Real-time Orbit Determination for Space Rendezvous and Docking Based on EKF and Multi-source Information Fusion
In order to realize real-time orbit determination for space rendezvous and docking, a multi-source information fusion method based on extended Kalman filtering is established.The method fuses data sources from USB measurement, relay satellite, telemetry data between the target and the spacecraf, and data from onboard acceleration meter.The software procedure is also presented.
Multi-source Information FusionReal-time Orbit Determination
NETL
NSTL
万方数据
维普
