The invention discloses a power control system for a tilt-rotor aircraft, and the system comprises a position controller which is used for generating an overload instruction; the position ring is used for generating an overall attitude angle control instruction and/or a rotor wing overload control quantity of the aircraft according to the overload instruction; the attitude controller is used for generating an overall attitude control demand instruction of the aircraft and/or an overall coordinated turning control instruction of the aircraft according to the overall attitude angle control instruction; and the actuator controller is used for generating an actuator control instruction according to the attitude control demand instruction of the whole aircraft and/or the rotor wing overload control quantity. According to the invention, a series control method is adopted, full-mode control of a rotor wing mode, a transition mode and a fixed wing mode can be completed at the same time through a set of controller architecture, and two sets of controllers do not need to be arranged at the same time, so that the technical problems of complex work task, large workload, many uncertainty during transition and the like in the control law design of the tilting layout aircraft are solved.
本发明公开了一种倾转旋翼飞行器的动力控制系统,其包括:位置控制器,其用于生成过载指令;位置环,其用于根据过载指令生成飞行器的整体姿态角控制指令和/或旋翼过载控制量;姿态控制器,其用于根据所述整体姿态角控制指令生成飞行器整体的姿态控制需求指令和/或飞行器整体的协调转弯控制指令;以及,作动器控制器,其用于根据飞行器整体的姿态控制需求指令和/或旋翼过载控制量生成作动器控制指令。本发明采用串联控制方法,通过一套控制器架构即可同时完成旋翼模态、过渡模态、固定翼模态的全模态控制,无需同时设置两套控制器,以解决倾转布局飞行器控制律设计工作任务复杂、工作量大、且过渡时存在诸多不确定性等技术问题。
Power control system of tilt-rotor aircraft
一种倾转旋翼飞行器的动力控制系统
13.05.2025
Patent
Elektronische Ressource
Chinesisch
Hybrid power system, tilt-rotor aircraft and control method
Europäisches Patentamt | 2022
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