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空天防御  2025, Vol. 8 Issue (4): 38-45    
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变构型技术在临近空间高速飞行器中的应用前景及挑战
杨建东1, 赵文文1, 李晓龙2, 殷玮1, 刘伟1, 蔡克荣2
1. 上海机电工程研究所,上海 201109; 2. 上海航天技术研究院,上海 201109
The Prospect and Challenges of Using Morphing Technology in High-Speed Vehicles in the Near Space
YANG Jiandong1, ZHAO Wenwen1, LI Xiaolong2, YIN Wei1,LIU Wei1, CAI Kerong2
1. Shanghai Electro-Mechanical Engineering Institute, Shanghai 201109, China; 2. Shanghai Academy of Spaceflight Technology, Shanghai 201109, China
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摘要 变构型技术应用于临近空间高速飞行器能够提升飞行器的飞行性能、突防能力及作战效能,具有广阔的应用前景。本文聚焦变构型技术在临近空间高速飞行器应用前景及挑战,从变构型方式、变构型驱动和变构型控制三方面介绍变构型技术研究进展与现状;剖析临近空间高速飞行器特点和应用前景;总结飞行器总体设计、变构型机构设计和飞行控制三方面难点。针对以上难点,提出了多学科耦合变构型飞行器总体设计、变形/承载/防热一体化变构型结构设计、快响应/高精度/高功重比伺服设计、高精度气动力预示及建模、气动弹性快速分析方法、耦合强非线性下高精度控制等关键技术。
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关键词 变构型技术临近空间高速飞行器飞行器设计    
Abstract:Morphing technology applied to hypersonic vehicles in near-space can enhance flight performance, penetration capability, and combat effectiveness, obtaining a broad application prospect. This paper focused on the application prospects and challenges of morphing technology in hypersonic near-space vehicles. It comprehensively summarised the research progress and status of morphing technology from three aspects: morphing methods, morphing drive, and morphing control. It delved into the characteristics and application prospects of hypersonic near-space vehicles, and systematically identified three significant difficulties: overall vehicle design, morphing mechanisms design, and flight control design. To resolve the above findings, this study proposed several key future technologies, including multidisciplinary coupled overall design for morphing vehicles, integrated deformation-bearing-thermal protection structure design, high-response-speed/high-precision/high-power-to-weight-ratio servo design, high-precision aerodynamic prediction and modelling, rapid aerodynamic elasticity analysis methods, and high-precision control under strongly coupled nonlinear conditions.
Key wordsallosteric technology    high-speed aircraft in near space    vehicles design
收稿日期: 2025-03-31      出版日期: 2025-09-09
ZTFLH:  V 221  
基金资助:上海市2024年度“科技创新行动计划”启明星项目扬帆专项(24YF2719700)
作者简介: 杨建东(1992—),男,硕士,工程师。
引用本文:   
杨建东, 赵文文, 李晓龙, 殷玮, 刘伟, 蔡克荣. 变构型技术在临近空间高速飞行器中的应用前景及挑战[J]. 空天防御, 2025, 8(4): 38-45.
YANG Jiandong, ZHAO Wenwen, LI Xiaolong, YIN Wei, LIU Wei, CAI Kerong. The Prospect and Challenges of Using Morphing Technology in High-Speed Vehicles in the Near Space. Air & Space Defense, 2025, 8(4): 38-45.
链接本文:  
https://www.qk.sjtu.edu.cn/ktfy/CN/      或      https://www.qk.sjtu.edu.cn/ktfy/CN/Y2025/V8/I4/38

参考文献
[1] 阎宏磊, 陆远, 郭杰, 唐胜景, 李响. 欠驱动高超滑翔飞行器集群协同编队控制方法[J]. 空天防御, 2024, 7(1): 56-62.
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