{"product_id":"effects-of-time-varying-moments-on-a-large-tethered-satellite-in-orbit-analysis-for-circular-and-elliptical-orbits-von-narayan-iyer","title":"Effects of Time Varying Moments on a Large Tethered Satellite in Orbit","description":"\u003cp\u003eThe 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.\u003c\/p\u003e\u003cdiv class=\"aw-variant-hidden-subtitle-div\" id=\"aw-variant-subtitle-9783659649875\"\u003e\u003ch3\u003eAnalysis for Circular and Elliptical Orbits\u003c\/h3\u003e\u003c\/div\u003e","brand":"Libri","offers":[{"title":"Softcover - 9783659649875","offer_id":39449269469277,"sku":"9783659649875","price":32.9,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0940\/0622\/files\/903ed2e1-a005-4096-84fb-199d8f1c002d.jpg?v=1770098196","url":"https:\/\/shop.autorenwelt.de\/products\/effects-of-time-varying-moments-on-a-large-tethered-satellite-in-orbit-analysis-for-circular-and-elliptical-orbits-von-narayan-iyer","provider":"Autorenwelt Shop","version":"1.0","type":"link"}