• Title/Summary/Keyword: Active decoy

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Effective Response Time Verify of Active Decoy Against Anti-Ship Missile Using DEVS Simulation (DEVS 시뮬레이션을 사용한 능동기만기의 대함미사일에 대한 효과적인 대응시간 검증)

  • Choi, Soon-Ho;Cho, Tae-Ho
    • Journal of the Korean Institute of Intelligent Systems
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    • v.25 no.5
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    • pp.495-501
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    • 2015
  • Abroad warships are confronted with various menaces. The most critical threat of the warship is an Anti-Ship Missile (ASM). The ASM is able to be launched at a variety of environments and platforms. The ASM can evades conventional naval radar systems and electronic countermeasure techniques for providing a fatal damage to the warship. To cope with the ASM, an active decoy is an effective method to minimize the direct damage to the warship. The active decoy increases survivability of the warship because the ASM can lure pursuit of the active decoy instead of the warship. In this paper, our proposed method verifies an available response time of the active decoy to deal with the ASM using the active decoy of the warship in marine environments. We defined models of the warship, the ASM, and the active decoy, and executed simulation by combining the models. By the simulation result, the proposed method demonstrated the superiority of the mobile active decoy of the response time decoy among various active decoys, and estimated a protection area to prevent the ASM according the response time of the mobile active decoy against the ASM.

Evaluation of Effective Jamming/Deception Area of Active Decoy against Ground Tracking Radars on Dynamic Combat Scenarios (동적 교전 시나리오에서 지상 추적 레이다에 대한 이탈방사체의 효과적 재밍/기만 영역 분석)

  • Rim, Jae-Won;Lee, Sangyeob;Koh, Il-Suek;Baek, Chung;Lee, Seungsoo
    • The Journal of Korean Institute of Electromagnetic Engineering and Science
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    • v.28 no.4
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    • pp.269-278
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    • 2017
  • We analyze the jamming/deception performance of an active decoy against ground tracking radars on dynamic combat scenarios. Based on the movement and the interference flow of an airborne platform, the trajectories of the active decoy is accurately calculated by solving 6-degree of freedom equations of motion. On realistic combat scenarios, numerical simulations are examined to analyze the jamming performance of the decoy for various movements of the platform and RF specifications of the active decoy. Effective jamming/deception area against the ground tracking radars is estimated from the simulation.

Engagement-Scenario-Based Decoy-Effect Simulation Against an Anti-ship Missile Considering Radar Cross Section and Evasive Maneuvers of Naval Ships

  • Kim, Kookhyun
    • Journal of Ocean Engineering and Technology
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    • v.35 no.3
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    • pp.238-246
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    • 2021
  • The survivability of a naval ship is the ability of the ship and its onboard systems to remain functional and continue a designated mission in man-made hostile environments. A passive decoy system is primarily used as a weapon system for improving the survivability of a naval ship. In this study, an engagement scenario-based simulation program was developed for decoy effectiveness assessments against an anti-ship missile (ASM), which tracks a target with sea-skimming and active radar homing. The program can explain the characteristics of a target ship, such as the radar cross section and evasive maneuvers, as well as the operational performance of the onboard decoy system, the guidance method of the ASM, and the engagement environment's wind speed and direction. This paper describes the theory and formulations, configuration, and user interface of the developed program. Numerical examples of a decoy effect assessment of a virtual naval ship against an ASM are presented.

Survivability for Airborne Platform on Encounter Scenarios where Repeater-type Active Decoy Counteracts Active RF Seeker System Operating Based on PN Guidance Law (PN 유도 기반 능동 RF 탐색기 조우 시나리오에서 반복형 능동 유인체 대응에 따른 공중 플랫폼 생존성 분석)

  • Rim, Jae-Won;Jung, Ki-Hwan;Lee, Hyunsoo;Koh, Il-Suek
    • The Journal of Korean Institute of Electromagnetic Engineering and Science
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    • v.29 no.4
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    • pp.256-265
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    • 2018
  • We herein analyze the survivability of an airborne platform when an active decoy delivers jamming attacks against an active RF seeker system that operates based on the proportional navigation guidance law. In encounter scenarios with various conditions, such as platform maneuvering, the decoy's RF specification, and the seeker's approaching range and angles, the missed distance of the RF seeker is evaluated. By comparing the missed distance with the proximity of the fuze range, the platform's survivability is determined and the survival area of the platform is drawn on several encounter scenarios.

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.

Requirement Analysis of Propulsion System for Active Anti-Ship Missile Decoy (능동형 대함 유도탄 기만기의 추진 시스템 요구 조건 분석)

  • Moon, Yongjun;Kwon, Sejin
    • Journal of the Korean Society of Propulsion Engineers
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    • v.17 no.4
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    • pp.1-9
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    • 2013
  • An active anti-ship missile decoy system was designed conceptually to analyze propulsion system requirements and feasibility to use a liquid bi-propellant rocket engine. Overall mass, size, and shape were assumed referring to specifications of Nulka which was developed by US and Australia in 1990s. The propulsion system was assumed to be a 1,000 N-class $H_2O_2$/kerosene rocket engine with a pressurized feed system. A three-degree-of-freedom optimal trajectory was calculated based on the assumptions, and mass budget was designed from the calculation results. It was found that the requirements for the propulsion system is that it shall be operated more than 100 sec; it shall be re-ignitable; it shall have a throttle capability of a range from 35% to 100% when the maximum thrust at sea level is 1,000 N.

Simulation of Dynamic EADs Jamming Performance against Tracking Radar in Presence of Airborne Platform

  • Rim, Jae-Won;Jung, Ki-Hwan;Koh, Il-Suek;Baek, Chung;Lee, Seungsoo;Choi, Seung-Ho
    • International Journal of Aeronautical and Space Sciences
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    • v.16 no.3
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    • pp.475-483
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    • 2015
  • We propose a numerical scheme to simulate the time-domain echo signals at tracking radar for a realistic scenario where an EAD (expendable active decoy) and an airborne target are both in dynamic states. On various scenarios where the target takes different maneuvers, the trajectories of the EAD ejected from the target are accurately calculated by solving 6-DOF (Degree-of-Freedom) equations of the motion for the EAD. At each sampling time of the echo signal, the locations of the EAD and the target are assumed to be fixed. Thus, the echo power from the EAD can be simply calculated by using the Friis transmission formula. The returned power from the target can be computed based on the pre-calculated scattering matrix of the target. In this paper, an IPO (iterative physical optics) method is used to construct the scattering matrix database of the target. The sinc function-interpolation formulation (sampling theorem) is applied to compute the scattering at any incidence angle from the database. A simulator is developed based on the proposed scheme to estimate the echo signals, which can consider the movement of the airborne target and EAD, also the scattering of the target and the RF specifications of the EAD. For applications, we consider the detection probability of the target in the presence of the EAD based on Monte Carlo simulation.