直升机搜潜协同子区域划分模型研究

doi:10.7527/S1000-6893.2013.0183

Abstract

Abstract:

This paper analyzes the defects of several conventional models on subsets of anti-submarine searching region division, and establishes controllable search efficiency models of dipping sonar and sonar buoys carried by helicopter (s) which take into consideration detecting probability. Then subsets of searching region division models are established based on the controllable search efficiency models. Simulations and analysises were done using the controllable search efficiency models. The results of simulations performed in this study demonstrate that the controllable searching region division models can meliorate insufficiencies of conventional models. Besides, the proposed models exhibit advantages in terms of average detecting probability, model applicability, etc.

Key words: helicopters, region coordination, subset of searching region, equivalent search area, controllable searching efficiency, detecting probability

CLC Number:

QI Xuewen, YAN Jian'gang, YANG Dawei, GAO Dongfei. Study on Subsets of Searching Region Division Models of Coordinated Anti-submarine by Helicopters[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2013, 34(11): 2599-2606.

References

[1] Lentz F C.Integration of ASW helicopter operations and environment into NPSNET.Monterey: Naval Postgraduate School,1995: 11-70.

[2] Abbatiello J J.British naval aviation and the anti-submarine campaign.London: Department of War Studies,King's College London,2004: 70-160.

[3] Chuan E C K.A helicopter submarine search game.Monterey: Naval Postgraduate School,1988.

[4] Ketter T N.Anti-submarine warfare in the 21st century.Newport: Naval War College,2004: 4-14.

[5] Dawson H C,Jr.Anti-submarine warfare: still an essential warfare art.ADA263556,1993.

[6] Zhang L,Zhu L,Gu Q.The modeling method of joint mobile formation antisubmarine research in the surface ship and helicopter coordination.Command Control & Simulation,2012,34(2): 14-17.(in Chinese) 张磊,朱琳,顾颀.舰艇编队舰机协同反潜警戒模型研究.指挥控制与仿真,2012,34(2): 14-17.

[7] Chen Z L.New concept of U.S.Navy anti-submarine warfare.Submarine Academic Research,2005,23(1): 74-75.(in Chinese) 陈忠礼.美海军反潜作战新概念.潜艇学术研究,2005,23(1): 74-75.

[8] Wu X H,Shen P H,Fan H G.Research on antisubmarine region of ship carried helicopter.Journal of Naval Aeronautical Engineering Institute,2009,24(2): 229-232.(in Chinese) 吴晓海,沈培华,樊洪港.舰载直升机反潜区域探讨.海军航空工程学院学报,2009,24(2): 229-232.

[9] Wei D P,Zhao H Y.The optimal area search model.China Science and Technology Information,2012(16): 55,58.(in Chinese) 魏东平,赵洪雅.最优区域搜索模型.中国科技信息,2012(16): 55,58.

[10] Yang R J,He Y,Sun M T.Scope analysis for active/passive combined multi-base air anti-submarine.Acta Aeronautica et Astronautica Sinica,2004,25(4): 381-384.(in Chinese) 杨日杰,何友,孙明太.主/被动联合多基地航空搜潜范围分析.航空学报,2004,25(4): 381-384.

[11] Tracey P A.Some priorities for a target probability area.ADA085057,2001.

[12] Qu Y P.Effectiveness evaluation and decision modeling on searching submarine of antisubmarine aircrafts.Beijing: National Defense Industry Press,2011: 69-72.(in Chinese) 屈也频.反潜飞机搜潜效能评估与决策建模.北京: 国防工业出版社,2011: 69-72.

[13] Zhao X M,Sun M T.Discussion on search efficiency model of dipping sonobuoy.Electronics Optics & Control,2005,12(2): 37-41.(in Chinese) 赵绪明,孙明太.吊放声纳搜索效率模型探讨.电光与控制,2005,12(2): 37-41.

[14] Cong H R,Shen P Z,Meng X C.A coordinated submarine searching method used for sector searching area and its effectiveness simulation.Electronics Optics & Control,2011,18(12): 9-13.(in Chinese) 丛红日,沈培志,孟祥超.针对扇形应召搜索区的一种直升机协同搜潜方法及其效能仿真.电光与控制,2011,18(12): 9-13.

[15] Wang Z G,Zhao X Z.Dipping position analysis of "segmentation sector method" anti-submarine by helicopters.Military System Engineering,2000(2): 20-24.(in Chinese) 王在刚,赵晓哲.直升机"分割扇面法"搜潜时的吊点位置分析.军事系统工程,2000(2): 20-24.

[16] Sun M T,Wang T,Zhao X M.Modeling and simulation the efficiency of the dipping sonar on the antisubmarine helicopter.Fire Control and Command Control,2005,30(3): 33-36.(in Chinese) 孙明太,王涛,赵绪明.反潜直升机吊声搜潜效能的建模仿真.火力与指挥控制,2005,30(3): 33-36.

[17] Bao X L,Xie L Z,Zhai L X.The using of aviation sonobuoys in anti-submarine operations.China High Technology Enterprises,2009(12): 46-47.(in Chinese) 包小林,谢灵珠,翟丽雪.航空声纳浮标在反潜作战中的使用.中国高新技术企业,2009(12): 46-47.

[18] Sheng Z,Xie S Q,Pan C Y.Probability theory and mathematical statistics.Beijing: Higher Education Press,2001: 56-62.(in Chinese) 盛骤,谢式千,潘承毅.概率论与数理统计.北京: 高等教育出版社,2001: 56-62.

Study on Subsets of Searching Region Division Models of Coordinated Anti-submarine by Helicopters

PDF (PC)

Knowledge

Abstract

Cite this article

share this article

References

Related Articles 15

Recommended Articles

Metrics

Comments

[1]	SUN Canfei, HUANG Linran, SHEN Yong. Fault diagnosis of helicopter planetary gear transmission system under complex operating conditions [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(8): 625480-625480.
[2]	YANG Zongyao, ZHANG Jingzhou, SHAN Yong. Effects of slot-inlet arrangement at infrared-suppressor-integrated rear airframe on flow organization and infrared radiation characteristics [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(7): 124445-124445.
[3]	CHEN Yaping, YU Jianjian, HU Lei, WANG Yutang. Characteristics and application of bending moments of helicopter rotor shaft [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(5): 524168-524168.
[4]	LI Yanqing, XUAN Yimin. Coupling analysis method for helicopter thermal management and infrared radiation characteristics [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(3): 124270-124270.
[5]	WANG Luofeng, CHEN Renliang. Rigid-elastic coupled flight dynamic modeling and air resonance stability analysis for heavy lift helicopter [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(12): 124634-124634.
[6]	HU Zhou, WANG Zhisheng, WANG Congqing. Decoupling Control Algorithm of Helicopter with Input Saturation Based on Information Fusion [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2014, 35(5): 1394-1403.
[7]	LIU Yang, XIANG Jinwu. Effect of the Trailing Edge Flap on Dynamic Stall Performance of Helicopter Rotor Airfoil [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2013, 34(5): 1028-1035.
[8]	WANG Bo, ZHAO Qijun, ZHAO Guoqing, XU Guohua. Experimental Research and Numerical Analysis on Aerodynamic Characteristics of Rotors with Improved CLOR Blade-tip [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2013, 34(2): 235-245.
[9]	PAN Chengxiong;ZHANG Jingzhou;SHAN Yong. Modeling and Analysis of Helicopter Skin Temperature Distribution [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2011, 32(2): 249-256.
[10]	SONG Laishou, XIA Pinqi. Coupled Fuselage/Piezoelectric Stack Actuator Optimization Method for Active Vibration Control of Helicopter [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2011, 32(10): 1835-1841.
[11]	Yang Jianling;Zhang Liyan;Zhou Shaohua;Fang Yonghong;Huang Wenjun. Geometric Modeling of Composite Helicopter Rotor Blade Plies [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2010, 31(1): 191-197.
[12]	Feng Yachang;Du Huifang. CONTROL SYSTEM OF SEMI DIFFERENTIAL YAWING FOR COAXIAL HELICOPTERS [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1997, 18(1): 117-119.
[13]	Yang Yidong;Yuan Weidong. HELICOPTER VIBRATION REDUCTION TECHNIQUE WITH HARMONIC ACTIVE CONTROL [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1996, 17(5): 55-60.
[14]	Wang Zili. INVESTIGATION OF RELIABILITY AND MAINTAINABILITY PARAMETERS FOR HELICOPTERS [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1995, 16(S1): 20-27.
[15]	Cao Yihua. OPERATION REQUIREMENTS OF TURRETED GUN IN HELICOPTER AIR COMBAT AND MATHEMATIC INVERSE SOLUTION [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1995, 16(3): 22-29.