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舰艇摇荡对舰载导弹飞行参数影响的分析
引用本文:夏龙世,邹强,宋贵宝,胡波.舰艇摇荡对舰载导弹飞行参数影响的分析[J].海军航空工程学院学报,2005,20(2):223-226.
作者姓名:夏龙世  邹强  宋贵宝  胡波
作者单位:海军航空工程学院研究生管理大队,空军工程大学工程学院,海军航空工程学院飞行器工程系,91685部队 西安,710038,烟台,264001,海南陵水,572425
摘    要:提出了分析导弹飞行参数受舰艇摇荡影响问题的思路,给出了导弹飞行参数在舰艇摇荡条件下的变化模型,反映了影响作用的本质,并给出了实际的仿真结果及分析结论。

关 键 词:舰艇摇荡  导弹  飞行参数  影响
修稿时间:2004年12月10

Analysis of Ship-rocking Effect On Flight Parameters of Ship-borne Missiles
XIA Long-shi,ZOU Qiang,SONG Gui-bao,HU Bo Graduate Students'Brigade of NAEI Engineering College of AFEU,Xi'an.Analysis of Ship-rocking Effect On Flight Parameters of Ship-borne Missiles[J].Journal of Naval Aeronautical Engineering Institute,2005,20(2):223-226.
Authors:XIA Long-shi  ZOU Qiang  SONG Gui-bao  HU Bo Graduate Students'Brigade of NAEI Engineering College of AFEU  Xi'an
Institution:XIA Long-shi,ZOU Qiang,SONG Gui-bao,HU Bo Graduate Students'Brigade of NAEI Engineering College of AFEU,Xi'an,710038 Department of Airborne Vehicle Engineering,NAEI,Yantai,264001 The 91685th Unit of PLA,Lingshui,Hainan,572425
Abstract:In this paper method of analyzing ship-rocking effect on flight parameters of ship-borne missiles is given, essential variation models of some important flight parameters are acquired by this method. As the results, simulating with these models draws some conclusion and some advice is presented.
Keywords:ship-rocking  missile  flight parameter  effect  
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