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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In 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 currently work for a large aerospace company in USA as a Systems Engineer, and I hold a private pilot license.