The invention relates to a control system of an unmanned aerial vehicle engine. The system comprises a main control system, a propulsion system, a rudder system and a feedback system, a rudder sheet driving transmission mechanism of the rudder system comprises a control connecting rod controlled by a rudder sheet driving motor, two rudder sheets are connected to the control connecting rod, and thecontrol connecting rod drives the two rudder sheets to rotate. Symmetry of the two opposite rudder sheets is fully utilized, one rudder sheet driving motor is adopted to control the two rudder sheetsthrough the control connecting rod, meanwhile, movement information of the control connecting rod is directly fed back to a processing module through a sensor, and therefore the rudder piece drivingmotor is controlled and adjusted. In this way, the two rudder sheets are controlled by one rudder sheet driving motor, and the processing module can control and adjust the two rudder sheets only by processing the feedback information of one rudder sheet once, so that the corresponding rudder sheet driving motors do not need to be processed respectively through the feedback of the two rudder sheetsin the information processing process.
本发明涉及无人飞行器发动机的控制系统,包括主控系统,推进系统,舵系统,反馈系统,舵系统的舵片驱动传动机构包括由一个舵片驱动电机控制的控制连杆,两个所述的舵片连接在该控制连杆上,控制连杆带动该两个舵片转动。充分利用相对的两个舵片的对称性,采用一个舵片驱动电机通过本控制连杆控制两个舵片同时该控制连杆的活动信息直接通过传感器反馈到处理模块中,由此对舵片驱动电机进行控制、调整,这样即通过一个舵片驱动电机控制两个舵片的方式并且处理模块只需按曾经处理一个舵片的反馈信息即可完成对两个舵片的控制、调整,这样使得在信息处理中无需经过对两个舵片的反馈分别处理对应的舵片驱动电机。
Control system of unmanned aerial vehicle engine
无人飞行器发动机的控制系统
2020-12-29
Patent
Electronic Resource
Chinese
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