助推—滑翔飞行器轨迹设计研究综述
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(海军航空工程学院控制工程系,山东 烟台 264001)

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V249.122

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A Survey of Boost-Glide Aircraft Trajectory Design
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(Department of Control Engineering,NAAU,Yantai Shangdong 264001,China)

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    摘要:

    近年来,随着武器防御系统的不断发展,具有高突防能力的基于助推—滑翔概念的超声速跨大气层飞行器成为国内外的研究热点。目前国内外出现多种助推—滑翔飞行器轨迹设计方法,但较全面地对各种方法进行综合研究的文献非常有限且近期未见公开发表。通过对这方面相关文献的研究,将助推—滑翔飞行器轨迹设计的关键问题分类,总结了常见解决方案的特点和应用情况,对一些热点问题进行了探讨,并对未来的工作提出了建议。

    Abstract:

    In recent years, with the development of the weapon defense system, the hypersonic boost-glide vehicle weapon which span the atmosphere with high penetrativity become an interesting research point. At present, some methods for boost-glide aircraft trajectory design have appeared all over the world. But only a few of papers were presented about the survey of this field and that not being published recently. By the investigation of a bibliography of a lot of papers, the key problems of trajectory design were categorized and the characteristic and application of the familiar solutions were summarized, some hot problems were discussed, then the proposals for further research were presented.

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引用本文

杨秀霞,张毅,施建洪,盖峻峰.助推—滑翔飞行器轨迹设计研究综述[J].海军航空大学学报,2012,27(3):245-252
YANG Xiu-xia, ZHANG Yi, SHI Jian-hong, GAI Jun-feng. A Survey of Boost-Glide Aircraft Trajectory Design[J]. JOURNAL OF NAVAL AVIATION UNIVERSITY,2012,27(3):245-252

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  • 在线发布日期: 2018-07-05
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