相关内容提交#655
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majj0319 wants to merge 27 commits into
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donghaiwang
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Jun 18, 2026
donghaiwang
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Jun 18, 2026
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landing/undergraduate/undergraduate/ |
donghaiwang
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Jun 18, 2026
donghaiwang
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Jun 18, 2026
| \noindent 论文作者（签字）：\includegraphics[width=2.4cm]{images/image3.jpeg}\hfill 时间：2026年5月25日 | ||
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| \noindent 指导教师已阅（签字）：\includegraphics[width=2.6cm]{images/image4.jpeg}\hfill 时间：2026年5月25日 |
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| %!TEX root = ../hutbthesis_main.tex | |||
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| \chapter{.绪论} | |||
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| 在国内，针对固定翼飞行器、无人机着陆展开的研究里，重点聚焦于起落架结构的优化工作、整体布局的分析工作、缓冲器性能的研究工作等多个方面。帅涛针对某一型号的起落架进行了设计、模态分析，明确指出起落架的固有频率、振型对于着陆冲击响应会产生非常重要的影响。周著学、于萍借助有限元分析方法针对小型航拍无人机的起落架进行了优化设计，阐述了合理调整结构、材料参数能够让应力分布得到改善并且提高承载能力。薛影、张超、吴星星剖析了无人机起落架布置对于起飞性能所造成的影响，显示出起落架的几何布局、安装位置与飞行性能存在着显著的耦合关系，而这对于着陆控制系统的总体设计同样具备参考价值。 | ||
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| 罗杰等人针对某型无人机起落架放下阶段缓冲器的气液流动特性展开了研究，进而揭示出缓冲器内部气液流动变化对于阻尼性能、响应过程所产生的影响。蒲雅熙是从油气缓冲器气液两相阻尼特性着手，对不同工况下缓冲器阻尼变化规律予以分析，表明着陆速度与冲击条件会直接作用于缓冲器工作状态\linkcite{10}。 |
Member
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PR标题需要概括所做的修改 |
Member
参考文献中人名显示异常，其他的都需要检查下
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Member
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测试的场景可以在README.md中提供一个网盘链接供下载 |
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