• Title/Summary/Keyword: Anti-ship missile

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Roll Compensation for Homing Seekers with 2-Axis Gimbal (2축 김발 호밍 탐색기에서의 롤운동 보상)

  • Whang, Ick-Ho
    • Proceedings of the KIEE Conference
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    • 2001.07d
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    • pp.1932-1934
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    • 2001
  • In this paper, a horizontal LOS(line of sight) rate estimator for conventional sea skimming ASM(anti-ship missile) is proposed. A LOS rate dynamics model in 2 axis gimbal system and in homing geometry is derived. And a new LOS rate estimator is proposed by applying a Kalman filter theory to the LOS rate dynamics model. The proposed filter can estimate LOS rates with taking roll motions into account. Simulation results show the proposed filter produces smaller estimation errors than a conventional method.

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A Study on the Setting Procedure of Standard Value and Design Target Value for the RCS Reduced Design for Naval Ships (함정 RCS 기준치 및 설계 목표치 설정을 위한 절차 연구)

  • An, Byeongjun;Seo, Sangkui
    • The Journal of Korean Institute of Electromagnetic Engineering and Science
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    • v.26 no.6
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    • pp.581-588
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    • 2015
  • In this paper, we researched that setting standard for RSC(Radar Cross Section) of naval surface ship could be determined and considered in various ways on ship's survivability, technical building feasibility, operation and so on. This study presented fundamental capacity on anti-ship missile, radar, flight and so no and the procedure to set of target/standards for RSC. The RCS standards is good at setting low as low as to improve survivability aspect, but because we should consider effect, technical limit, cost etc, this paper analyzed necessary elements to set standard than to suggest specific number and suggested procedure to set standars according to suggest the boundary of RCS.

Ducted Rocket Propulsion System Development Proposal (Ducted Rocket의 현황과 추진기관 개발방안)

  • Lee Jun-Ho;Choi Sung-Han;Hwang Jong-Sun
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2005.11a
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    • pp.475-478
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    • 2005
  • Ducted rocket produces thrust by 2 steps, primary incomplete combustion in the gas generator, and secondary complete combustion reaction in combustion chamber mixed by air taken through duct. the range of a rocket is determined by the weight of propellant, especially the weight of fuel. So ducted rocket has more efficiency and high terminal speed compared to traditional solid rocket motor. This propulsion system expected to be applied to various kinds of missile for anti-aircraft, anti-ship

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Analysis of the Combat Effectiveness of FFG with Guided-Rocket on the Threats of Multiple USV (다수 무인수상정 위협에 대한 호위함용 유도 로켓의 전투효과도 분석)

  • MIN, Seungsik;OH, Kyungwon;RYU, Jaekwan
    • Journal of Aerospace System Engineering
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    • v.14 no.5
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    • pp.58-65
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    • 2020
  • In this paper, the combat effectiveness of ship guidance rockets to counter the threat of multiple USV(Unmanned Surface Vehicle) was analyzed in three cases. The probability of sinking a number of USVs approaching by distance was compared using various weapon systems and guided rocket systems installed on the naval vessels. As a result of the analysis, it was found that the combat effectiveness of the guided rocket was improved compared to the close defense system of the anti-ship missile installed on the naval vessels.

Tracking Error Performance of Tracking Filters Based on IMM for Threatening Target to Navel Vessel

  • Fang, Tae-Hyun;Choi, Jae-Weon
    • International Journal of Control, Automation, and Systems
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    • v.5 no.4
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    • pp.456-462
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    • 2007
  • Tracking error performance is investigated for the typical maneuvering pattern of the anti-ship missile for tracking filters based on IMM filter in both clear and cluttered environments. Threatening targets to a navel vessel can be categorized into having three kinds of maneuvering patterns such as Waver, Pop-Up, and High-Diver maneuvers, which are classified according to launching platform or acceleration input to be applied. In this paper, the tracking errors for three kinds of maneuvering targets are represented and are investigated through simulation results. Studying estimation errors for each maneuvering target allows us to have insight into the most threatening maneuvering pattern and to construct the test maneuvering scenario for radar system validation.

A new concept for blast hardened bulkheads with attached aluminum foam

  • Kim, Sung-Ho;Woo, Heekyu;Choi, Gul-Gi;Yoon, Kyungho
    • Structural Engineering and Mechanics
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    • v.65 no.3
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    • pp.243-250
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    • 2018
  • The use of blast hardened bulkheads (BHBs) is an effective vulnerability hardening technique for improving the survivability of naval warships when internal explosions occur due to being shot by an anti-surface missile. In this paper, a new concept of BHBs reinforced by aluminum (Al) foam is proposed. The new concept can significantly reduce the blast pressures transferred to bulkheads and, unlike conventional BHBs, can be easily installed to operating naval warships. Chamber model blast tests were performed to demonstrate the effectiveness of the Al-foam BHBs and the results are further supported by numerical simulations. Finally, a practical preliminary is proposed for the Al-foam BHBs.

A LOS Rate Estimator for Homing Seekers with 2 Axis Gimbal System (2축 김발 호밍 탐색기를 위한 시선변화율 추정기법)

  • Whang, Ick-Ho;Hwang, Tae-Won
    • Journal of Institute of Control, Robotics and Systems
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    • v.7 no.12
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    • pp.1024-1030
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    • 2001
  • In this paper, a horizontal LOS(line of sight) rate estimator for conventional sea skimming ASM(anti-ship missile) is proposed. A LOS rate dynamics model for a 2-axis gimbal system and the homing geometry is derived. A new LOS rate estimator is proposed by applying the Kalman filter theory to the LOS rate dynamics model. The proposed filter estimates LOS rates by taking roll motions into account. Simulation results show that the proposed filter produces smaller estimation errors than a conventional method.

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A Research on Naval Electronic Warfare System Engagement HILS Technology (해상 전자전체계 조우 HILS 연구)

  • Shin, Dong-Cho;Lee, Jeong-Hoon;Ryu, Si-Chan
    • Journal of the Korea Institute of Military Science and Technology
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    • v.13 no.5
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    • pp.785-792
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    • 2010
  • This paper on the Research of Naval Electronic Warfare System HILS(Hardware In the Loop System) describes the EW engagement HILS construction method for evaluation of the operational concept analysis on active RF Decoy in staying in the air and the deceit ability to anti-ship missile seeker. We obtain the EW M&S technology of EW engagement HILS and EW efficiency analysis from this project. This Naval Electronic Warfare System HILS technology will support Active Decoy Development Project and any other HILS of EW weapon in KOREA ARMY/NAVY/AIR FORCE.

A Design Method of the Simulation Program for HILS (HILS를 위한 시뮬레이션 프로그램 설계 기법)

  • Park, Haerhee;Jeon, In-Soo;Song, Chang-Joon
    • Journal of the Korea Institute of Military Science and Technology
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    • v.16 no.4
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    • pp.435-440
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    • 2013
  • In this paper, a design method of the simulation program for HILS(Hardware-In-the-Loop Simulation) system is proposed. The present method consists of definition of requirements for HILS, development of specifications, and implementation of the program to satisfy the specifications. In the implementation of the program, the application of hardware interface and the concept of structural modularization are proposed to satisfy the specifications. The concepts of CSCI(Computer Software Configuration Item) and encapsulation are used for structural modularization. The proposed method was practically applied to the development of the simulation program for the efficient operation in HILS of an anti-ship missile system.

A Passive Ranging Filter with Initial Range Error Compensation (초기 거리오차 보상 피동 거리 추정 필터)

  • 황익호;정상근
    • Journal of the Korea Institute of Military Science and Technology
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    • v.5 no.2
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    • pp.185-194
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    • 2002
  • To extract relative ranges from LOS(line of sight) information, we propose a passive ranging filter which is suitable for anti-ship missiles in HOJ(home on jam) mode. The proposed filter is devised to cope with the case that a passive ranging filter may include a large initial range estimation error since modem jammers are capable of very long range jamming. In addition, under the assumption that the missile motion is dominant over the HOJ engagement situation, the engagement geometry is modeled by a second order system. A new passive ranging filter is proposed by constructing an extended Kalman filter(EKF) based on the model. And then a least square initial state error estimation algorithm is attached to the EKF. Simulation results show that the proposed filter has a good range estimation performance with small computational load.