The invention provides a dual-redundancy control system for a main landing gear of an unmanned aerial vehicle, and belongs to the technical field of aircrafts, and the dual-redundancy control system specifically comprises a dual-redundancy controller, an electric mechanism and a limiting mechanism which are arranged on an actuator cylinder of the main landing gear, the dual-redundancy controller is connected with the actuator cylinder of the main landing gear through a controller electric connector, and the electric mechanism is connected with the limiting mechanism. The electric mechanism comprises a first driving motor and a second driving motor, the limiting mechanisms are arranged in the main undercarriage actuating cylinder, the first driving motor and the second driving motor correspond to the corresponding limiting mechanisms respectively, and each limiting mechanism comprises a limit switch and a potentiometer assembly. The dual-redundancy controller receives signals of the limit switch and the potentiometer assembly and controls the electric mechanism. Through the processing scheme provided by the invention, the task reliability and the control precision of the system are improved, and the fault isolation capability of the system is improved.
本申请提供了一种无人机主起落架的双余度控制系统,属于航空器技术领域,具体包括设置在主起落架作动筒上的双余度控制器、电动机构和限位机构,双余度控制器通过控制器电连接器与主起落架作动筒连接,电动机构包括第一驱动电机和第二驱动电机,限位机构设置在主起落架作动筒内部,且第一驱动电机和第二驱动电机分别对应有相对应的限位机构,限位机构包括极限开关和电位器组件,双余度控制器接收极限开关和电位器组件的信号并对电动机构进行控制。通过本申请的处理方案,提高了系统任务可靠性以及控制精度,以及系统的故障隔离能力。
Dual-redundancy control system of main landing gear of unmanned aerial vehicle
一种无人机主起落架的双余度控制系统
2022-12-23
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |