• 제목/요약/키워드: power-space functions

검색결과 140건 처리시간 0.031초

국제민간항공기구의 이론적 고찰 (A Theoretical Analysis of International Civil Aviation Organization)

  • 김관옥
    • 항공우주정책ㆍ법학회지
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    • 제14권
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    • pp.151-174
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    • 2001
  • Theories of international organization have explained the creation, maintenance, and decline of international organization. However, their explanations on changes of international organization have been much more different one another. For example, the theory of hegemonic stability argues that international organization can be created and maintained only by a hegemonic state and will be declined if the hegemonic state decline. On the other hand, the functional approach believes that the positive functions and effects that international organization provides motivate states to create and maintain the organization, while the game-theoretical approach explains international organization based on cost-benefit calculation of rational states. Thus, the empirical evaluation of the arguments of the theories of international organization and defining the major factors that determine international organization are necessary not only for the development of theories of international organization but also for making desirable policies toward international organization. For the purpose, this paper compares and contrasts the three major theories of international organization and applies the approaches to the case of the International Civil Aviation Organization (ICAO) to test their arguments. Since the ICAO has been rarely examined by the theories of international organization, the case study could be desirable case to evaluate theories of international organization. In this sense, this paper attempts to define the major factors that determine the creation, maintenance, and decline of the ICAO. In particular, since the Korean government has changed its policy for air transport security system recently, it will investigate the role of ICAO on the policy change to define the limits and strength of ICAO. In conclusion, this paper will assess the relative explanatory power of each approach based on the analysis of the creation and changes of ICAO

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The Development of Modularized Post Processing GPS Software Receiving Platform using MATLAB Simulink

  • Kim, Ghang-Ho;So, Hyoung-Min;Jeon, Sang-Hoon;Kee, Chang-Don;Cho, Young-Su;Choi, Wansik
    • International Journal of Aeronautical and Space Sciences
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    • 제9권2호
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    • pp.121-128
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    • 2008
  • Modularized GPS software defined radio (SDR) has many advantages of applying and modifying algorithm. Hardware based GPS receiver uses many hardware parts (such as RF front, correlators, CPU and other peripherals) that process tracked signal and navigation data to calculate user position, while SDR uses software modules, which run on general purpose CPU platform or embedded DSP. SDR does not have to change hardware part and is not limited by hardware capability when new processing algorithm is applied. The weakness of SDR is that software correlation takes lots of processing time. However, in these days the evolution of processing power of MPU and DSP leads the competitiveness of SDR against the hardware GPS receiver. This paper shows a study of modulization of GPS software platform and it presents development of the GNSS software platform using MATLAB Simulink™. We focus on post processing SDR platform which is usually adapted in research area. The main functions of SDR are GPS signal acquisition, signal tracking, decoding navigation data and calculating stand alone user position from stored data that was down converted and sampled intermediate frequency (IF) data. Each module of SDR platform is categorized by function for applicability for applying for other frequency and GPS signal easily. The developed software platform is tested using stored data which is down-converted and sampled IF data file. The test results present that the software platform calculates user position properly.

통신위성 배터리 충,방전기 설계 및 해석 (Design and Analysis of a Battery Charge and Discharge Regulator of Communication Satellite)

  • 최재동
    • 한국항공우주학회지
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    • 제31권7호
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    • pp.118-126
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    • 2003
  • 본 연구에서는 모듈형태의 배터리 충-방전기가 정상상태뿐만 아니라 과도상태에서 예기치 못한 결함이 발생할지라도 실패 없이 전원을 공급하는 것이 가능한 병렬형 양방향 컨버터로 설계되어졌다. 컨버터 모듈은 안정성, 성능 및 고신뢰성을 얻기 위해 독립적인 제어가 가능하도록 설계되었으며, 제어기를 위해 사용된 평균전류모드방식은 노이즈 면역, 빠른 응답 및 평균전류 신호 획득과 같은 장점을 갖는다. 병렬 연결된 배터리 충-방전기에 대한 등가모델이 제시되었으며, 충전연속모드, 방전연속/불연속 모드에 대한 전달함수가 분석되었다. 병렬 양방향 컨버터는 스텝 부하변화와 하나의 컨버터 모듈 실패에 대해 각각 수행되었다. 그리고 병렬 양방향 컨버터의 성능이 실험결과들을 통해 검증되었다.

Memory Organization for a Fuzzy Controller.

  • Jee, K.D.S.;Poluzzi, R.;Russo, B.
    • 한국지능시스템학회:학술대회논문집
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    • 한국퍼지및지능시스템학회 1993년도 Fifth International Fuzzy Systems Association World Congress 93
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    • pp.1041-1043
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    • 1993
  • Fuzzy logic based Control Theory has gained much interest in the industrial world, thanks to its ability to formalize and solve in a very natural way many problems that are very difficult to quantify at an analytical level. This paper shows a solution for treating membership function inside hardware circuits. The proposed hardware structure optimizes the memoried size by using particular form of the vectorial representation. The process of memorizing fuzzy sets, i.e. their membership function, has always been one of the more problematic issues for the hardware implementation, due to the quite large memory space that is needed. To simplify such an implementation, it is commonly [1,2,8,9,10,11] used to limit the membership functions either to those having triangular or trapezoidal shape, or pre-definite shape. These kinds of functions are able to cover a large spectrum of applications with a limited usage of memory, since they can be memorized by specifying very few parameters ( ight, base, critical points, etc.). This however results in a loss of computational power due to computation on the medium points. A solution to this problem is obtained by discretizing the universe of discourse U, i.e. by fixing a finite number of points and memorizing the value of the membership functions on such points [3,10,14,15]. Such a solution provides a satisfying computational speed, a very high precision of definitions and gives the users the opportunity to choose membership functions of any shape. However, a significant memory waste can as well be registered. It is indeed possible that for each of the given fuzzy sets many elements of the universe of discourse have a membership value equal to zero. It has also been noticed that almost in all cases common points among fuzzy sets, i.e. points with non null membership values are very few. More specifically, in many applications, for each element u of U, there exists at most three fuzzy sets for which the membership value is ot null [3,5,6,7,12,13]. Our proposal is based on such hypotheses. Moreover, we use a technique that even though it does not restrict the shapes of membership functions, it reduces strongly the computational time for the membership values and optimizes the function memorization. In figure 1 it is represented a term set whose characteristics are common for fuzzy controllers and to which we will refer in the following. The above term set has a universe of discourse with 128 elements (so to have a good resolution), 8 fuzzy sets that describe the term set, 32 levels of discretization for the membership values. Clearly, the number of bits necessary for the given specifications are 5 for 32 truth levels, 3 for 8 membership functions and 7 for 128 levels of resolution. The memory depth is given by the dimension of the universe of the discourse (128 in our case) and it will be represented by the memory rows. The length of a world of memory is defined by: Length = nem (dm(m)+dm(fm) Where: fm is the maximum number of non null values in every element of the universe of the discourse, dm(m) is the dimension of the values of the membership function m, dm(fm) is the dimension of the word to represent the index of the highest membership function. In our case then Length=24. The memory dimension is therefore 128*24 bits. If we had chosen to memorize all values of the membership functions we would have needed to memorize on each memory row the membership value of each element. Fuzzy sets word dimension is 8*5 bits. Therefore, the dimension of the memory would have been 128*40 bits. Coherently with our hypothesis, in fig. 1 each element of universe of the discourse has a non null membership value on at most three fuzzy sets. Focusing on the elements 32,64,96 of the universe of discourse, they will be memorized as follows: The computation of the rule weights is done by comparing those bits that represent the index of the membership function, with the word of the program memor . The output bus of the Program Memory (μCOD), is given as input a comparator (Combinatory Net). If the index is equal to the bus value then one of the non null weight derives from the rule and it is produced as output, otherwise the output is zero (fig. 2). It is clear, that the memory dimension of the antecedent is in this way reduced since only non null values are memorized. Moreover, the time performance of the system is equivalent to the performance of a system using vectorial memorization of all weights. The dimensioning of the word is influenced by some parameters of the input variable. The most important parameter is the maximum number membership functions (nfm) having a non null value in each element of the universe of discourse. From our study in the field of fuzzy system, we see that typically nfm 3 and there are at most 16 membership function. At any rate, such a value can be increased up to the physical dimensional limit of the antecedent memory. A less important role n the optimization process of the word dimension is played by the number of membership functions defined for each linguistic term. The table below shows the request word dimension as a function of such parameters and compares our proposed method with the method of vectorial memorization[10]. Summing up, the characteristics of our method are: Users are not restricted to membership functions with specific shapes. The number of the fuzzy sets and the resolution of the vertical axis have a very small influence in increasing memory space. Weight computations are done by combinatorial network and therefore the time performance of the system is equivalent to the one of the vectorial method. The number of non null membership values on any element of the universe of discourse is limited. Such a constraint is usually non very restrictive since many controllers obtain a good precision with only three non null weights. The method here briefly described has been adopted by our group in the design of an optimized version of the coprocessor described in [10].

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3자유도 차량모델을 이용한 차선추종 µ 제어기 설계 (The Controller Design for Lane Following with 3-Degree of Freedom Vehicle Dynamics)

  • 지상원;임태우;유삼상;김환성
    • 동력기계공학회지
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    • 제17권3호
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    • pp.72-81
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    • 2013
  • Many articles have been published about a 2-degree of freedom model that includes the lateral and yaw motions for controller synthesis in intelligent transport system applications. In this paper, a 3-degree of freedom linear model that includes the roll motion is developed to design a robust steering controller for lane following maneuvers using ${\mu}$-synthesis. This linear perturbed system includes a set of parametric uncertainties in cornering stiffness and unmodelled dynamics in steering actuators. The state-space model with parametric uncertainties is represented in linear fractional transformation form. Design purpose can be obtained by properly choosing the frequency dependent weighting functions. The objective of this study is to keep the tracking error and steering input energy small in the presence of variations of the cornering stiffness coefficients. Furthermore, good ride quality has to be achieved against these uncertainties. Frequency-domain analyses and time-domain numerical simulations are carried out in order to evaluate these performance specifications of a given vehicle system. Finally, the simulation results indicate that the proposed robust controller achieves good performance over a wide range of uncertainty for the given maneuvers.

A Hierarchical Model Predictive Voltage Control for NPC/H-Bridge Converters with a Reduced Computational Burden

  • Gong, Zheng;Dai, Peng;Wu, Xiaojie;Deng, Fujin;Liu, Dong;Chen, Zhe
    • Journal of Power Electronics
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    • 제17권1호
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    • pp.136-148
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    • 2017
  • In recent years, voltage source multilevel converters are very popular in medium/high-voltage industrial applications, among which the NPC/H-Bridge converter is a popular solution to the medium/high-voltage drive systems. The conventional finite control set model predictive control (FCS-MPC) strategy is not practical for multilevel converters due to their substantial calculation requirements, especially under high number of voltage levels. To solve this problem, a hierarchical model predictive voltage control (HMPVC) strategy with referring to the implementation of g-h coordinate space vector modulation (SVM) is proposed. By the hierarchical structure of different cost functions, load currents can be controlled well and common mode voltage can be maintained at low values. The proposed strategy could be easily expanded to the systems with high number of voltage levels while the amount of required calculation is significantly reduced and the advantages of the conventional FCS-MPC strategy are reserved. In addition, a HMPVC-based field oriented control scheme is applied to a drive system with the NPC/H-Bridge converter. Both steady-state and transient performances are evaluated by simulations and experiments with a down-scaled NPC/H-Bridge converter prototype under various conditions, which validate the proposed HMPVC strategy.

Thrust Performance and Plasma Acceleration Process of Hall Thrusters

  • Tahara, Hirokazu
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2004년도 제22회 춘계학술대회논문집
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    • pp.262-270
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    • 2004
  • Basic experiments were carried out using the THT-IV low-power Hall thruster to examine the influences of magnetic field shape and strength, and acceleration channel length on thruster performance and to establish guidelines for design of high-performance Hall thrusters. Thrusts were measured with varying magnetic field and channel structure. Exhaust plasma diagnostic measurement was also made to evaluate plume divergent angles and voltage utilization efficiencies. Ion current spatial profiles were measured with a Faraday cup, and ion energy distribution functions were estimated from data with a retarding potential analyzer. The thruster was stably operated with a highest performance under an optimum acceleration channel length of 20 mm and an optimum magnetic field with a maximum strength of about 150 Gauss near the channel exit and with some shape considering ion acceleration directions. Accordingly, an optimum magnetic field and channel structure is considered to exist under an operational condition, related to inner physical phenomena of plasma production, ion acceleration and exhaust plasma feature. A new Hall thruster was designed with basic research data of the THT-IV thruster. With the thruster with many considerations, long stable operations were achieved. In all experiments at 200-400 V with 1.5-3 mg/s, the thrust and the specific impulse ranged from 15 to 70 mN and from 1100 to 2300 see, respectively, in a low electric power range of 300~1300 W. The thrust efficiency reached 55 %. Hence, a large map of the thruster performance was successfully made. The thermal characteristics were also examined with data of both measured and calculated temperatures in the thruster body. Thermally safe conditions were achieved with all input powers.

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DEVELOPMENT AND EVALUATION OF A TEMPORARY PLACEMENT AND CONVEYANCE OPERATION SIMULATION SYSTEM USING AUGMENTED REALITY

  • Yan, Weida;Aoyama, Shuhei;Ishii, Hirotake;Shimoda, Hiroshi;Sang, Tran T.;Inge, Solhaug Lars;Lygren, Toppe Aleksander;Terje, Johnsen;Izumi, Masanori
    • Nuclear Engineering and Technology
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    • 제44권5호
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    • pp.507-522
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    • 2012
  • When decommissioning a nuclear power plant, it is difficult to make an appropriate plan to ensure sufficient space for temporary placement and conveyance operations of dismantling targets. This paper describes a system to support temporary placement and conveyance operations using augmented reality (AR). The system employs a laser range scanner to measure the three-dimensional (3D) information of the environment and a dismantling target to produce 3D surface polygon models. Then, the operator simulates temporary placement and conveyance operations using the system by manipulating the obtained 3D model of the dismantling target in the work field. Referring to the obtained 3D model of the environment, a possible collision between the dismantling target and the environment is detectable. Using AR, the collision position is presented intuitively. After field workers evaluated this system, the authors concluded that the system is feasible and acceptable to verify whether spaces for passage and temporary storage are sufficient for temporary placement and conveyance operations. For practical use in the future, some new functions must be added to improve the system. For example, it must be possible for multiple workers to use the system simultaneously by sharing the view of dismantling work.

장소와 공간의 재현적 관점에서 본 드론 쇼트와 핸드헬드 쇼트의 영상 미학 : <세계테마기행> '유카탄 반도'편을 중심으로 (The Visual Aesthetics of Drone Shot and Hand-held Shot based on the Representation of Place and Space : focusing on World Travel' Peninsula de Yucatán' Episode)

  • 류재형
    • 한국엔터테인먼트산업학회논문지
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    • 제14권3호
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    • pp.251-265
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    • 2020
  • 이 연구는 드론 쇼트(Drone Shot)와 핸드헬드 쇼트(Hand-held Shot)라는 두 촬영기법의 미학적 기능을 비교, 분석하는 데에 그 목적이 있다. 연구를 위해 세르토(Certeau)의 장소와 공간의 개념을 이해하였다. 두 촬영기법의 미학적 기능을 비교, 분석할 텍스트로서 <세계테마기행> '유카탄 반도'편을 선정하고 그들의 미학적 특성이 잘 드러나는 장면들을 중심으로 장소와 공간의 개념을 적용, 분석하였다. 분석 결과, 드론 쇼트는 자기반영성이 제거된 고요한 움직임으로 도시를 내려다보면서 지역의 전반적인 분위기와 정보를 제공하는 권위적인 시점을 취하였으며, 이러한 기능은 그 지역의 고유한 규칙 및 질서 등에 대한 선지식을 전달하는 내레이션이나 자막 등을 통해 강화되었다. 반대로 핸드헬드 쇼트는 도시에 내재된 규칙과 질서 등에 얽매이지 않고 자유보행을 통해 공간을 실천적으로 경험하였다. 관람 코스로 굳어진 주요 명소보다 소도시와 시골의 일상에 관심을 기울이면서 인간적인 보행을 실천한다는 점에서 권력 주체의 전략에 저항하는 전술을 담아내었다.

구면 스레피안 함수로 표현된 지각 자기이상값과 구배 성분 (Spherical Slepian Harmonic Expression of the Crustal Magnetic Vector and Its Gradient Components)

  • 김형래
    • 자원환경지질
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    • 제49권4호
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    • pp.269-280
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    • 2016
  • 지역에 최적화된 스레피안 구면함수(spherical Slepian function)를 활용하여 남극을 중심으로 반경 $20^{\circ}$ 범위의 지역에 지각 자기이상의 3개의 방향 성분과 6개의 구배성분들을 표현하였다. 2013년 11월 유럽 항공 우주국이 발사한 3개의 자력 위성인 Swarm은 궤도 전개를 통해 동서 방향의 구배값은 물론 남북 및 수직방향의 구배값을 얻을 수 있도록 계획하였다. 이미 발사된 여러 중력위성들(i.e., GRACE and GOCE) 역시 이러한 구배값을 활용하여 보다 정확한 중력 이상값 및 지표에서의 시간에 따른 중력변화 연구등을 수행해 왔으나 자력 위성자료를 통해서는 많은 연구들이 이루어지고 있지 않는 상태이다. 한편 지역화 모델링은 관심 지역 또는 자료 분포의 제한인 지역인 경우에 활용될 수 있다. 또한 전지구 모델보다 효율적인 연산이 가능하여 위성자료로부터 고해상도의 지각 자기이상값을 표현할 수 있다는 장점을 지니고 있다. 또한 기존의 전지구 구면조화함수의 선형 결합으로 이루어진 기저함수들은 서로 직교성(orthogonality)이 유지되므로 스레피안 구면함수의 계수를 전지구 구면조화함수의 계수로 변환이 가능하여 스펙트럼 분석에 활용할 수 있다. 따라서 Swarm 위성자료의 구배 성분을 이용한 지역화 모델링 방법은 앞으로 많은 활용이 기대되며 여기서는 Swarm 위성자료로부터 얻어진 지각 자기이상값의 전지구 조화함수 계수 모델을 사용하여 자기이상의 방향성분과 구배성분을 유도하고 이를 스레피안 구면 조화함수에 적용하여 관심지역인 남극지역의 방향 성분과 구배 성분을 표현하고 이에 대한 결과를 토의 하고자 한다.