Effects of Time Varying Moments on a Large Tethered Satellite in Orbit
Analysis for Circular and Elliptical Orbits
978-3-659-64987-5
3659649872
52
2019-09-06
32.90 €
eng
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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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Воздушные и космические технологии
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