• Title/Summary/Keyword: defense performance

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Design Methodology for the Enhancement of SSD Performance (SSD 성능 향상을 위한 설계 단계에서의 방법론)

  • Kim, Seung-Wan;Kim, Hun;Youn, Hee-Yong
    • Proceedings of the Korean Society of Computer Information Conference
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    • 2014.07a
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    • pp.231-234
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    • 2014
  • 플래시 메모리는 빠른 처리 속도, 비 휘발성, 저 전력, 강한 내구성 등으로 인해 최근 여러 분야에서 활용도가 증가하고 있다. 또한, 최근 비트 당 가격이 저렴해지면서 NAND 플래시 기반의 SSD (Solid State Disk)가 기존 기계적 메커니즘의 HDD(Hard Disk Drive)를 대체할 새로운 저장 장치로 주목받고 있다. 이 논문에서는 SSD 설계에서 고려해야 할 사항들을 정리하였으며, SSD의 성능향상을 위해 설계 고려사항들에 대한 해결방안을 위한 연구방향을 제시한다.

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FUZZY CONTROL LAW OF HIGHLY MANEUVERABLE HIGH PERFORMANCE AIRCRAFT

  • Sul Cho;Park, Rai-Woong;Nam, Sae-Kyu;Lee, Man-Hyung
    • 제어로봇시스템학회:학술대회논문집
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    • 1998.10a
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    • pp.205-209
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    • 1998
  • A synthesis of fuzzy variable structure control is proposed to design a high-angle-of-attack flight system for a modification version of the F-18 aircraft. The knowledge of the proportional, integral, and derivative control is combined into the fuzzy control that addresses both the highly nonlinear aerodynamic characteristics of elevators and the control limit of thrust vectoring nozzles. A simple gain scheduling method with multi-layered fuzzy rules is adopted to obtain an appropriate blend of elevator and thrust vectoring commands in the wide operating range. Improving the computational efficiency, an accelerated kernel for on-line fuzzy reasoning is also proposed. The resulting control system achieves the good flying quantities during a high-angle-of- attack excursion. Thus the fuzzy logic can afford the control engineer a flexible means of deriving effective control laws in the nonlinear flight regime.

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A Robust Recursive Control Approach to Nonlinear Missile Autopilot (강인 반복 제어를 이용한 비선영 유도탄 자동조종장치)

  • Nam, Heon-Seong;Lyou, Joon
    • Journal of Institute of Control, Robotics and Systems
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    • v.7 no.12
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    • pp.1031-1035
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    • 2001
  • In this paper, a robust recursive control approach for nonlinear system, which is based on Lyapunov stability, is proposed. The proposed method can apply to extended systems including cascaded systems and the stability is guaranteed in the sense of Lyapunov. The recursive design procedure so called “robust recursive control approach” is used to find a stabilizing robust controller and simultaneously estimate the uncertainty parameters. First, a nonlinear model with uncertainties whose bounds are unknown is derived. Then, unknown bounds of uncertainties are estimated. By using these estimates, the stabilizing robust controller is updated at each step. This approach is applied to the pitch autopilot design of a nonlinear missile system and simulation results indicate good performance.

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Research on In-band Spurious Evasion Techniques of Hybrid Frequency Synthesizer

  • Kim, Seung-Woo;Yoo, Woo-Sung
    • Journal of IKEEE
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    • v.19 no.2
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    • pp.176-185
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    • 2015
  • The study aims to a design hybrid frequency synthesizer in spectrum analyzer and to propose new techniques designed for evasion of in-band spurious. The study focuses on calculating the exact location of multiple phase locked loop of hybrid frequency synthesizer and spurious of direct digital synthesizer to evade in-band spurious outside of frequency range that the user wants to see and thereby simulating technique to improve input related spurious of spectrum analyzer for algorithm. The proposed technique is designed to calculate spurious evasion algorithm in central processing system when in-band spurious arises, and to move output frequency of DDS(direct digital synthesizer) into the place where no in-band spurious exists thereby improving performance of frequency synthesizer. The study used simulation and result representation to prove the effectiveness of the proposed technique.

Efficient Search Method of Deperming Protocol for Magnetic Silence of Vessel

  • Kim, Jong-Wang;Kim, Sang-Hyun;Kim, Ji-ho;Lee, Hyang-Beom;Chung, Hyun-Ju
    • Journal of Magnetics
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    • v.22 no.1
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    • pp.85-92
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    • 2017
  • This research is proposed with the efficient searching method of deperming protocol for magnetic silence. The deperming protocol has been changed depending on the initial magnetic field, the final magnetic field, and the shot number, so deciding parameter is highly important. Therefore, in this paper, the value of the initial magnetic field is supposed to be fixed to that of the saturation field, and excluding the initial magnetic field in the variable, the deperming protocol has been analyzed depending on the final magnetic field and the change of the shot number. In the result of this experiment, the final magnetic field gets high performance to the reverse of the direction of the initial magnetization, and it is resulted that the shot number inverse proportion to the size of the final magnetic field.

A Study on the Nozzle-Rotor Interactions of Partial Admission Supersonic Turbines

  • Seong, Young-sik;Han, Seong-hoon;Kim, Kui-soon;Park, Chang-kyu
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2004.03a
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    • pp.391-397
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    • 2004
  • The performance characteristics of partial admission supersonic turbines are analyzed by using the commercial CFD program FLUENT6.0. The governing equations were discretized with Euler implicit method in time and 2nd-order upwind scheme of FVM in space. The k-$\varepsilon$ turbulence model was utilized to describe the turbulent flow field. In order to investigate the nozzle--rotor interactions and the effect of partial admission, the flows in supersonic turbine rotor cascades with a nozzle are computed. Extensive computations of partial admission supersonic turbines provide the shock structures and flow patterns in the nozzle and rotor. It is clearly shown that the nozzle flow is highly affected by the shocks or expansion waves propagated from the rotor leading edge. And the rotor flow is also affected by the shocks or wakes originated from the nozzle.

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Comparative electrochemical study of sulphonated polysulphone binded graphene oxide supercapacitor in two electrolytes

  • Mudila, Harish;Zaidi, M.G.H.;Rana, Sweta;Alam, S.
    • Carbon letters
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    • v.18
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    • pp.43-48
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    • 2016
  • Sulphonated polysulphone (SPS) has been synthesized and subsequently applied as binder for graphene oxide (GO)-based electrodes for development of electrochemical supercapacitors. Electrochemical performance of the electrode was investigated using cyclic voltammetry in 1M Na2SO4 and 1M KOH solution. The fabricated supercapacitors gave a specific capacitance of 161.6 and 216.8 F/g with 215.4 W/kg and 450 W/kg of power density, in 1M Na2SO4 and 1M KOH solutions, respectively. This suggests that KOH is a better electrolyte than Na2SO4 for studying the electrochemical behavior of electroactive material, and also suggests SPS is a good binder for fabrication of a GO based electrode.

A Study on the Hopfield Network for automatic weapon assignment (자동무장할당을 위한 홉필드망 설계연구)

  • 이양원;강민구;이봉기
    • Journal of the Korea Institute of Information and Communication Engineering
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    • v.1 no.2
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    • pp.183-191
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    • 1997
  • A neural network-based algorithm for the static weapon-target assignment (WTA) problem is Presented in this paper. An optimal WTA is one which allocates targets to weapon systems such that the total expected leakage value of targets surviving the defense is minimized. The proposed algorithm is based on a Hopfield and Tank's neural network model, and uses K x M processing elements called binary neuron, where M is the number of weapon platforms and K is the number of targets. From the software simulation results of example battle scenarios, it is shown that the proposed method has better performance in convergence speed than other method when the optimal initial values are used.

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Research on the Penetrator Characteristics and Flight Stability of Explosively Formed Penetrator (EFP 관통자 특성과 비행 안정성에 대한 연구)

  • Yi, Youngsun
    • Journal of the Korea Institute of Military Science and Technology
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    • v.23 no.4
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    • pp.355-362
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    • 2020
  • EFP composed of explosive, charge and liner generally penetrates standoff a target by Monroe effect. Its performance highly depends on penetrator characteristics and flight stability. Penetration ability can be dramatically reduced when the penetrator reaches the target with AOA, even if the penetrator has high kinetic energy and L/D ratio. Therefore, it is important to research not only penetrator characteristics and but also flight stability. In this work, the effect of liner shape on penetrator characteristics was examined using free flight test and numerical tools. It was found that tip velocity of penetrator was increased with decreasing liner thickness. It was also found that thicker liner had higher static margin leading to better flight status.

A Study on Effective ATM Multi-Path Routing Method (효율적인 ATM 다중 경로 라우팅 기법에 관한 연구)

  • Go, Jang-Hyeok;Lee, Dong-Ho
    • The Transactions of the Korea Information Processing Society
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    • v.6 no.3
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    • pp.681-691
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    • 1999
  • It was already proved that ATM stability and flexibility of service application, but because of the various characteristics of traffics and the QoS on user demand caused by them, there are a lot of researches for traffic management method. However, there are a few of researches for ATM routing method acting on traffic management practically. In this paper, we focus on multi-path routing method transporting cells with multiple paths and compare this method with existing single path routing method and analyze multi-path routing method into three elements with simple formula and propose anew methods improving the performance of ATM routing and simulate these methods.

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