智能平流层浮空器Loon关键技术分析与仿真  

Simulation research and key technologies analysis of intelligent stratospheric aerostat Loon

作　　者：邓小龙 杨希祥[1] 朱炳杰[1] 麻震宇[1] 侯中喜[1] DENG Xiaolong;YANG Xixiang;ZHU Bingjie;MA Zhenyu;HOU Zhongxi(College of Aerospace Science and Engineering,National University of Defense Technology,Changsha 410073,China)

机构地区：[1]国防科技大学空天科学学院,长沙410073

出　　处：《航空学报》2023年第8期23-39,共17页Acta Aeronautica et Astronautica Sinica

基　　金：国家自然科学基金(61903369,52172410)。

摘　　要：基于风场利用的智能平流层浮空器具有驻空时间长、系统构成简单、部署速度快、使用效费比高、自主能力强等优点,是临近空间飞行器发展的重要方向。针对典型基于风场利用的平流层浮空器Loon项目,通过对项目实施及实践探索的综述,深入分析其囊体材料与结构、高度调控、能源与推进、安控回收、风场建模、自主控制等关键技术特点,基于学科建模对总体参数、超热超压、气体泄漏、能源平衡、轨迹规划等方面进行仿真研究,总结了Loon智能平流层浮空器的技术特点,为基于风场利用的平流层浮空器设计与应用研究提供参考。With the merits of long endurance,compact system configuration,rapid deployment,high costeffectiveness and strong path planning capability,the intelligent stratospheric aerostat based on utilization of wind field is an important direction for the development of near space vehicles.As a typical intelligent stratospheric aerostat proj⁃ect using the wind field,Loon balloon is studied in this work.By reviewing and analyzing implementation and practical exploration of the project,the characteristics of the key technologies,including envelope material and structure,alti⁃tude control,energy and propulsion,safety control and recovery,wind field modeling,and autonomous control,have been analyzed.Based on the subject modeling method,simulation is carried out to analyze the overall parameters,super-heat and super-pressure properties,lift gas leakage,energy balance,trajectory planning.The technical charac⁃teristics of Loon balloon project are summarized,providing a reference for the design and application of the intelligent stratospheric aerostats based on utilization of wind field.

关 键 词：临近空间 平流层浮空器 Loon气球 超压结构 自主导航 区域驻留 

分 类 号：V11[航空宇航科学与技术—人机与环境工程]