Hybrid gasoline and electric power aircraft balance control system

The invention discloses a hybrid gasoline and electric power aircraft balance control system. The system comprises a data processing center, a sensing center, a first control unit, a second control unit, a gasoline engine, motors and a wireless transmission module, wherein the sensing center compris...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	SHI XIAOMEI, DENG QING, ZHANG WUYUN, MING JUN'AN, FU BINGXIANG, HAO GANG, WANG SHAOZHI
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	CONTROLLING PHYSICS REGULATING SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
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