雷伞系统稳定特性及控制技术研究  

Stability Characteristics and Control Technology ofTorpedo-Parachute System

作　　者：程文鑫 张峻峰 汪帅 刘坚 CHENG Wenxin;ZHANG Junfeng;WANG Shuai;LIU Jian(Program Management Center of Naval Armament Department,Beijing 100071,China;The 705 Research Institute,ChinaState Shipbuilding Corporation Limited,Xi’an 710077,China;Unit 92840th,the People’s Liberation Army of China,Qingdao266404,China)

机构地区：[1]海装装备项目管理中心,北京100071 [2]中国船舶集团有限公司第705研究所,陕西西安710077 [3]中国人民解放军92840部队,山东青岛266404

出　　处：《水下无人系统学报》2023年第3期488-494,共7页Journal of Unmanned Undersea Systems

摘　　要：随着火箭助飞鱼雷入水速度越来越高,鱼雷入水安全性对入水姿态变化越来越敏感,而在雷伞系统降落过程中,极易出现圆锥摆运动,导致鱼雷入水时攻角过大,巨大的击水载荷会使鱼雷结构发生破坏。为提高鱼雷入水安全性,需采取一定的稳定控制措施,有效减小鱼雷入水前攻角。文章结合雷伞系统多体运动仿真模型和基于脉冲姿控发动机的姿态控制策略开展雷伞系统姿态控制技术研究,对鱼雷入水前的雷伞弹道和带伞姿控过程进行了仿真,仿真结果表明,当降落伞锥摆频率与鱼雷摆动频率接近时鱼雷才会出现明显的锥摆运动,而通过引入姿控过程破坏鱼雷自身锥摆频率可以显著减小降落伞锥摆对鱼雷的影响,使得在一定条件下带伞姿控可以取得很好的姿态控制效果。The safety of a rocket-assisted torpedo entering water becomes more sensitive to the water-entry angle as the water-entry speed of the torpedo increases.Conical pendulum motion is likely to occur during the descent of the torpedo-parachutesystem.The pendulum movement causes the torpedo to have an excessively large angle of attack when it enters the water,resulting in a large impact load that damages the torpedo.To prevent structural damage to the torpedo as it enters the water,itis necessary to reduce the angle of attack before the torpedo enters the water.In this study,the multi-body motion simulationmodel of the torpedo system and the attitude-control strategy based on pulse attitude control engine are combined to analyzethe attitude-control technology of the torpedo system.Simulation results indicated that when the frequency of the conicalpendulum motion of the parachute was close to that of the torpedo,the torpedo had obvious conical pendulum motion,and theinfluence of the parachute on the torpedo could be significantly reduced by introducing the attitude-control process to changethe conical pendulum frequency of the torpedo.Thus,under certain conditions,attitude control of the torpedo with theparachute can achieve feasible results.

关 键 词：火箭助飞鱼雷 雷伞系统 姿控发动机 

分 类 号：TJ63[兵器科学与技术—武器系统与运用工程]