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发明公开
CN106996794A 一种无人直升机状态监测装置 审中-实审

一种无人直升机状态监测装置
摘要：
本发明公开了一种无人直升机状态监测装置，其包括安装在无人直升机内的飞行控制系统、监测控制器、报警蜂鸣器、旋螺桨测速计和输出显示器，所述飞行控制系统与监测控制器连接，所述报警蜂鸣器、旋螺桨测速计和输出显示器分别与监测控制器连接所述飞行控制系统包括自带的GPS模块、IMU惯性测量单元、高度计、油门和其他状态数据模块；所述监测控制器通过各自对应GPS模块、IMU惯性测量单元、高度计、油门和其他状态数据模块的传感器直接读取GPS数据、IMU姿态数据、高度数据、油量输出数据以及其他状态数据。
摘要（英）：

The invention discloses an unmanned helicopter state monitoring device. The unmanned helicopter state monitoring device comprises a flight control system, a monitoring controller, an alarm buzzer, a rotating screw speedometer and an output display which are arranged in an unmanned helicopter, wherein the flight control system is connected with the monitoring controller; the alarm buzzer, the rotating screw speedometer and the output display are connected with the monitoring controller respectively; the flight control system comprises a built-in GPS (Global Positioning System) module, an IMU (Inertial Measurement Unit), a height meter, an accelerator and an other-state data module; the monitoring controller is used for directly reading GPS data, IMU attitude data, height data, fuel capacity output data and other state data through sensors corresponding to the GPS module, the IMU, the height meter, the accelerator and the other-state data module.

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