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44 results about "Model decomposition" patented technology

The decomposition model assumes that sales are affected by four factors: the general trend in the data, general economic cycles, seasonality, and irregular or random occurrences. The forecast is made by considering each of these components separately and then combining them together.

3dsMax-based nuclear facility model radiation field dosage simulation method

ActiveCN107194103AQuick assignmentRealize radiation field dose calculationDesign optimisation/simulationSpecial data processing applicationsVoxelDecay factor
The invention provides a 3dsMax-based nuclear facility model radiation field dosage simulation method. The method comprises the following steps of: constructing a model by 3dsMax software according to determined nuclear facility parameters, and storing a file in a 3DS format; importing a 3DS nuclear facility model file and obtaining model parameters; decomposing the 3dsMax nuclear facility model into voxels by using an octree method; writing determined voxel parameters and material information into an input card; importing the input card into a point nuclear integration program; calculating an accumulation factor; calculating a mean free path, in a radiation field, of a gamma ray; establishing a flux rate-dosage rate conversion factor, quality decay factors of chemical elements and materials and a single-layer accumulation factor database by utilizing an SQLite database engine; carrying out combined operation on a box by using a Boolean connective operator, and constructing a complicated radiation field geometric structure; and calculating a three-dimensional radiation field dosage by using a point nuclear integration method. The method provided by the invention is capable of realizing radiation field dosage calculation of complicated 3dsMax nuclear facility models with sizes, materials and energy parameters.
Owner:HARBIN ENG UNIV

Method and system for judging position of automobile power window

The invention discloses a method and system for judging the position of an automobile power window. The method comprises the steps that real-time sampling is started for the ripple current of a motor for controlling the window, and after at least two sampling periods are carried out, the continuous first ripple current sampling value, second ripple current sampling value and third ripple current sampling value are acquired in each sampling period; in each sampling period, according to comparison of the first ripple current sampling value, the second ripple current sampling value and the third ripple current sampling value, it is determined that the ripple current in the current sampling period is located on the wave trough or the wave crest or the non-wave-trough portion or the non-wave-crest portion, and the total wave crest number and the total wave trough number of the current sampling period are recorded after real-time sampling is started; and the position of the window is calculated according to the total wave crest number and the total wave trough number. According to the method and system, the features of the ripple current are extracted, the features of the wave crest and the wave trough of the ripple current are subjected to modeling decomposition and extraction, and therefore precise current ripple counting is obtained, and the position of the power window can be calculated accurately.
Owner:SAIC GENERAL MOTORS +1

Region saturation load prediction method based on model family decomposition and integration technology

The invention discloses a region saturation load prediction method based on a model family decomposition and integration technology. In the existing load prediction technology, single prediction methods are used, such as trend extrapolation, grey prediction and linear regression; and the prediction results for each prediction method are different greatly. The region saturation load prediction method includes the steps: extracting the main influence factors for region load growth; selecting a suitable single prediction method or model to predict region saturation load; and finally determining the weight of each single prediction method or model so as to perform combined prediction of the region saturation load scale. The region saturation load prediction method based on a model family decomposition and integration technology integrates with the advantages of each single saturation load prediction method, can perform optimized combination and comprehensive analysis, can comprehensively consider the influence of the indexes which are closely related with power consumption, integrates with the saturation load determination index set to predict the saturation scale and the saturation year of the region electric power consumption quantity, and is conductive to assisting long term of power grid planning in the region.
Owner:STATE GRID ZHEJIANG ELECTRIC POWER COMPANY ECONOMIC TECHN INST +2

EMD (Empirical Mode Decomposition) endpoint effect suppression method based on HMM (Hidden Markov Model) correction and neural network extension

InactiveCN103440226AInhibition of EMD endpoint effectsSolve the problem of estimation errorBiological neural network modelsComplex mathematical operationsDecompositionAlgorithm
The invention discloses an EMD (Empirical Mode Decomposition) endpoint effect suppression method based on HMM (Hidden Markov Model) correction and neural network extension. The method comprises the steps of A) using a sensor to obtain a signal; B) using a neural network extension algorithm to estimate partial known data in a signal endpoint, calculating estimation errors and predicting data outside the endpoint; C) using an HMM algorithm to establish a model for the estimation errors and using the parameters of the model to predict the extension errors of the used extension algorithm; D) using the predicted error data to correct the extended data to obtain final extended data; E) performing empirical model decomposition to the extended signal and abandoning the extended data at two ends to obtain IMF (Intrinsic Mode Function) components of the original signal; and F) extracting signal features by analyzing the IMF components after endpoint effect suppression. The EMD endpoint effect suppression method based on HMM correction and neural network extension has the advantages that the neural network extension algorithm can be corrected, the errors existing in a data extension method are reduced, and the endpoint effect in empirical model decomposition is effectively suppressed.
Owner:YANSHAN UNIV

Multicore parallel solving method for computation of polymer molecular weight distribution

The invention discloses a multicore parallel solving method for the computation of polymer molecular weight distribution, comprising the following steps of: establishing a mechanism model of free radical polymerization dynamic simulation to solve the polymer molecular weight distribution by taking the free radical polymerization dynamic simulation as an object; dividing the mechanism model into a small-scale free radical polymerization model and a large-scale free radical polymerization model through a decoupling method; solving the small-scale free radical polymerization model by utilizing a variable step-size and order backward difference method; and solving the large-scale free radical polymerization model to accelerate the solution of the computation of the polymer molecular weight distribution through a parallel sequential method by taking a multicore computer system as a computing platform. Compared with the traditional non-parallel solving method of the computation of the polymer molecular weight distribution, the invention can increase the solving speed of the mechanism model by sufficiently utilizing the multicore characteristics of the multicore computer system; and in addition, the multicore parallel solving method has simple and clear principle and is convenient to implement on any multicore computer system.
Owner:ZHEJIANG UNIV

Complete polarization synthetic aperture radar target decomposition method for adaptive selection unitary transformation

InactiveCN104698447ASuppressing Scatter Overestimation ProblemsLess freedomRadio wave reradiation/reflectionSynthetic aperture radarOmega
The invention provides a complete polarization synthetic aperture radar target decomposition method for adaptive selection unitary transformation. The method comprises the following steps: (1) performing two unitary transformations for singh for data coherence T matrix of the complete polarization synthetic aperture radar to obtain the matrix, (the formula is as shown in specification); (2) performing other two unitary transformations for the coherence T matrix to obtain the matrix T(omega), wherein the first unitary transformation is used for performing the spiral angle compensation and restraining the volume scattering excessive estimation of model decomposition, the second unitary transformation is used for further restraining the volume scattering excessive estimation and reducing one degree of freedom of the coherence T matrix; (3) comparing with element (the formula is as shown in specification) of the matrix (the formula is as shown in specification) with the element T33(omega) of the matrix T(omega); if (the formula is as shown in specification), and (the formula is as shown in specification), otherwise, T is equal to T(omega); (4) performing three-component model decomposition on coherence T matrix. The two unitary transformations for singh in the step (1) or the two unitary transformations in the step (2) can be selected for the coherence T matrix in a self-adaption mode by the method according to the real situation of the object, and the volume scattering excessive estimation problem of the model decomposition can be effectively restrained.
Owner:NAT SPACE SCI CENT CAS

Electric power system optimal support set positioning method based on anticipated fault decomposition

The invention discloses an electric power system optimal support set positioning method based on anticipated fault decomposition. In order to stabilize the frequency of a power grid, multiple units having decisive effects on safety and reliability of the power grid need to be selected. The method comprises steps of by considering different anticipated faults of the power grid, establishing an electric power system safety restraining optimal power flow mode by taking the minimization of the climbing ability of generator sets as an objective; adopting an anticipated fault decomposition method to decompose the model into a main problem under a normal operation mode and sub problems under each anticipated fault operation mode; through iteration solving of the main problem under the normal operation mode and the sub problem under each anticipated fault operation mode, achieving solving of above electric power system safety restraining optimal power flow mode; and according to the steps, solving the smallest climbing ability transformation quantity of the generator sets, carrying out progressively decreased ranking on the generator sets with the non-zero transformation quantity and successively recording the generator sets to be the optimal support sets with progressively decreased priorities according to the sequences to be output as the results. The method is excellent in applicability and actual requirements are well met.
Owner:HANGZHOU E ENERGY ELECTRIC POWER TECH +2

Time mark separation aircraft elastomer control method based on nonlinear information

The invention discloses a time mark separation aircraft elastomer control method based on nonlinear information, belongs to the field of aircraft control, is especially suitable for a hypersonic-velocity aircraft elastomer, and is used for solving a problem that a conventional elastomer hypersonic-velocity aircraft cannot achieve the rigid-flexible mode separation control. The method comprises thesteps: carrying out the kinetic analysis of a hypersonic-velocity aircraft elastomer kinetic model, and clearly determining the coupling mode of rigid-flexible modes; carrying out the quick-slow timemark decomposition of the model through the singular perturbation theory, and enabling a rigid mode and a flexible mode in the kinetic model to be separated; designing a control strategy based on thelinear information for a slow variable time mark part for representing the rigid mode of the system, and enabling a nonlinear item obtained after model decomposition to be directly substituted into acontroller; designing a sliding-mode control strategy for a quick variable time mark part for representing the flexible mode of the system; finally integrating the two types of control input into onetype of control input as the general rudder deviation, thereby achieving the effective control of the rigid-flexible modes of an aircraft.
Owner:XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA

Polarization SAR model decomposition evaluation method based on electromagnetic scattering simulation

The invention discloses a polarization SAR model decomposition evaluation method based on electromagnetic scattering simulation. The method comprises the steps of (S1) setting surface electromagneticgeometric parameters, aircraft flight parameters and radar satellite position parameters and calculating a surface real beta value of a target scene by using a classical forward model, (S2) processingthe polarization SAR simulation data of the target scene by using a polarization SAR model decomposition method to be evaluated and carrying out inversion to obtain an inversion beta value, and (S3)calculating a mean square root error of the inversion beta value and the surface real beta value, and evaluating the polarization SAR model decomposition method to be evaluated with a principle that the smaller the mean square root error is, the better the effect of the decomposition method is. According to the scheme of the invention, the electromagnetic scattering simulation theory and the polarization SAR model decomposition theory are organically combined, a decomposition algorithm is evaluated from the perspective of electromagnetic wave simulation and model decomposition, the method is fair and just, and a reference can be provided for the selection of an excellent model decomposition method for different application scenes.
Owner:CENT SOUTH UNIV

3D (Three-dimensional) printing-oriented model decomposition and arrangement method

ActiveCN105427374ASolve the problem that it cannot be printed in the printing spaceEfficient arrangementAdditive manufacturing apparatus3D modellingDecompositionAlgorithm
The invention puts forwards a 3D (Three-dimensional) printing-oriented model decomposition and arrangement method. The method comprises the following steps: giving a model S and a printing space PV, calculating the decomposition of the initial pyramid attribute blocks of the model S, carrying out voxelization on the pyramid attribute blocks to generate a first initial intermediate solution isolu0; initializing an intermediate solution set ISolu={isolu0}, and initializing an optimal complete solution P*; for each intermediate solution isolui in the intermediate solution set ISolu, calculating one series of candidate intermediate solutions generated by the intermediate solutions, and solving an optimal decomposition and arrangement solution of the model S; and carrying out local optimization on a three-dimensional grid of a plurality of extracted blocks, causing the blocks to be more tightly arranged through the translation of each block along the negative direction of a Z axis, and therefore, obtaining the optimal decomposition and arrangement about the model S. The model is decomposed into few blocks, the few blocks are effectively arranged into a printing space, and therefore, a printing process is effectively carried out.
Owner:SHINING 3D TECH CO LTD

Satellite orbit determining method and device based on maximum model decomposition

The invention provides a satellite orbit determining method and device based on maximum model decomposition. The satellite orbit determining method comprises the steps that based on the KAM principle, a Fourier series expansion model of position coordinates of a satellite is established when the satellite operates on an orbit; according to the descending order of amplitudes, the Fourier series expansion model of the position coordinates is decomposed, and a decomposed similar series expansion model of the position coordinates is obtained; based on the actual observation values of the position coordinates of the satellite when the satellite operates on the orbit, the amplitudes and the corresponding frequencies in the similar series expansion model of the position coordinates are determined; through the similar series expansion model of the position coordinates, the position coordinates of the satellite on the orbit at any moment are predicated. The satellite orbit is determined more rapidly and conveniently by the adoption of the satellite orbit determining method and device based on maximum model decomposition, the satellite orbit determining method and device based on maximum model decomposition is practical, only the frequencies and the amplitudes of the satellite orbit need to be computed and stored in the predication process, storage resources are saved, and the processing efficiency is greatly improved.
Owner:ACAD OF MATHEMATICS & SYSTEMS SCIENCE - CHINESE ACAD OF SCI

Structural parameter identification method for two-degree-of-freedom system based on vibration response signal

The invention relates to a structural parameter identification method for a two-degree-of-freedom based on a vibration response signal. The content of the structural parameter identification method comprises the steps of performing structural excitation, and acquiring a vibration displacement signal; acquiring a natural frequency and a natural angular frequency of each order of the system by applying FFT (Fast Fourier Transform); decomposing the vibration displacement signal by using a rapid empirical model decomposition method so as to acquire a plurality of intrinsic mode function (IMF) components; solving an instantaneous frequency of each IMF component, comparing the instantaneous frequency of each IMF component with the natural frequency acquired by FFT so as to screen out IMF components capable of representing the natural frequency of the system; processing the screened IMF components by applying Hilbert transform, acquiring each slowly-varying amplitude and slowly-varying phase angle of a vibration response, and performing parameter correction; and substituting known parameters into an identification model to solve, solving an average value, and acquiring structural parameters of the system. The structural parameter identification method can simultaneously utilize time-frequency domain information of data, is high in anti-noise capacity and can directly utilize vibration response data to perform parameter identification.
Owner:YANSHAN UNIV
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