The invention relates to a fuel supply system and flight control integrated design method of a long-endurance aircraft, which is used for simplifying the complexity of a fuel supply system of an unmanned aerial vehicle, improving the integration degree of the aircraft and reducing the design difficulty of a flight control system. The invention relates to preliminary architecture design of a fuel supply system, structural design of a fuel tank, design of a ventilation/pressurization subsystem, design of a fuel supply and transportation subsystem, gravity center control and simulation of a long-endurance unmanned aerial vehicle, design of a travel control and fuel supply system comprehensive control computer, and design of a fuel supply and flight control integrated architecture.
本发明涉及长航时飞行器的燃油供应系统与飞行控制一体化设计方法,用于简化无人机的燃油供应系统复杂度,提高飞行器的一体化程度,并降低飞行控制系统设计难度。本发明涉及燃油供应系统初步架构设计,燃油箱结构设计,通气/增压子系统设计,供输油子系统设计,长航时无人机重心控制与仿真,行控制与燃油供应系统综合控制计算机设计,燃油供应与飞行控制一体化架构设计。
Fuel supply system and flight control integrated design method of long-endurance aircraft
长航时飞行器的燃油供应系统与飞行控制一体化设计方法
2024-03-29
Patent
Elektronische Ressource
Chinesisch
IPC: | B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen |
Design method and system for realizing long-endurance flight of multi-rotor aircraft
Europäisches Patentamt | 2015
|High Altitude Long Endurance Aircraft Design Studies
British Library Conference Proceedings | 1993
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