The invention relates to the technical field of aircrafts, in particular to a control method of a tandem type hybrid power aircraft, which comprises a starting system, a power generation system, a monitoring system, an electric drive system, an integrated microcontroller, a PC (Personal Computer) upper computer and a power management control module, and is characterized in that the PC upper computer is connected with the integrated microcontroller through a network cable; the integrated microcontroller is connected with the power management control module; the control method of the tandem hybrid aircraft comprises the step of controlling the hybrid aircraft to be switched among a power generation system battery dual-output operation mode, a power generation system output battery input operation mode, a pure battery output operation mode and a pure power generation system output operation mode according to P power generation, P power and P fan. Therefore, the energy demand distribution condition of the tandem hybrid aircraft under different working modes and working conditions is improved, the operation efficiency of each core component of the system is improved, the robustness of a control strategy is guaranteed, and energy consumption is reduced.
本发明涉及飞行器技术领域,特别涉及一种串联式混合动力飞行器的控制方法,其包括串联式混合动力飞行器包括起动系统、发电系统、监测系统、电驱系统、集成微控制器、PC上位机和功率管理控制模块,PC上位机与集成微控制器通过网线连接,集成微控制器与功率管理控制模块连接,串联式混合动力飞行器的控制方法包括依据P发、P电和P扇控制混合动力飞行器在发电系统电池双输出运行模式、发电系统输出电池输入运行模式、纯电池输出运行模式和纯发电系统输出运行模式之间切换。借此改善串联式混合动力飞行器在不同工作模式和工况下的能量需求分配状况,提高系统各核心部件运行效率,保障控制策略鲁棒性,节约能源消耗。
Control method of tandem type hybrid power aircraft
串联式混合动力飞行器的控制方法
2025-02-18
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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