The present invention discloses a method for continuously establishing an intersatellite link supporting the
orbital maneuver of the BeiDou-3
satellite. The method uses the post-control theoretical
orbit to assist in
link building, so that the intersatellite link can operate stably and reliably. First, the intersatellite link topology routing of the
satellite is planned, and an intersatellite
link building plan is formulated. Then, before the
orbital maneuver, two sets of
satellite almanac parameters for the entire network are generated and the almanac parameters are added to the satellite. Then, the almanac
link building is immediately enabled, and finally the
orbital maneuver is implemented, so that the intersatellite link remains continuous. The method for continuously establishing an intersatellite link of the present invention is completely based on the satellite design state, and the
processing flow can be automated. It can improve the intersatellite link of the orbital maneuvering satellite from being interrupted for K hours to being continuously uninterrupted throughout the whole process, and provides a technical guarantee for improving the service availability of the
navigation system.