Four-axis aircraft control system

The utility model discloses a four-axis aircraft control system. The system is characterized by comprising a six-axis gyroscope, an LED display unit, a PWM control unit, an MCU processor, an air pressure sensor, a power circuit, a left up-and-down motor drive circuit, a right up-and-down motor drive...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: JIN TIAN, ZOU XINFU, ZHANG WEIHUA, WANG CHAO, YAO DANYONG
Format: Patent
Sprache:chi ; eng
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Beschreibung
Zusammenfassung:The utility model discloses a four-axis aircraft control system. The system is characterized by comprising a six-axis gyroscope, an LED display unit, a PWM control unit, an MCU processor, an air pressure sensor, a power circuit, a left up-and-down motor drive circuit, a right up-and-down motor drive circuit, a camera circuit, a GPS route return circuit and an aircraft remote controller. The four-axis aircraft can achieve the functions of optical flow positioning, air pressure height determination, aerial photography and the like. 本实用新型公开了一种四轴飞行器控制系统,其特征在于,其包括六轴陀螺仪、LED显示单元、PWM控制单元、MCU处理器、气压传感器、电源电路、左上下电机驱动电路、右上下电机驱动电路、摄像电路、GPS路线返航电路及飞行器遥控器组成。四轴飞行器能实现光流定位、气压定高、航拍等功能。