Unmanned aerial vehicle cluster booster rocket ignition control system and working method thereof

The invention discloses an unmanned aerial vehicle cluster booster rocket ignition control system and a working method thereof. The system comprises a display module, an information processing module,a physical port recognition module, a computer (including upper computer software), an ignition cont...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: MAO SHIBIN, WANG DEMING, BU PEIHE
Format: Patent
Sprache:chi ; eng
Schlagworte:
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Beschreibung
Zusammenfassung:The invention discloses an unmanned aerial vehicle cluster booster rocket ignition control system and a working method thereof. The system comprises a display module, an information processing module,a physical port recognition module, a computer (including upper computer software), an ignition control module, a remote-control receiver and a telemetering receiver. Ignition triggering conditions are judged through the computer (including the upper computer software), remote control code recognition logic and telemetering code recognition logic, and manual or automatic triggering of multi-channel booster rocket ignition is achieved. According to the unmanned aerial vehicle cluster booster rocket ignition control system and the working method thereof, multi-aircraft ignition launching is supported in an unmanned aerial vehicle cluster scene, automatic or manual ignition launching of different types of unmanned aerial vehicle booster rockets can be adapted to, and the problem that a booster rocket ignition contro