on the rotation angle of a large tethered satellite that is orbiting a planet. Two different types of orbits were investigated: a simple circular orbit and an elliptical orbit. Cases with zero and non-zero initial angular rotation velocity were investigated as well. This investigation will assist satellite docking missions. The large rigid tethered satellite is a futuristic concept, and this investigation is meant to assist possible docking missions to the satellite. To simplify the problem, the rotation is constrained to the orbital plane.
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Effects of Time Varying Moments on a Large Tethered Satellite in Orbit
Published by
LAP LAMBERT Academic Publishing Sep 2019, 2019
ISBN 10: 3659649872
ISBN 13: 9783659649875
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Taschenbuch
Seller: BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, Germany
Seller rating 5 out of 5 stars
Taschenbuch. Condition: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -The purpose of this book is to investigate the effect of a varying moment on the rotation angle of a large tethered satellite that is orbiting a planet. Two different types of orbits were investigated: a simple circular orbit and an elliptical orbit. Cases with zero and non-zero initial angular rotation velocity were investigated as well. This investigation will assist satellite docking missions. The large rigid tethered satellite is a futuristic concept, and this investigation is meant to assist possible docking missions to the satellite. To simplify the problem, the rotation is constrained to the orbital plane. 52 pp. Englisch. Seller Inventory # 9783659649875
Quantity: 2 available
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Effects of Time Varying Moments on a Large Tethered Satellite in Orbit
Published by
LAP LAMBERT Academic Publishing, 2019
ISBN 10: 3659649872
ISBN 13: 9783659649875
New
Softcover
Seller: moluna, Greven, Germany
Seller rating 4 out of 5 stars
Condition: New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Autor/Autorin: Iyer NarayanIn December 2016, I graduated from Purdue University in USA for Aeronautical and Astronautical Engineering. I am highly passionate about flight and have continually pursued knowledge and experience in this field. I curren. Seller Inventory # 385768353
Quantity: Over 20 available
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Effects of Time Varying Moments on a Large Tethered Satellite in Orbit
Published by
LAP LAMBERT Academic Publishing Sep 2019, 2019
ISBN 10: 3659649872
ISBN 13: 9783659649875
New
Taschenbuch
Seller: buchversandmimpf2000, Emtmannsberg, BAYE, Germany
Seller rating 5 out of 5 stars
Taschenbuch. Condition: Neu. Neuware -The purpose of this book is to investigate the effect of a varying moment on the rotation angle of a large tethered satellite that is orbiting a planet. Two different types of orbits were investigated: a simple circular orbit and an elliptical orbit. Cases with zero and non-zero initial angular rotation velocity were investigated as well. This investigation will assist satellite docking missions. The large rigid tethered satellite is a futuristic concept, and this investigation is meant to assist possible docking missions to the satellite. To simplify the problem, the rotation is constrained to the orbital plane.Books on Demand GmbH, Überseering 33, 22297 Hamburg 52 pp. Englisch. Seller Inventory # 9783659649875
Quantity: 2 available
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Effects of Time Varying Moments on a Large Tethered Satellite in Orbit : Analysis for Circular and Elliptical Orbits
Published by
LAP LAMBERT Academic Publishing, 2019
ISBN 10: 3659649872
ISBN 13: 9783659649875
New
Taschenbuch
Seller: AHA-BUCH GmbH, Einbeck, Germany
Seller rating 5 out of 5 stars
Taschenbuch. Condition: Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - The purpose of this book is to investigate the effect of a varying moment on the rotation angle of a large tethered satellite that is orbiting a planet. Two different types of orbits were investigated: a simple circular orbit and an elliptical orbit. Cases with zero and non-zero initial angular rotation velocity were investigated as well. This investigation will assist satellite docking missions. The large rigid tethered satellite is a futuristic concept, and this investigation is meant to assist possible docking missions to the satellite. To simplify the problem, the rotation is constrained to the orbital plane. Seller Inventory # 9783659649875
Quantity: 1 available
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Effects of Time Varying Moments on a Large Tethered Satellite in Orbit: Analysis for Circular and Elliptical Orbits
Published by
LAP LAMBERT Academic Publishing, 2019
ISBN 10: 3659649872
ISBN 13: 9783659649875
New
paperback
Seller: Mispah books, Redhill, SURRE, United Kingdom
Seller rating 4 out of 5 stars
paperback. Condition: New. New. book. Seller Inventory # ERICA82936596498726
Quantity: 1 available