顾及不同天线夹角增益下的北斗星间Ka定轨仿真验证方法、系统及设备
By generating a simulation verification method for inter-satellite Ka orbit determination that takes into account different antenna angle gains, the problem of insufficient orbit determination accuracy and resource waste of high-orbit satellites in the BeiDou-3 system was solved, the inter-satellite link resource allocation was optimized, and precise orbit determination and resource conservation of high-orbit satellites were achieved.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- WUHAN UNIV
- Filing Date
- 2025-10-31
- Publication Date
- 2026-07-17
AI Technical Summary
High-orbit satellites cannot meet the requirements for precise orbit determination in the BeiDou-3 system, and inter-satellite link resources are limited. The existing time slot planning table lacks optimization schemes, resulting in insufficient orbit determination accuracy and waste of resources.
By generating a simulation verification method for inter-satellite Ka orbit determination that takes into account different antenna angle gains, setting simulation observation parameters, simulating random and systematic errors, generating antenna pattern information, performing parameter estimation and precise orbit determination verification, and optimizing inter-satellite link resource allocation.
It has achieved the precise orbit determination requirements of high-orbit satellites, optimized the allocation of inter-satellite link resources, improved orbit determination accuracy and saved resources, and is adaptable to the link construction planning under different average visible BeiDou satellite numbers.
Smart Images
Figure CN121232227B_ABST