• Title/Summary/Keyword: Maximizing

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An Exploratory Study on Maximizing Tendency and Continuance Intention of Web Sites

  • Lee, Gyu-Dong;Lee, Jae-Eun;Sanford, Clive
    • Asia pacific journal of information systems
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    • v.20 no.3
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    • pp.73-90
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    • 2010
  • Although research on acceptance of information systems provides useful insights in understanding users' behavior, we need to further understand factors that cause long-term or continued use. This article therefore examines the role of users' maximizing tendency (i.e., individual differences in pursuing the best option) in continuance intention of Web sites. By controlling for disconfirmation, ease of use, and product involvement, we empirically investigate the relationships between satisfaction, usefulness, and continuance intention to online bookstore Web sites. As suggested by the information technology continuance model, the effects of satisfaction to and perceived usefulness on continuance intention to Web sites are positive for individuals with low maximizing tendency (i.e., satisficers). Satisfaction and usefulness, however, are not associated with continuance intention for individuals with a high maximizing tendency (i.e., maximizers). The implications for both researchers and practitioners are discussed.

Optimal Conditions for Maximizing Altitude of Sounding Rocket (사운딩로켓의 고도 극대화를 위한 최적조건)

  • Park, Aeny;Lee, Sang-Hyeon
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2011.11a
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    • pp.144-149
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    • 2011
  • A study to determine the optimal jet conditions for maximizing altitude of the sounding rocket is conducted. The behavior of a simplified linear momentum equation including aerodynamic drag is investigated. The analytic solutions are obtained and compared with numerical solutions. It is shown that there are the optimal jet conditions for maximizing altitude of a sounding rocket according to the rocket mass ratio.

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Maximizing Efficiency Control of Induction Motor for Electric Vehicle Drive Systems (전기자동차 구동용 유도전동기의 최대효율제어)

  • Kim, Jong-Koo;Kim, Myung-Chan;Lee, Jong-Chan
    • Proceedings of the KIPE Conference
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    • 2005.07a
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    • pp.1-3
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    • 2005
  • This paper is to evaluate practical advantage in using maximizing efficiency control strategy in induction motor drives for electric vehicles. A maximizing efficiency control strategy consist of a flux estimation with direct field oriented controller is proposed and compared with the general constant flux control strategy. The comparison is carried out by simulation.

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An Effect of Maximizing Efficiency Control of Induction Motor for Electric Vehicle Drive Systems(II) (전기자동차 구동시스템에서의 유도전동기의 최대효율제어 효과(II))

  • 최욱돈;김동희;노채균
    • Journal of the Korean Institute of Illuminating and Electrical Installation Engineers
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    • v.14 no.5
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    • pp.74-79
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    • 2000
  • This paper presents the test result of electric vehicle to evaluate a point of difference between maximizing efficiency control and conventional constant flux control(CFX) strategy of induction motor driver. A proposed maximizing efficiency control(MEC) strategy is compared with th constant flux control strategy. The comparison test is carried out with two types of F.T.P-72 and E.P.A driving schedule. This research shown the effectiveness of an enlargement of driving distance of the electric vehicle when a maximizing efficiency control strategy adopted.

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Design of Sensitivity-Maximizing Input for Submersibles' Manoeuvring Coefficients using Genetic Algorithm Technique (유전 알고리즘을 이용한 수중운동체 조종성미계수의 민감도 최대화 입력 설계)

  • Yeo, Dong-Jin;Rhee, Key-Pyo
    • Journal of the Society of Naval Architects of Korea
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    • v.43 no.2 s.146
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    • pp.156-163
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    • 2006
  • The accuracy of estimates of hydrodynamic coefficients can be increased by using sensitivity-maximizing inputs. In this study, sensitivity-maximizing actuator commands of a submersible, which are sequences of bang-bang type commands, were obtained using Genetic Algorithm (GA) optimization technique. By comparing the total sensitivity values, deduced actuator inputs were found to be superior to the other sea trials. Based on the sensitivity distribution of conventional sea trials and sensitivity distribution results through deduced input scenario a review of submersibles' manoeuvring equations of motion was conducted .

Non-Robust and Robust Regularized Zero-Forcing Interference Alignment Methods for Two-Cell MIMO Interfering Broadcast (두 셀 다중 안테나 하향링크 간섭 채널에서 비강인한/강인한 정칙화된 제로포싱 간섭 정렬 방법)

  • Shin, Joonwoo
    • The Journal of Korean Institute of Communications and Information Sciences
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    • v.38A no.7
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    • pp.560-570
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    • 2013
  • In this paper, we propose transceiver design strategies for the two-cell multiple-input multiple-output (MIMO) interfering broadcast channel where inter-cell interference (ICI) exists in addition to inter-user interference (IUI). We first formulate the generalized zero-forcing interference alignment (ZF-IA) method based on the alignment of IUI and ICI in multi-dimensional subspace. We then devise a minimum weighted-mean-square-error (WMSE) method based on "regularizing" the precoders and decoders of the generalized ZF-IA scheme. In contrast to the existing weighted-sum-rate-maximizing transceiver, our method does not require an iterative calculation of the optimal weights. Because of this, the proposed scheme, while not designed specially to maximize the sum-rate, is computationally efficient and achieves a faster convergence compared to the known weighed-sum-rate maximizing scheme. Through analysis and simulation, we show the effectiveness of the proposed regularized ZF-IA scheme.

Optimal Conditions for Maximizing Altitude of Sounding Rocket (사운딩로켓의 고도 극대화를 위한 최적조건)

  • Lee, Sang-Hyeon
    • Journal of the Korean Society of Propulsion Engineers
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    • v.16 no.3
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    • pp.41-48
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    • 2012
  • A study to determine the optimal jet conditions for maximizing altitude of the sounding rocket is conducted. The behavior of a simplified one-dimensional momentum equation including aerodynamic drag is investigated. The case where an analytic solution exists and the case where the mass flow rate is constant are calculated. The solutions are compared with numerical solutions. It is shown that there are the optimal jet conditions for maximizing altitude of a sounding rocket and the optimal condition is a function of the rocket mass ratio.

Characteristic Equation to Determine Optimal Ejection Conditions of Sounding Rocket: Analytic Solution Cases (사운딩로켓의 최적 분사조건 결정을 위한 특성방정식: 해석적 해의 경우)

  • Lee, Sang-Hyeon
    • Journal of the Korean Society of Propulsion Engineers
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    • v.17 no.1
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    • pp.26-34
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    • 2013
  • An analytic approach to determine the optimal conditions for maximizing altitude of a sounding rocket is suggested. The behavior of the one-dimensional momentum equation including thrust, gravitational force and aerodynamic drag force is investigated. For the case where an analytic solution exists, a characteristic equation for determining optimal condition for maximizing altitude at the burn-out state and that for maximizing altitude at the stationary state are developed and verified with numerical experiments.

Performance Evaluation of Bluetooth Radio Link with ARQ Protocol (ARQ를 고려한 블루투스 무선 링크의 성능 분석)

  • Park, Hong-Seong;Jung, Myoung-Soon
    • Journal of Industrial Technology
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    • v.21 no.A
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    • pp.59-64
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    • 2001
  • This paper analyzes the performance of the several types of ACL(Asynchronous ConnectionLess) packets used in Bluetooth according to a BER(Bit Error Rate) and a packet length and proposes an optimal packet type and an optimal size of the packet being able to be used under the given BER. This paper proposes how to obtain the optimal packet type and the optimal size of the packet maximizing the performance measure under the given BER. In addition, this paper shows that the optimal type and size of the packet maximizing the throughput are different from those maximizing the mean transmission time. This occurs because the Bluetooth uses not only one type of packet but also various types of packets.

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Optimum Design of Transverse Flux Linear Motor for Maximizing Thrust Force Using Table of Orthogonal Array (직교배열표를 이용한 추력을 최대화하기 위한 횡자속 선형전동기의 최적설계)

  • Hong, Do Kwan;Woo, Byung Chul;Kang, Do Hvun
    • The Transactions of the Korean Institute of Electrical Engineers B
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    • v.54 no.11
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    • pp.505-510
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    • 2005
  • On this study, we optimized maximizing the thrust force at the TFLM(Transverse Flux Linear Motor) using design of experiments by the table of orthogonal array and the analysis of means(ANOM), and classified the most contributive design factor maximizing the thrust force at the TFLM by analysis of variance(ANOVA). From now on, we are going to apply the required technique to design various uses and shapes of the TFLM.