To address the problem of how to remove low Earth orbit(LEO)debris with space-based high-powered pulse laser,a combined model of high-powered pulse laser ablation and variation of the debris' orbit element is advanced.By theoretical analysis,an expression of the single laser pulse's optimal interaction direction about the LEO debris' orbit element is derived,and the single laser pulse's optimal removal is proved to be mirror symmetric about the orbit major axis of debris.In consequence,aimed at optimizing b...
网络出版地址:www.cnki.net/kcms/detail/10.7527/S1000-6893.2014.0295.html引用格式:Han W H,Gan Q B,He Y,et al.Optimal direction and a process design of removing low Earth orbit debris with space-based la-ser[J].Acta Aeronautica et Astronautica Sinica,2015,36