{"title":"Keplerian Orbit and Satellite skCUBE","authors":"P. Szabó, K. Gombíková, M. Ferencová, M. Kosuda","doi":"10.1109/NTAD.2019.8875530","DOIUrl":null,"url":null,"abstract":"This paper describes the basic concepts for determining the cosmic objects position and motion according to the Kepler's Laws and Newton's law of Universal Gravitation. In addition, the paper also includes an algorithm to compute the (miniature) satellites orbit. The algorithm input data was received from two-line elements (TLE) record. One of the program outputs is the computation of the skCUBE miniature satellite orbit. Following the authors' research, this paper also contains a brief overview of the skCUBE development and its evolution. The MATLAB Live Editor was used for program implementation of the algorithm.","PeriodicalId":186247,"journal":{"name":"2019 New Trends in Aviation Development (NTAD)","volume":"15 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2019-09-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"1","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"2019 New Trends in Aviation Development (NTAD)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/NTAD.2019.8875530","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 1
Abstract
This paper describes the basic concepts for determining the cosmic objects position and motion according to the Kepler's Laws and Newton's law of Universal Gravitation. In addition, the paper also includes an algorithm to compute the (miniature) satellites orbit. The algorithm input data was received from two-line elements (TLE) record. One of the program outputs is the computation of the skCUBE miniature satellite orbit. Following the authors' research, this paper also contains a brief overview of the skCUBE development and its evolution. The MATLAB Live Editor was used for program implementation of the algorithm.
本文叙述了根据开普勒定律和牛顿万有引力定律确定宇宙物体位置和运动的基本概念。此外,本文还提出了一种计算(微型)卫星轨道的算法。算法输入数据来自两行元素(TLE)记录。其中一个程序输出是skCUBE微型卫星轨道的计算。根据作者的研究,本文还简要概述了skCUBE的发展及其演变。利用MATLAB Live Editor对算法进行程序实现。