Method and device for automatically realizing synchronous orbit satellite position keeping

Abstract

The invention discloses a method and a device for automatically realizing synchronous orbit satellite position keeping. The method comprises the steps of setting ignition parameters, a satellite taskmode, a position keeping operation job calling rule, a position keeping operation job script execution process and a fault interpretation rule; according to the ignition parameters, the satellite taskmode, the position keeping operation job calling rule, the position keeping operation job script execution process and the fault interpretation rule, generating a position keeping operation script set based on a SCL language, wherein the position keeping operation script set includes a plurality of position keeping operation scripts; and calling the position keeping operation script from the position keeping operation script set according to the current satellite position keeping operation task and the position keeping operation job calling rule, and automatically realizing synchronous orbitsatellite position keeping according to the position keeping operation script. The technical problem that in the prior art, the quality and efficiency of satellite position keeping operation are low is solved.

Description

technical field [0001] The present application relates to the technical field of space vehicle position maintenance, in particular to a method and device for automatically realizing the position maintenance of synchronous orbit satellites. Background technique [0002] Satellites in geosynchronous orbit refer to satellites that revolve around the earth, the sun or stars, etc., and operate in specific orbits, such as geosynchronous orbit satellites or sun synchronous orbit satellites, etc. static state. Since geostationary orbit satellites are susceptible to deviation from the predetermined operating position due to the influence of the environment and tasks during the specific orbit operation, in order to ensure that the geosynchronous orbit satellites operate according to the predetermined operating position, it is necessary to perform position protection operations on geosynchronous orbit satellites. [0003] At present, the traditional position-keeping operation uplink c...

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Problems solved by technology

[0004] The technical problem solved by this application is: aiming at the low quality and efficiency of satellite position keeping operation in the prior art, a method and device for automatically realizing the position keeping of geostationary orbit satellites are provided. The solution provided by the embodiment of this application In this process, according to the set ignition parameters, satellite task mode, job calling rules for position keeping operation, script execution process of position keeping operation and fault analysis rules, a set of position keeping job scripts is generated based on SCL language. When the satellite is in position keeping operation, directly Centrally call the position keeping job script from the position keeping job script, and realize the independent execution of the uplink command according to the position keeping job script, which can minimize the manual operation tasks and workload on the ground, and improve the quality and efficiency of the satellite position keeping operation.

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