The invention discloses integrated navigation equipment, which is applied to an aircraft and comprises a power supply device, an inertial measurement device, a Beidou receiver, a central processing unit, a power amplifier and a hydraulic steering engine. The inertial measurement device is in communication connection with the central processor and is used for acquiring and sending the acceleration increment, the angular velocity increment, the acceleration and the angular velocity of the aircraft to the central processor. The central processor is configured to generate a control signal based on the acceleration increment, the angular velocity increment, the acceleration and the angular velocity. The power amplifier is used for receiving and amplifying the control signal. The hydraulic steering engine receives the control signal amplified by the power amplifier and drives the aircraft to fly according to a preset guide channel, the hydraulic steering engine is further used for sending a feedback signal to the power amplifier, and the power amplifier is further used for sending the feedback signal to the central processing unit. The Beidou receiver is in communication connection with the central processor and is used for acquiring and sending the positioning information of the aircraft to the central processor.
本发明公开了一体化导航设备,应用于飞行器,包括电源装置、惯性测量装置、北斗接收机、中央处理器、功率放大器和液压舵机。惯性测量装置与中央处理器通信连接,用于获取并向中央处理器发送飞行器的加速度增量、角速度增量以及加速度和角速度。中央处理器用于基于加速度增量、角速度增量以及加速度和角速度生成控制信号。功率放大器用于接收并放大控制信号。液压舵机接收由功率放大器放大后的控制信号,并驱动飞行器按照预设导引航道飞行,液压舵机还用于向功率放大器发送反馈信号,以及功率放大器还用于向中央处理器发送反馈信号。北斗接收机与中央处理器通信连接,用于获取并向中央处理器发送飞行器的定位信息。
Integrated navigation system, method and aircraft
一种一体化导航系统、方法和飞行器
2023-06-13
Patent
Electronic Resource
Chinese
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