[1]段齐骏,张福祥.舰载多管火箭武器系统发射姿态控制对策[J].南京理工大学学报(自然科学版),2002,(06):595-598.
 DuanQijun ZhangFuxiang.The Countermeasure for Launching Attitude Control of Ship-based Multi-rocket System[J].Journal of Nanjing University of Science and Technology,2002,(06):595-598.
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舰载多管火箭武器系统发射姿态控制对策()
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《南京理工大学学报》(自然科学版)[ISSN:1005-9830/CN:32-1397/N]

卷:
期数:
2002年06期
页码:
595-598
栏目:
出版日期:
2002-12-30

文章信息/Info

Title:
The Countermeasure for Launching Attitude Control of Ship-based Multi-rocket System
作者:
段齐骏张福祥
南京理工大学机械工程学院, 南京210094
Author(s):
DuanQijun ZhangFuxiang
School of Mechanical Engineering,NUST,Nanjing 210094
关键词:
火箭 舰船 发射系统
Keywords:
rocket ship launching system wave
分类号:
TJ762.3
摘要:
实施舰载多管火箭武器系统发射姿态控制的目的 ,是提高火箭发射的精度。火箭发射过程中 ,载体存在 2种形式的振动 :随波振动和燃气流造成的冲击振动。因此系统的发射精度同时与船体的运动及发射系统的动力学结构特征等两方面因素密切相关。该文通过研究船体在火箭发射时的姿态及各姿态下火箭武器的发射特性 ,对发射时船体姿态求优 ,获得了对系统发射姿态实施控制的有效途径
Abstract:
Carrying out launching at titude cont rol is to increase the high concent rat ion of rocket . During the launching, ships have tw o ty pes of vibrat ion stimulated by wave and the force of exhaust gas, so the precision w ill be closely related to the ship mot ion and the feature of dy namic st ructure of launching system. By studying the launching at titude of ship and the launch ing characterist ics of rocket weapon under different at t itudes, the optimum att itude of ship for launching is selected. An effect ive w ay of cont rolling the at titude of system can be obtained.

参考文献/References:

1  彭英声. 舰船耐波性基础. 北京: 国防工业出版社, 1988
2   段齐骏. 舰载多管火箭武器系统发射动力学及其耐波性研究: [ 博士学位论文] . 南京: 南京理工大学, 2001
3 段齐骏, 邱亚峰, 张福祥. 舰载武器装备发射精度与载体运动关系研究. 弹道学报, 2000,12( 2) : 60~ 64
4   段齐骏, 邱亚峰, 张福祥. 陆基武器移植对舰船的要求. 南京理工大学学报, 2000, 24( 4) :299~ 301

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备注/Memo

备注/Memo:
国防科技预研行业基金资助项目
段齐骏  女  38 岁  副教授  博士
更新日期/Last Update: 2002-12-30