State Least-square Estimation of Relative Orbit Modification Point for Following Spacecraft
Guo Bibo1,2 Liang Bin1 Qiu Yue1 Qiang Wenyi2(1 Institute of Space Intelligent System,Harbin Institute of Technology,Harbin 150001)(2 Astronautics School,Harbin Institute of Technology,Harbin 150001)
