TY - JOUR
T1 - 基于奇异谱分析的空间非合作目标无源机动检测方法
AU - Gong, Baichun
AU - Yang, Shihang
AU - Han, Fei
AU - Sun, Yue
AU - Ning, Xin
N1 - Publisher Copyright:
© 2024 Editorial Department of Journal of Chinese Inertial Technology. All rights reserved.
PY - 2024/10
Y1 - 2024/10
N2 - To solve the maneuver detection problem in the initial orbit determination stage of the space situation awareness mission for non-cooperative targets, a passive maneuver detection method based on singular spectrum analysis is proposed. Firstly, a nonlinear relative dynamics and a line-of-sight measurement model are established in the local vertical local horizontal frame. Subsequently, the features of the line-of-sight (LOS) angle sequences are extracted by singular spectrum analysis, the calculation method of the differential evaluation index and threshold are designed, and the AND/OR gates are used for comprehensive judgment. Finally, the maneuver detection model is verified, tested and analyzed in GEO type orbit and different working conditions. With a camera precision of no less than 3×10-4 rad, small pulse maneuvers within the range of 1 m/s for non-cooperative targets with an altitude difference of 1000 km could be effectively detected, the success rate of maneuver detection above 1 m/s is more than 90%.
AB - To solve the maneuver detection problem in the initial orbit determination stage of the space situation awareness mission for non-cooperative targets, a passive maneuver detection method based on singular spectrum analysis is proposed. Firstly, a nonlinear relative dynamics and a line-of-sight measurement model are established in the local vertical local horizontal frame. Subsequently, the features of the line-of-sight (LOS) angle sequences are extracted by singular spectrum analysis, the calculation method of the differential evaluation index and threshold are designed, and the AND/OR gates are used for comprehensive judgment. Finally, the maneuver detection model is verified, tested and analyzed in GEO type orbit and different working conditions. With a camera precision of no less than 3×10-4 rad, small pulse maneuvers within the range of 1 m/s for non-cooperative targets with an altitude difference of 1000 km could be effectively detected, the success rate of maneuver detection above 1 m/s is more than 90%.
KW - maneuver detection
KW - relative navigation
KW - singular spectrum analysis
KW - space non-cooperative target
KW - space situational awareness
UR - http://www.scopus.com/inward/record.url?scp=85210926057&partnerID=8YFLogxK
U2 - 10.13695/j.cnki.12-1222/o3.2024.10.013
DO - 10.13695/j.cnki.12-1222/o3.2024.10.013
M3 - 文章
AN - SCOPUS:85210926057
SN - 1005-6734
VL - 32
SP - 1052
EP - 1060
JO - Zhongguo Guanxing Jishu Xuebao/Journal of Chinese Inertial Technology
JF - Zhongguo Guanxing Jishu Xuebao/Journal of Chinese Inertial Technology
IS - 10
ER -