Portada del libro de Effects of Time Varying Moments on a Large Tethered Satellite in Orbit
Título del libro:

Effects of Time Varying Moments on a Large Tethered Satellite in Orbit

Analysis for Circular and Elliptical Orbits

LAP LAMBERT Academic Publishing (2019-09-06 )

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ISBN-13:

978-3-659-64987-5

ISBN-10:
3659649872
EAN:
9783659649875
Idioma del libro:
Inglés
Notas y citas / Texto breve:
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.
Editorial:
LAP LAMBERT Academic Publishing
Sitio web:
https://www.lap-publishing.com/
Por (autor):
Narayan Iyer
Número de páginas:
52
Publicado en:
2019-09-06
Stock:
Disponible
Categoría:
Aire y la tecnología espacial
Precio:
32.90 €
Palabras clave:
Tethered Satellite, Space Dynamics, Elliptical orbit, Circular Orbit, Dumbbell satellite, Time Varying Moments, ode45

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