• 제목/요약/키워드: random procedure

검색결과 493건 처리시간 0.024초

위성 무선 인터페이스를 위한 임의접속 절차 (The Random Access Procedure for Satellite Radio Interface)

  • 남승현;김희욱;홍태철;강군석;구본준;안도섭
    • 한국위성정보통신학회논문지
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    • 제5권2호
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    • pp.14-18
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    • 2010
  • 미래의 통신망은 지상 네트워크과 위성 네트워크가 결합하거나 협동 통신 하는 방향으로 진화할 것으로 예상된다. 위성/지상 통합 시스템에서 위성과 지상 무선 인터페이스 간 공통성은 단말의 비용을 고려했을 때 매우 중요하게 고려되어야 한다. 특히, 차세대 IMT-Advanced 시스템으로 LTE기반의 지상 시스템이 고려되고 있는 점을 감안했을 때, LTE 기반의 위성 시스템에 대한 연구가 절실히 요구된다. 현존하는 LTE기반의 지상 무선 통신 시스템의 프레임은 최대 100 km 크기의 셀에서 임의 접속이 가능하도록 설계되어 있다. 그러나 위성 시스템의 경우 수 천 km에 이르는 빔 커버리지를 갖기 때문에 최대 100 km의 셀 크기를 고려하여 설계된 LTE프레임 구조 내에서 지상 시스템을 위한 임의 접속 방법을 그대로 적용할 수 없다. 따라서, 본 논문에서는 LTE기반 지상 시스템에서 지원하는 프레임 구조에서 시스템 latency를 줄이고 낮은 복잡도를 가지는 위성 시스템 환경에 적절한 임의 접속 절차를 제안하고자 한다.

The random structural response due to a turbulent boundary layer excitation

  • De Rosa, S.;Franco, F.;Romano, G.;Scaramuzzino, F.
    • Wind and Structures
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    • 제6권6호
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    • pp.437-450
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    • 2003
  • In this paper, the structural random response due to the turbulent boundary layer excitation is investigated. Using the mode shapes and natural frequencies of an undamped structural operator, a fully analytical model has been assembled. The auto and cross-spectral densities of kinematic quantities are so determined through exact analytical expansions. In order to reduce the computational costs associated with the needed number of modes, it has been tested an innovative methodology based on a scaling procedure. In fact, by using a reduced spatial domain and defining accordingly an augmented artificial damping, it is possible to get the same energy response with reduced computational costs. The item to be checked was the power spectral density of the displacement response for a flexural simply supported beam; the very simple structure was selected just to highlight the main characteristics of the technique. In principle, it can be applied successfully to any quantity derived from the modal operators. The criterion and the rule of scaling the domain are also presented, investigated and discussed. The obtained results are encouraging and they allow thinking successfully to the definition of procedure that could represent a bridge between modal and energy methods.

Cumulative Sums of Residuals in GLMM and Its Implementation

  • Choi, DoYeon;Jeong, KwangMo
    • Communications for Statistical Applications and Methods
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    • 제21권5호
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    • pp.423-433
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    • 2014
  • Test statistics using cumulative sums of residuals have been widely used in various regression models including generalized linear models(GLM). Recently, Pan and Lin (2005) extended this testing procedure to the generalized linear mixed models(GLMM) having random effects, in which we encounter difficulties in computing the marginal likelihood that is expressed as an integral of random effects distribution. The Gaussian quadrature algorithm is commonly used to approximate the marginal likelihood. Many commercial statistical packages provide an option to apply this type of goodness-of-fit test in GLMs but available programs are very rare for GLMMs. We suggest a computational algorithm to implement the testing procedure in GLMMs by a freely accessible R package, and also illustrate through practical examples.

Direct implementation of stochastic linearization for SDOF systems with general hysteresis

  • Dobson, S.;Noori, M.;Hou, Z.;Dimentberg, M.
    • Structural Engineering and Mechanics
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    • 제6권5호
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    • pp.473-484
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    • 1998
  • The first and second moments of response variables for SDOF systems with hysteretic nonlinearity are obtained by a direct linearization procedure. This adaptation in the implementation of well-known statistical linearization methods, provides concise, model-independent linearization coefficients that are well-suited for numerical solution. The method may be applied to systems which incorporate any hysteresis model governed by a differential constitutive equation, and may be used for zero or non-zero mean random vibration. The implementation eliminates the effort of analytically deriving specific linearization coefficients for new hysteresis models. In doing so, the procedure of stochastic analysis is made independent from the task of physical modeling of hysteretic systems. In this study, systems with three different hysteresis models are analyzed under various zero and non-zero mean Gaussian White noise inputs. Results are shown to be in agreement with previous linearization studies and Monte Carlo Simulation.

Efficient weight initialization method in multi-layer perceptrons

  • Han, Jaemin;Sung, Shijoong;Hyun, Changho
    • 한국경영과학회:학술대회논문집
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    • 한국경영과학회 1995년도 추계학술대회발표논문집; 서울대학교, 서울; 30 Sep. 1995
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    • pp.325-333
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    • 1995
  • Back-propagation is the most widely used algorithm for supervised learning in multi-layer feed-forward networks. However, back-propagation is very slow in convergence. In this paper, a new weight initialization method, called rough map initialization, in multi-layer perceptrons is proposed. To overcome the long convergence time, possibly due to the random initialization of the weights of the existing multi-layer perceptrons, the rough map initialization method initialize weights by utilizing relationship of input-output features with singular value decomposition technique. The results of this initialization procedure are compared to random initialization procedure in encoder problems and xor problems.

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관성측정장치의 오차계수 식별기법 및 실험 (IMU calibration technique and laboratory test)

  • 성상만;이달호;이장규
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 1996년도 한국자동제어학술회의논문집(국내학술편); 포항공과대학교, 포항; 24-26 Oct. 1996
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    • pp.664-667
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    • 1996
  • This paper presents the error parameter estimation technique for IMU(Inertial Measurement Unit) which is core sensor of INS(Inertial Navigation System) and verifies it via laboratory test. Firstly the error characteristic of gyroscope and accelerometer which is contained in IMU is examined and the error modelling is executed. The error of IMU can be divided into deterministic and random part, and the deterministic error can be divided into static and dynamic part. This paper consider the random part as constant. Secondly the error parameter estimation technique and following procedure for laboratory test is explained. Thirdly according to the test procedure the IMU test for static error is executed using 2-axis rate table and estimation result is presented with discussion about its validity.

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항공기 지상 진동 시험 및 동특성 모델의 개선 (The Ground Vibration Test on an Aircraft and FE Model Update)

  • 유홍주;변관화;박금룡
    • 소음진동
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    • 제8권4호
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    • pp.690-699
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    • 1998
  • This paper discusses the techniques, procedures and the results of the ground vibration test(GVT) performed on the development aircraft and the simple procedure of FE model updating technique from the GVT results. The GVT was carried out using random excitation technique with MIMO(Multi-Input-Multi-Output) data acquistion method, and taking full advantage of poly-reference global parameter estimation technique to identify the vibration modes. In dynamic FE modeling, the aircraft was represented by beam elements and all dynamic analysis was performed using MSC/NASTRAN for this model. In updating procedure, the stiffness of the beam model was adjusted iteratively so as to get the natural frequencies and mode shapes close to the GVT results.

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계획기간의 연동적 고려 경우의 추계적 생산계획 (A Stochastic Production Planning Problem in Rolling Horizon Environment)

  • Sung, C. S.;Lee, Y. J.
    • 한국경영과학회지
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    • 제14권2호
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    • pp.67-74
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    • 1989
  • This paper considers single-product production and inventory management problem where cumulative demands up to each time period are mutually independent random variables(known) having continuous probability distributions and the associated cost-minimizing production schedule (when to produce and how much to produce) need be determined in rolling horizon environment. For the problem, both the production cost and the inventory holding and backlogging costs are included in the whole system cost. The probability distributions of these costs are expressed in terms of random demands, and utilized to exploit a solution procedure for a production schedule which minimizes the expected unit time system cost and also reduces the probability of rist that, for the first-period of each production cycle (rolling horizon), the cost of the "production" option will exceed that of the "non-production" one. Numerical examples are presented for the solution procedure illustration.cedure illustration.

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The influence of production inconsistencies on the functional failure of GRP pipes

  • Rafiee, Roham;Fakoor, Mahdi;Hesamsadat, Hadi
    • Steel and Composite Structures
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    • 제19권6호
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    • pp.1369-1379
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    • 2015
  • In this study, a progressive damage modeling is developed to predict functional failure pressure of GRP pipes subjected to internal hydrostatic pressure. The modeling procedure predicts both first-ply failure pressure and functional failure pressure associated with the weepage phenomenon. The modeling procedure is validated using experimental observations. The random parameters attributed to the filament winding production process are identified. Consequently, stochastic simulation is conducted to investigate the influence of induced inconsistencies on the functional failure pressures of GRP pipes. The obtained results are compared to realize the degree to which random parameters affect the performance of the pipe in operation.

Optimal input cross-power spectra in shake table testing of asymmetric structures

  • Ammanagi, S.;Manohar, C.S.
    • Earthquakes and Structures
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    • 제9권5호
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    • pp.1115-1132
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    • 2015
  • The study considers earthquake shake table testing of bending-torsion coupled structures under multi-component stationary random earthquake excitations. An experimental procedure to arrive at the optimal excitation cross-power spectral density (psd) functions which maximize/minimize the steady state variance of a chosen response variable is proposed. These optimal functions are shown to be derivable in terms of a set of system frequency response functions which could be measured experimentally without necessitating an idealized mathematical model to be postulated for the structure under study. The relationship between these optimized cross-psd functions to the most favourable/least favourable angle of incidence of seismic waves on the structure is noted. The optimal functions are also shown to be system dependent, mathematically the sharpest, and correspond to neither fully correlated motions nor independent motions. The proposed experimental procedure is demonstrated through shake table studies on two laboratory scale building frame models.