• Title/Summary/Keyword: Opimal Design

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A Study on D-Optimal Design Using the Genetic Algorithm

  • Yum, Joon-Keun
    • Communications for Statistical Applications and Methods
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    • v.7 no.1
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    • pp.357-370
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    • 2000
  • This study has adapted a genetic algorithm for an optimal design for the first time. the models that was used a simulation are the first and second order response surfaces model, Using an genetic algorithm in D-opimal it is more efficient than previous algorithms to get an object function. Not like other algorithm without any restrictions like troublesome about the initial solution not falling into a local optimal solution it's the most suitable algorithm.

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The Opimal Parameter Design of Interior Permanent Magnent Synchronous Motor for Electri Vehicle Driver System (전기 자동차 구동용 매입형 영구자속 동기 전동기의 파라메타 최적 설계)

  • Ha, Kyong-Ho;Lim, Ki-Chae;Kang, Gyu-Hong;Hong, Jung-Pyo;Kim, Gyu-Tak;Ku, Dae-Hyun;Park, Jung-Woo;Ha, Hoi-Doo
    • Proceedings of the KIEE Conference
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    • 1997.07a
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    • pp.195-197
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    • 1997
  • In this paper, the optimal design of interior permanent magnet synchronous motors for electric vehicle driver system is achieved to maximize the torque in constant torque region. Initial design is peformed taking into account load characteristics of electric vehicle and we use sequential uncostrained minimization techniques. In the results, the torque in constant torque region is improved about 13.5%.

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Dynamic Behaviors and Optimal Design of an Aircraft Nose Landing Gear using ADAMS (ADAMS를 이용한 항공기 전륜착륙장치의 동적거동해석 및 최적설계)

  • Kim, Sun-Goo;Kim, Cheol;Kim, Young-Man
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.35 no.7
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    • pp.612-618
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    • 2007
  • The dynamic behaviors of a KT-1 family aircraft nose landing gear have been analyzed and the optimal design of an aircraft shock absorber has been conducted to improve efficiency of shock energy absorption. The nose landing gear is modeled as a 2 DOF system using ADAMS and various operational and environmental landing conditions were considered. The results of dynamic simulation for various landing conditions agree well with experiments. Also the effect of parameters of a shock strut on the dynamic behaviors and on shock energy absorption of the nose landing gear has been evaluated for optimal design to define design variables. It has been found that the parameters of a shock strut such as oil-density and orifice area have more effects on dynamic behaviors than those of operation conditions. Optimal design is performed to maximize the efficiency of shock energy absorption using Feasible Direction Method. As a result the design values of the shock strut for maximum efficiency of shock energy absorption are derived and it turns out that efficiency and dynamic behaviors of the nose landing gear were improved by the optimal design.

An Optimal Algorithm for the Design of a Proxy Blind Signature Agent (대리 은닉서명 에이전트의 설계를 위한 최적화 알고리즘)

  • Rhee, Hyunsook
    • Journal of the Korea Society of Computer and Information
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    • v.18 no.7
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    • pp.85-92
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    • 2013
  • In this paper, on the basis of Guilin Wang's proxy signature scheme and the Schnorr blind signature, we propose a secure proxy blind signature scheme. A proxy blind signature scheme is a digital signature scheme which combines the properties of a proxy signature and a blind signature scheme. Guilin Wang proposed a provably secure proxy signature scheme, which is based on a two-party Schnorr signature scheme. Also, using the proposed proxy blind signature scheme, we propose the proxy agent system for the electronic voting. We show the proposed scheme satisfies the security properties of both the blind signature and the proxy signature scheme and is efficient and optimal proxy blind signature scheme.