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论文:2012,Vol:30,Issue(5):706-711 |
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引用本文： |
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王司令, 宋保维, 段桂林, 张克涵. 高空远程滑翔鱼雷控制系统设计与仿真[J]. 西北工业大学 |
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Wang Siling, Song Baowei, Duan Guilin, Zhang Kehan. An Effective Design and Simulation of Control System for High Altitude Long-Range Gliding Torpedo[J]. Northwestern polytechnical university |
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| 高空远程滑翔鱼雷控制系统设计与仿真 |
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| 王司令1, 宋保维1, 段桂林2, 张克涵1 |
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1. 西北工业大学 航海学院, 陕西 西安 710072;
2. 中船重工第 710 所, 湖北 宜昌 443003 |
| 摘要: |
| 针对已有的滑翔鱼雷进行改进,提出一种新型的高空远程滑翔鱼雷。这种滑翔鱼雷通过加装在鱼雷腹部的助推火箭进行低空突防,以实现远距离打击敌方潜艇的目的。分析高空远程滑翔鱼雷的工作流程,分别建立了无动力滑翔段、低空突防段和反推减速段六自由度非线性运动学和动力学模型。指出三段弹道的特点,并进行弹道设计,提出控制系统的总体要求并设计各弹道相应的控制律。基于MATLAB Simulink中Air-Weapons-Torpedoes工具箱设计仿真平台,结合总体方面计算出的流体动力参数对空中全弹道进行仿真。结果显示在该控制律下,高空远程滑翔鱼雷具有明显的增程效果和一定的突防能力,实现了预先设计的弹道。 |
| 关键词:
滑翔
鱼雷
建模
飞行控制
弹道仿真
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| An Effective Design and Simulation of Control System for High Altitude Long-Range Gliding Torpedo |
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| Wang Siling1, Song Baowei1, Duan Guilin2, Zhang Kehan1 |
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1. College of Marine Engineering, Northwestern Polytechnical University, Xi'an 710072, China;
2. CSIC710, Yichang 443003, China |
| Abstract: |
| High altitude long-range gliding torpedo is a new concept of anti-submarine weapon which was put for-ward in recent years.A gliding torpedo was improved in Northwestern Polytechnical University that can attack sub-marines from a remote distance.The air trajectory model and the design of control law are quite important in theconceptual design stage.In the full paper, we explain the trajectory model of the gliding torpedo and the controllaw.In this abstract, we just add some pertinent remarks to listing the two topics of explanation.The first topic istrajectory models.Section 1 develops the three mathematical models of the first topic: aerial gliding trajectory, lowaltitude breaking defense trajectory and the slowing down trajectory.The second topic is the control law on the gli-ding torpedo and it is covered in section 2.In the second topic, the characteristics of the three sections of trajectoryare pointed out and the corresponding control law of each section is put forward.Initial conditions of simulation areshown in Table 2.Finally, the whole aerial trajectory was simulated with MATLAB Simulink.The simulation re-sults are summarized in Figs.2 through 9.The simulation results show preliminarily that the attack range of high al-titude long-range gliding torpedo and the penetration ability can indeed be realized under this control law. |
| Key words:
antisubmarine aircraft
computer simulation
control system analysis
design
efficiency
lineariza-tion
mathematical models
nonlinear systems
optimization
scheduling
schematic diagrams
torpe-does
trajectories;flight control
gliding torpedoes
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| 收稿日期: 2011-11-12
修回日期:
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| DOI: |
| 基金项目: 西北工业大学重点创新项目(2008KJ01001)资助 |
| 通讯作者:
Email： |
| 作者简介: 王司令(1985-)，西北工业大学博士研究生，主要从事水下航行器动力推力系统的设计与控制研究。
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参考文献: |
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[1] 王志杰.研制高空反潜鱼雷的必要性及关键技术.鱼雷技术,2009,19(3):1-4Wang Zhijie.Necessity and Key Technologies for Developing High Altitude Anti-Submarine Torpedo.Torpedo Technology,2009,19(3):1-4 (in Chinese)
[2] 潘 光,吴文辉,毛昭勇.高空远程滑翔鱼雷全弹道仿真关键技术.鱼雷技术,2009,17(4):10-15Pan Guang,Wu Wenhui,Mao Zhaoyong.Key Technologies about Complete Trajectory Simulation for High Altitude Long-RangeGliding Torpedo.Torpedo Technology,2009,17(4):10-15 (in Chinese)
[3] 吴盘龙,薄煜明,胡 瑞.简易制导炸弹坐标系转换的误差分析与修正.兵工学报,2008,29(10):1271-1276Wu Panlong,Bo Yuming,Hu Rui.Error Analysis and Modification of Coordinate Transform of Simplified Guided Bomb.ActaArmamentarii,2008,29(10): 1272-1276 (in Chinese)
[4] 薛晓中,孙传杰.简易制导炸弹方案弹道优化设计.兵工学报,2004,25 (3): 376～378Xue Xiaozhong,Sun Chuanjie.Optimization Design for the Ballistics of Simply Guided Bombs.Acta Armamentarii,2004,25(3): 376-378 (in Chinese)
[5] 李 昕,张 超,马国梁,王旗,王道波.GPS/SINS 制导炸弹建模与弹道仿真.东南大学学报(自然科学版),2008,11(38):168-171Li Xin,Zhang Chao,Ma Guoliang,Wang Qi,Wang Daobo.Modeling and Trajectory Simulation of Guided Bomb Based onGPS/SINS.Journal of Southeast University(Natural Science Edition),2008,11(38):168-171 (in Chinese)
[6] Vinh N X.Optimal Trajectories in Atmospheric Flight.Amsterdam: Elsevier Scientific Publishing Co,1981
[7] Chern J S.Analytical Solution for Horizontal Gliding Flight.AIAA-2000-4113
[8] Vinh N X,Yang C Y,Chern J S.Optimal Trajectories for Maximum Endurance Gliding in a Horizontal Plane.Journal of Guid-ance,Control and Dynamics,1984,7(2): 246-248
[9] Shamma J S.Analysis of Gain-Scheduled Control for Nonlinear Plants.IEEE Trans on Automatic Control,1990,35: 898-907
[10] Shamma J S.Gain Scheduling: Potential Hazards and Possible Remedies.IEEE Trans on Control Systems Magazine,1992,12:101-107
[11] 王永虎.空投雷弹入水冲击响应分析及相关技术研究: [博士学位论文].西安:西北工业大学,2008Wang Yonghu.Dynamic Response Analysis of Airborne Torpedo and Deep-Mine during Water-Entry Impact and Research of theRelative Technology.Ph.D.Thesis,Xi'an: Northwestern Polytechnical University,2008 (in Chinese) |
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