Aircraft auxiliary airfoil control system
Aircraft auxiliary airfoil control system
The invention relates to the technical field of control systems, particularly to an aircraft auxiliary airfoil control system, thereby solving a technical problem of low safety factor in the prior art. The airplane auxiliary airfoil control system comprises a control unit, an execution unit, and a detection compensation unit. The control unit comprises a management computer, two paths of logic control modules and a working relay group. The execution unit is connected with the control unit, and the execution unit receives a command of the control unit to act; the detection compensation unit isconnected with the execution unit and feeds back new data and conveys the data to the control unit. Misoperation of pilots is avoided, the safety of the aircraft is greatly improved, and the flight safety of the aircraft is improved through the double-control auxiliary airfoil control system and the arrangement of the double-control handle and the logic control module.
本发明涉及控制系统技术领域，具体涉及一种飞机辅助翼面控制系统，旨要解决的技术问题在于克服现有技术中的安全系数低的缺陷，主要是通过以下技术方案得以实现的：一种飞机辅助翼面控制系统，包括：控制单元，所述控制单元包括管理计算机、逻辑控制模块和工作继电组，所述逻辑控制模块包括有两路；执行单元，所述执行单元与所述控制单元相互连接，所述执行单元接收所述控制单元命令进行动作；检测补偿单元，所述检测补偿单元检测与所述执行单元连接并反馈新输送所述控制单元，通过双操纵的辅助翼面控制系统，设置双操纵手柄和逻辑控制模块，避免了飞行员的误操作，大大提高了飞机的安全性，增加了飞机飞行的安全性。
Document information
Aircraft auxiliary airfoil control system
一种飞机辅助翼面控制系统
2020-07-10
Patent
Electronic Resource
Chinese
| IPC: | B64C AEROPLANES , Flugzeuge |
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