Aircraft correction instruction transmission link design method based on radio frequency integration

The invention discloses an aircraft correction instruction transmission link design method based on radio frequency integration, and the method comprises the steps: (1) carrying out the unified scheduling design of platform radio frequency front-end integration and rear-end integration, the water su...

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Bibliographische Detailangaben
Hauptverfasser: GUO HANGHANG, LAN HAI, CHENG YINGBIAO, FU XINYING, LI JIAWEI
Format: Patent
Sprache:chi ; eng
Schlagworte:
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