直接力与气动力复合控制前向拦截导引律综述
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( 1.海军航空工程学院控制工程系,山东烟台 264001;2.海军航空工程学院科研部,山东烟台 264001)

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V448.13

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A Survey of Head Pursuit Guidance Law with Blended Lateral Jets and Aerodynamic Control
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( 1.Naval Aeronautical and Astronautical University Department of Control Engineering , Yantai Shandong 264001, China;2.Naval Aeronautical and Astronautical University Department of Scientific Research, Yantai Shandong 264001, China)

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    摘要:

    直接力与气动力复合控制前向追击在拦截高空高速目标方面具有独特的优势。分别综述了前向拦截导引律和直接力气动力复合控制设计方法的研究进展,其中,直气复合控制分别从点火逻辑设计、控制分配方法、气动舵控制和直接力控制分别设计、俯仰和偏航通道同时设计、复合控制导弹的制导律设计等几方面进行分类分析,并介绍了复合控制前向拦截导引律进展。最后,指出了值得进一步研究的几个关键问题,可为今后的研究提供参考。

    Abstract:

    Head pursuit guidance with blended lateral jets and aerodynamic control has special advantages on interceptinghigh speed targets in high altitude. A comprehensive literature review was presented, and the different techniques em.ployed in head pursuit and blended control was introduced. For blended control, ignition logic design, control allocation,design of aerodynamic rudder control and the lateral jets control respectively, design of pitch channel and yaw channel to.gether and guidance law design with blended control were discussed in detail. Then, research on head pursuit guidancelaws with blended control was introduced. Finally, the subjects of future work were outlined, with the aim to provide a refer.ence for further researches.

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吴华丽,程继红,施建洪,张友安.直接力与气动力复合控制前向拦截导引律综述[J].海军航空大学学报,2016,31(3):323-331
WU Huali, CHENG Jihong, SHI Jianhong, ZHANG Youan. A Survey of Head Pursuit Guidance Law with Blended Lateral Jets and Aerodynamic Control[J]. JOURNAL OF NAVAL AVIATION UNIVERSITY,2016,31(3):323-331

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  • 在线发布日期: 2016-07-01
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