871 resultados para ERROR-CORRECTION
Resumo:
In most diffusion tensor imaging (DTI) studies, images are acquired with either a partial-Fourier or a parallel partial-Fourier echo-planar imaging (EPI) sequence, in order to shorten the echo time and increase the signal-to-noise ratio (SNR). However, eddy currents induced by the diffusion-sensitizing gradients can often lead to a shift of the echo in k-space, resulting in three distinct types of artifacts in partial-Fourier DTI. Here, we present an improved DTI acquisition and reconstruction scheme, capable of generating high-quality and high-SNR DTI data without eddy current-induced artifacts. This new scheme consists of three components, respectively, addressing the three distinct types of artifacts. First, a k-space energy-anchored DTI sequence is designed to recover eddy current-induced signal loss (i.e., Type 1 artifact). Second, a multischeme partial-Fourier reconstruction is used to eliminate artificial signal elevation (i.e., Type 2 artifact) associated with the conventional partial-Fourier reconstruction. Third, a signal intensity correction is applied to remove artificial signal modulations due to eddy current-induced erroneous T2(∗) -weighting (i.e., Type 3 artifact). These systematic improvements will greatly increase the consistency and accuracy of DTI measurements, expanding the utility of DTI in translational applications where quantitative robustness is much needed.
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An analysis is carried out, using the prolate spheroidal wave functions, of certain regularized iterative and noniterative methods previously proposed for the achievement of object restoration (or, equivalently, spectral extrapolation) from noisy image data. The ill-posedness inherent in the problem is treated by means of a regularization parameter, and the analysis shows explicitly how the deleterious effects of the noise are then contained. The error in the object estimate is also assessed, and it is shown that the optimal choice for the regularization parameter depends on the signal-to-noise ratio. Numerical examples are used to demonstrate the performance of both unregularized and regularized procedures and also to show how, in the unregularized case, artefacts can be generated from pure noise. Finally, the relative error in the estimate is calculated as a function of the degree of superresolution demanded for reconstruction problems characterized by low space–bandwidth products.
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Clinical Trial
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p.159-160
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Pensar que existen soluciones para cerrar la brecha entre el colegio y la universidad es utópico. Sin embargo, sí tiene sentido el trabajo que se haga con respecto al problema de la brecha para conocer y acercar los ideales y las expectativas que tienen las diferentes instituciones de educación. En la Universidad de los Andes fue evidente que dicho trabajo se podría orientar en diferentes direcciones y haciendo énfasis en la institución o bien en los profesores o bien en los estudiantes. Se podían abordar temas como: diseño curricular, creencias y actitudes de los profesores y de los estudiantes, métodos de enseñanza, concepciones sobre la enseñanza y el aprendizaje, dificultades y errores de aprendizaje y otros temas. Luego de varios traspiés en la elección del tema de investigación, elegimos finalmente explorar el tema del aprendizaje y considerar a los primíparos para el estudio por ser ellos los que viven realmente el proceso de transición del colegio a la universidad. Por otra parte, nos restringimos al área de precálculo motivados en parte porque en esta materia había un mayor índice de desaprobación. Concretamente, se propuso como objetivo general describir un perfil de aprendizaje en matemáticas del estudiante de Precálculo en el momento de ingresar a la Universidad. Del objetivo anterior se derivó el problema principal de este proyecto: definir los elementos conceptuales con los cuáles articular la descripción de dicho perfil. La presentación está dividida en cuatro partes, en la primera se expone un marco conceptual que presenta los elementos con los cuales se describirá el perfil, la segunda y tercera se refieren respectivamente a la metodología de la investigación y a los resultados obtenidos y la última a las conclusiones del trabajo.
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La investigación tiene dos fases: 1) Se plantea a los estudiantes de primer ingreso a la Universidad Panamericana, Guadalajara, México la simplificación de la expresión algebraica ; analizándose las respuestas equivocadas con su posible origen. 2) Se hace un estudio con 7 profesores de educación media básica y media superior, en el cual, se les presenta la simplificación errónea (a la izq.) con la consigna de mencionar el origen del error y cómo le ayudarían al alumno. Alumnos cometen errores de muy diverso origen, y los profesores encuestados no siempre analizan a profundidad el origen del error cometido por este alumno.
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The PHYSICA software was developed to enable multiphysics modelling allowing for interaction between Computational Fluid Dynamics (CFD) and Computational Solid Mechanics (CSM) and Computational Aeroacoustics (CAA). PHYSICA uses the finite volume method with 3-D unstructured meshes to enable the modelling of complex geometries. Many engineering applications involve significant computational time which needs to be reduced by means of a faster solution method or parallel and high performance algorithms. It is well known that multigrid methods serve as a fast iterative scheme for linear and nonlinear diffusion problems. This papers attempts to address two major issues of this iterative solver, including parallelisation of multigrid methods and their applications to time dependent multiscale problems.
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The concept of a “true” ground-truth map is introduced, from which the inaccuracy/error of any production map may be measured. A partition of the mapped region is defined in terms of the “residual rectification” transformation. Geometric RMS-type and Geometric Distortion error criteria are defined as well as a map mis-classification error criterion (the latter for hard and fuzzy produc-tion maps). The total map error is defined to be the sum (over each set of the map partition men-tioned above) of these three error components integrated over each set of the partition.
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Sound waves are propagating pressure fluctuations and are typically several orders of magnitude smaller than the pressure variations in the flow field that account for flow acceleration. On the other hand, these fluctuations travel at the speed of sound in the medium, not as a transported fluid quantity. Due to the above two properties, the Reynolds averaged Navier-Stokes (RANS) equations do not resolve the acoustic fluctuations. Direct numerical simulation of turbulent flow is still a prohibitively expensive tool to perform noise analysis. This paper proposes the acousticcorrectionmethod, an alternative and affordable tool based on a modified defect correction concept, which leads to an efficient algorithm for computational aeroacoustics and noise analysis.
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An aerodynamic sound source extraction from a general flow field is applied to a number of model problems and to a problem of engineering interest. The extraction technique is based on a variable decomposition, which results to an acoustic correction method, of each of the flow variables into a dominant flow component and a perturbation component. The dominant flow component is obtained with a general-purpose Computational Fluid Dynamics (CFD) code which uses a cell-centred finite volume method to solve the Reynolds-averaged Navier–Stokes equations. The perturbations are calculated from a set of acoustic perturbation equations with source terms extracted from unsteady CFD solutions at each time step via the use of a staggered dispersion-relation-preserving (DRP) finite-difference scheme. Numerical experiments include (1) propagation of a 1-D acoustic pulse without mean flow, (2) propagation of a 2-D acoustic pulse with/without mean flow, (3) reflection of an acoustic pulse from a flat plate with mean flow, and (4) flow-induced noise generated by the an unsteady laminar flow past a 2-D cavity. The computational results demonstrate the accuracy for model problems and illustrate the feasibility for more complex aeroacoustic problems of the source extraction technique.