TY - JOUR
T1 - Effective Velocity Calculation Method in Passive Synthetic Aperture for Emitter Localization
AU - Zhang, Liting
AU - Huan, Hao
AU - Tao, Ran
AU - Wang, Yue
AU - Tang, Xiaogang
AU - Lin, Hai
N1 - Publisher Copyright:
© 2022 IEEE.
PY - 2022
Y1 - 2022
N2 - Emitter localization has been an active research subject in electronic reconnaissance, target tracking, emergency response, and satellite interference source localization. Recently, researchers applied passive synthetic aperture in the emitter localization to improve the positioning accuracy. Passive synthetic aperture uses Doppler rate and zero Doppler point to target range and azimuth locations, respectively. In spaceborne model, effective satellite velocity is used in the range equation to fit the passive synthetic aperture model. Therefore, this study proposed a convex optimization approach to calculate the effective satellite velocity. We established an objective function by calculating the relationship among beam footprint velocity, satellite velocity, and effective satellite velocity. The optimal effective satellite velocity and range distance are obtained through iterating different range distances. Finally, the experimental results show that the positioning accuracy of proposed method is one order of magnitude higher than that of traditional FOA and FDOA method.
AB - Emitter localization has been an active research subject in electronic reconnaissance, target tracking, emergency response, and satellite interference source localization. Recently, researchers applied passive synthetic aperture in the emitter localization to improve the positioning accuracy. Passive synthetic aperture uses Doppler rate and zero Doppler point to target range and azimuth locations, respectively. In spaceborne model, effective satellite velocity is used in the range equation to fit the passive synthetic aperture model. Therefore, this study proposed a convex optimization approach to calculate the effective satellite velocity. We established an objective function by calculating the relationship among beam footprint velocity, satellite velocity, and effective satellite velocity. The optimal effective satellite velocity and range distance are obtained through iterating different range distances. Finally, the experimental results show that the positioning accuracy of proposed method is one order of magnitude higher than that of traditional FOA and FDOA method.
KW - convex optimization
KW - emitter localization
KW - spaceborne passive synthetic aperture
UR - http://www.scopus.com/inward/record.url?scp=85146929106&partnerID=8YFLogxK
U2 - 10.1109/GLOBECOM48099.2022.10000661
DO - 10.1109/GLOBECOM48099.2022.10000661
M3 - Conference article
AN - SCOPUS:85146929106
SN - 2334-0983
SP - 4191
EP - 4195
JO - Proceedings - IEEE Global Communications Conference, GLOBECOM
JF - Proceedings - IEEE Global Communications Conference, GLOBECOM
T2 - 2022 IEEE Global Communications Conference, GLOBECOM 2022
Y2 - 4 December 2022 through 8 December 2022
ER -