Effect of perturbations on debris-to-debris orbital transfers: A quantitative analysis

详细信息    查看全文

• 作者：Kartik Kumar^a ; ^b ; ^{kumar@dinamicatech.com} ; Enne Hekma^b ; Abhishek Agrawal^b ; Francesco Topputo^c
• 关键词：Space debris ; Active debris removal ; Mission design ; Orbital perturbations ; Lambert solver ; SGP4
• 刊名：Advances in Space Research
• 出版年：2017
• 出版时间：1 March 2017
• 年：2017
• 卷：59
• 期：5
• 页码：1289-1303
• 全文大小：3094 K
• 卷排序：59

文摘

Neglecting orbital perturbations when modeling debris-to-debris transfers can lead to significant errors. The greatest effect of orbital perturbations on debris-to-debris transfers occur in LEO. Errors in GTO and GSO are directly correlated to number of revolutions.