惯性导航系统动基座对准对舰舰导弹捕捉概率的影响

doi:10.3969/j.issn.1000-1093.2016.01.009

摘要/Abstract

摘要： 采用惯性导航系统的舰舰导弹作为海战场最重要的攻击武器，能否快速准确地在舰艇上对导弹捷联惯性导航系统进行初始对准，是影响舰舰导弹捕捉概率的重要因素。动基座对准误差导弹捷联惯性导航系统作为的初始误差，会随着工作时间增长不断累加，导致末制导雷达开机时导弹散布误差和航向误差角不断增大，将致使末制导雷达的捕捉概率下降。基于动基座初始对准误差对导弹飞行控制误差的影响，以目标位置误差圆分布为基础，建立舰舰导弹捕捉概率计算模型，通过不同条件的参数设置，仿真计算出某型舰舰导弹动基座初始对准误差对目标捕捉概率的影响。结果表明捕捉概率近似线性下降，下降值约为静基座对准时的4.2%~6.5%.

关键词: 兵器科学与技术, 舰舰导弹, 初始对准误差, 散布误差, 目标位置误差, 捕捉概率

Abstract: The shipborne ship-to-ship missile with INS is an important attacking weapon in naval battle. Therefore，the rapid and accurate initial alignment of ship’s INS (SINS) on moving ship becomes one of the critical technologies for the shipborne anti-ship missiles. As the initial error of SINS, the alignment error is accumulating over time, which can make the missile dispersion and yaw error angles increase, resulting in the decrease in the acquisition probability of homing radar. Considering the effect of initial alignment error on auto-control terminal error, a calculation model of acquisition probability for ship-to-ship missile is established based on the model of target position error. The influence of initial error of a certain ship-to-ship missile on target acquisition probability is analyzed by setting the different conditions and parameters. The results show that the probability is decreased linearly with 4.2%~6.5% of static alignment.

Key words: ordnance science and technology, ship-to-ship missile, initial alignment error, disperse error, target position error, acquisition probability

中图分类号:

高青伟，曾家有，吴芳，张千宇. 惯性导航系统动基座对准对舰舰导弹捕捉概率的影响[J]. 兵工学报, 2016, 37(1): 56-63.

GAO Qing-wei, ZENG Jia-you, WU Fang, ZHANG Qian-yu. Influence of Alignment of Moving Base for INS on Acquisition Probability of Homing Radar for Ship-to-ship Missile[J]. Acta Armamentarii, 2016, 37(1): 56-63.

参考文献

［1］高青伟，赵国荣，王希彬.传递对准中载舰挠曲变形和杆臂效应一体化建模与仿真[J]. 航空学报，2009，30 (11) ： 2172-2178.
GAO Qing-wei, ZHAO Guo-rong, WANG Xi-bin. Incorporate modeling and simulation of transfer alignment with flexure of carrier and lever-arm effect[J].Acta Aeronautica et Astronautica Sinica, 2009，30(11)：2172-2178. (in Chinese)
[2］徐仕会，冯培德，马红日. 惯导系统在动基座上的对准研究[J]. 兵工学报，2008，29(7)：887-890.
XU Shi-hui, FENG Pei-de, MA Hong-ri.Research on INS alignment with disturbing motion base[J]. Acta Armamentarii, 2008, 29(7)：887-890. (in Chinese)
[3］岳亚洲，李四海，张亚崇，等. 机载主子惯导间误差角估计的差分惯性滤波器设计及性能分析[J]. 航空学报，2013，34(10)：2402-2410.
YUE Ya-zhou, LI Si-hai, ZHENG Ya-chong, et al.Different inertial filter design and performance analysis for estimation of misalignment angle between airborne master INS and slave INS[J].Acta Aeronautica et Astronautica Sinica, 2013, 34(10):2402-2410. (in Chinese)
[4］聂永芳，冯林平，施建礼. 新误差分析方法对舰舰导弹作战使用的影响[J]. 舰船电子工程，2012，32(7)：57-59.
NIE Yong-fang, FENG Lin-ping, SHI Jian-li. Inflenence of a new error measure on the anti-ship missile operation[J].Ship Electronic Engineering, 2012, 32(7):57-59. (in Chinese)
[5］刘毅，刘志俭，吕新广. 初始对准误差对惯性制导误差影响的简化算法[J]. 航天控制，2006，24(2)：30-33.
LIU Yi, LIU Zhi-jian, LYU Xin-guang. A simplified algorithm for calculating the influence of initial alignment error on inertial guidance error[J]. Aerospace Control, 2006, 24(2):30-33. (in Chinese)
[6］程明文，刘勇志. 初始对准误差对目标落入概率影响的简化分析 [J]. 电光与控制，2010，17(10)：90-92.
CHENG Ming-wen, LIU Yong-zhi. Influence of initial alignment error of missile on target acquisition probability[J]. Electronics Optics & Control, 2010, 17(10):90-92. (in Chinese)
[7］郭少军，陆斌. 中末交班及红外误差对捕获跟踪概率的影响分析 [J]. 弹箭与制导学报，2011，31(4)：30-33.
GUO Shao-jun, LU Bin. The analysis of track and acquisition probability influenced by mid-terminal handover error and infrared device error [J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2011, 31(4):30-33. (in Chinese)
[8］曾家有，宋友凯，严建钢. 基于目标位置误差圆分布的舰舰导弹捕捉概率计算模型[J]. 战术导弹技术，2010，17(2)：55-58.
ZENG Jia-you，SONG You-kai，YANG Jian-gang. Acquisition probability computing model of anti-ship missile based on circularity distribution of target position error[J]. Tactical Missile Technology, 2010, 17(2):55-58. (in Chinese)
[9］曾家有.各种因素对现在点射击方式反舰导弹捕捉概率的影响分析[J]. 兵工学报，2011，32(6)：719-724.
ZENG Jia-you. Influence analysis of various factors to acquiring probability of anti-ship missile with shooting at target’s immediate position[J]. Acta Armamentarii, 2011, 32(6): 719-724. (in Chinese)
[10］曾家有,汪浩,孙涛. 反舰导弹末制导雷达最小方位搜索范围确定模型[J]. 航空学报，2009，30(12)：2411-2415.
ZENG Jia-you,WANG Hao,SUN Tao. Model on confirming the minimal searching angle of terminal guidance radar of anti-ship missile[J]. Acta Aeronautica et Astronautica Sinica, 2009, 30(12): 2411-2415. (in Chinese)
[11］陈力，张树森，李军林．反舰导弹目标捕捉概率影响因素分析[J]．火力与指挥控制，2010，35(6)：86-93.
CHEN Li, ZHANG Shu-sen, LI Jun-lin. The analysis on factors to affect the acquiring probability of anti-ship missile to target[J]. Control and Direction of Firepower, 2010, 35(6):86-93. (in Chinese)
[12］徐建志. 反舰导弹捕捉能力建模与仿真[J]. 系统仿真学报，2008，20(4)：874-877.
XU Jian-zhi. Modeling and simulating for anti-ship missile’s catching capability[J]. Journal of System Simulation,2008, 20(4): 874-877. (in Chinese)
[13］ Lu F X, Wu L. Calculation of the potential distribution area of the target in bi-station bearing crossing locating[C]∥2008 Congress on Image and Signal Processing. Sanya, China:IEEE，2008: 422-425.
[14］常皓,徐文旭,齐占元. 导弹作战过程误差传递及末制导捕获概率分析[J]. 弹箭与制导学报，2008，28(3)：81-84.
CHANG Hao, XU Wen-xu, QI Zhan-yuan. Analysis of the eachposition error on operational process and the terminal guidance missile’s probability acquisition[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2008, 28(3):81-84.(in Chinese)
[15］赵辉，沈闽锋，许士海. 反舰导弹超视距攻击捕捉概率模型研究[J]. 舰船电子工程，2008，28(1)：56-58.
ZHAO Hui, SHEN Min-feng, XU Shi-hai. Studies on model of target catching probability for anti-ship missile over the horizon[J]. Ship Electronic Engineering, 2008, 28(1):56-58. (in Chinese)
[16］汪新刚. 反舰导弹目标捕捉概率模型分析[J]. 战术导弹控制技术，2006(3)：104-106.
WANG Xin-gang. Model analysis of target capture probability for anti-ship missile [J]. Control Technology of Tactical Missile,2006 (3): 104-106. (in Chinese)
[17］王光辉. 末制导雷达初始搜索点对目标捕捉概率的影响[J]. 弹箭与制导学报，2002，22(3)：135-137.
WANG Guang-hui. Capture probability emulation of homing radar beginning to search at different position [J]. Transaction of Missile Rocket and Guidance, 2002, 22(3):135-137. (in Chinese)
[18］赵建军, 王光辉. 反舰导弹自控终点误差散布及其改进 [J]. 火力与指挥控制，2003，28(5)：12-14.
ZHAO Jian-jun,WANG Guang-hui. The error spreading and improving of auto-control terminal point of anti-ship missiles [J]. Fire Control & Command Control, 2003, 28(5):12-14. (in Chinese)
[19］徐建萍，汤国建. 反舰导弹目标捕捉概率的研究[J]. 战术导弹控制技术，2008(6)：45-48.
XU Jian-ping, TANG Guo-jian. Research on acquisition probability of anti-ship missile [J]. Control Technology of Tactical Missile, 2008(6):45-48. (in Chinese)

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