With the development of navigation technology, dual-antenna navigation receiver has been more and more applied to the spacecraft. The layout of the satellite navigation receiving antennas directly affects the performance of the navigation receiver. In this paper, the constraints of layout of the navigation receiving antennas are analyzed and the optimization design method is provided. Its effectiveness is verified by simulation and comparative analysis.
Research on the optimization layout of spacecraft navigation receiving antenna
01.08.2016
533920 byte
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
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