{"title":"最大可用性的业余卫星优化设计","authors":"P. Rezaei, N. Aboutorabian, M. Hakkak","doi":"10.1109/ICACT.2006.206183","DOIUrl":null,"url":null,"abstract":"In this paper, we wanted to maximize the LEO satellite access for different condition of ground station's latitude and different satellite's altitude. This purpose has been obtained with proper inclination angle of satellite orbit around of the earth (to the equator) in optimum value. The optimum angles have been determined by satellite tool kit (STK) simulations","PeriodicalId":247315,"journal":{"name":"2006 8th International Conference Advanced Communication Technology","volume":"57 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2006-05-08","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"5","resultStr":"{\"title\":\"Optimum designing of amateur satellite for maximum availability\",\"authors\":\"P. Rezaei, N. Aboutorabian, M. Hakkak\",\"doi\":\"10.1109/ICACT.2006.206183\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"In this paper, we wanted to maximize the LEO satellite access for different condition of ground station's latitude and different satellite's altitude. This purpose has been obtained with proper inclination angle of satellite orbit around of the earth (to the equator) in optimum value. The optimum angles have been determined by satellite tool kit (STK) simulations\",\"PeriodicalId\":247315,\"journal\":{\"name\":\"2006 8th International Conference Advanced Communication Technology\",\"volume\":\"57 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2006-05-08\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"5\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2006 8th International Conference Advanced Communication Technology\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/ICACT.2006.206183\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2006 8th International Conference Advanced Communication Technology","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/ICACT.2006.206183","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Optimum designing of amateur satellite for maximum availability
In this paper, we wanted to maximize the LEO satellite access for different condition of ground station's latitude and different satellite's altitude. This purpose has been obtained with proper inclination angle of satellite orbit around of the earth (to the equator) in optimum value. The optimum angles have been determined by satellite tool kit (STK) simulations