The Application of RCS Characteristic Analysis in Close Range Formation Flight
Objects in close range formation flight need to be identified before being tracked by radar and other noncooperation tracking equipments. As the distance between the concomitant satellite and the main satellite is very close in formation flight, and the schedule entering into the sight of observation station is uncertain, the two objects cannot be distinguished by use of orbit parameters and tracking schedules of observation station. After analyzing the physical and moving characteristics of them, we propose an identification method by use of mean RCS and attitude stability determination. The results show that the method is effective for formation flight object identification at close range.
RCS Characteristic Analysis Formation Flight
Niu Wei Li Bo Su Wei Kou Peng
State Key Laboratory of Astronautic Dynamics, Xian, Shaanxi, 710043, China Beijing Aerospace Control Center, Beijing 100094, China
国际会议
三亚
英文
559-562
2012-01-06（万方平台首次上网日期，不代表论文的发表时间）