首页|"冯如三号"高效超长航时无人滞空平台的设计与实践

"冯如三号"高效超长航时无人滞空平台的设计与实践

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超长航时无人滞空平台具有成本低、连续侦察能力强等特点,是未来新型飞行器的发展方向。该"冯如三号"高效超长航时无人滞空平台设计方案由该校本科生提出,采用了超高效气动布局、轻量化高强度复合材料、高效高可靠双环动力系统驱动及持久滞空飞行控制系统,通过车载起飞方式,在执行超长航时任务能力方面取得了全方位创新性突破。"冯如三号"高效超长航时无人机刷新了国际航联认证的"25~100 kg级油动无人机续航时间"世界纪录。
Design and experiment of the"Feng Ru 3"highly efficient ultra-long endurance unmanned aerial vehicle
[Objective]Ultra-long endurance unmanned aerial vehicles are advanced aircraft with excellent sustained flight capability and have the characteristics of low-cost,long-term,large-scale,and high-density intelligence collection and monitoring tasks.Due to these advantages,the ultra-long endurance unmanned aerial vehicle has become an important direction for future air vehicles.[Methods]Undergraduates from Beihang University have proposed a scheme for a highly efficient ultra-long endurance unmanned aerial vehicle,"Feng Ru 3."This scheme contains the ultra-high-aspect-ratio wing,low-drag drop-shaped fuselage,and high-placed empennage.These compose a highly efficient aerodynamic configuration.In addition,the flying platform structure is constructed from a novel composite material with light weight and high strength.This project has innovatively designed a dual-loop power system consisting of an inner loop electronic fuel injection system and an outer loop engine health monitoring system.The team has developed a durable loitering flight control system involving gust alleviation technology and PID parameter self-adaptation technology based on open-source flight control equipment.In addition,this project abandons the traditional takeoff and landing method of the landing gear and shows an innovative vehicle-based takeoff method.[Results]Ground testing(including wind tunnel test,structure static test,propulsion system test)and flight test(including autonomous takeoff and landing test,dolly takeoff test,and long-endurance flight test)are performed on"Feng Ru 3".The experimental results reveal that(1)the highly efficient aerodynamic configuration vastly increases the aerodynamic efficiency,resulting in a maximum lift-to-drag ratio of~18.36.(2)The wing and tail made by ultra-light and high-strength composites can withstand a load of 4G,and their flexural changes are within an acceptable range.The stiffness of the tail support carbon tube also meets the design requirements.(3)After multiple 120-h experiments,it is proved that the dual-loop power system can drive the propulsion system super efficiently,enduringly,reliably,and cost-effectively.(4)The introduction of the adaptive PID algorithm in the flight control system of this project can effectively support stable,energy-efficient,and reliable completion of long-endurance flight missions.(5)The project adopts a takeoff method using a vehicle.This approach can reduce about 5 kg of the weight of the landing gear and its additional structures present a higher aerodynamic efficiency,reducing approximately 10%of aerodynamic drag.[Conclusions]Due to the highly efficient aerodynamic configuration,ultra-light and high-strength composites,a highly reliable dual-loop power system,a durable loitering flight control system,and the vehicle-based takeoff method,this developed unmanned aerial vehicle has achieved a comprehensive breakthrough in the capability of executing ultra-long endurance missions.Despite extreme and adverse weather conditions,including wind gusts of 7-8 levels,"Feng Ru 3"successfully achieved an uninterrupted flight of 80 h,46 min,and 35 s.This achievement of"Feng Ru 3"has set the world record for"the endurance of 25-100 kg class oil-powered fixed-wing unmanned aerial vehicle"certified by the International Aviation Federation.

ultra-long enduranceunmanned aerial vehicleworld recordundergraduate

邱玉婷、王耀坤、张益铨、李淼、刘绚

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北京航空航天大学 北航学院,北京 100191

北京航空航天大学 航空科学与工程学院,北京 100191

超长航时 无人机 世界纪录 本科生

北京航空航天大学教学改革项目北京航空航天大学专项北京航空航天大学专项"冯如三号"无人机学生科创项目

403750ZG211S2151ZG211S2202

2024

实验技术与管理
清华大学

实验技术与管理

CSTPCD北大核心
影响因子:1.651
ISSN:1002-4956
年,卷(期):2024.41(4)
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