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30 results about "Robust analysis" patented technology

Robust Analysis, Inc. is a consulting and software company that specializes in analyzing problems that involve heavy tailed distributions.

Method for robust analysis of biological activity in microscopy images

A robust object segmentation method for analysis of biological activity receives an input image and performs segmentation confidence mapping using the input image to generate segmentation confidence map output. A thresholding is performed using the object segmentation confidence map to generate a high confidence object mask output. An object segmentation confidence mapping method for analysis of biological activity receives an input image and performs segmentation decision to create segmentation decision result. A difference operation is performed to generate the segmentation decision result. A confidence mapping is performed using the difference result to generate segmentation confidence. An object level robust analysis method for biological activity receives an input image and performs object segmentation using the input image to create object segmentation result. A robust object feature measurement is performed to generate robust object feature result. An FOV level robust analysis method for biological activity receives a plurality of object feature results and performs robust FOV summary feature extraction to create robust FOV summary features. A FOV regulated feature extraction is performed to generate FOV regulated features. A FOV regulated feature extraction method for biological activity receives a plurality of object feature results and performs control object selection using the plurality of object feature results to generate control objects output. A FOV regulated feature extraction is performed to generate FOV regulation features output. An object feature FOV regulation is performed using the plurality of object feature results and the FOV regulation features to generate FOV regulated object features output. A sample level robust analysis method for biological activity receives a plurality of FOV feature results and performs robust sample summary feature extraction to create robust sample summary features. A sample regulated feature extraction is performed to generate sample regulated features. An assay level robust analysis method for biological activity receives a plurality of sample feature results and performs robust assay summary feature extraction to create robust assay summary features. An assay regulated feature extraction is performed to generate assay regulated features.
Owner:LEICA MICROSYSTEMS CMS GMBH

System, method, and computer-accessible medium for providing a multi-objective evolutionary optimization of agent-based models

Agent-based models (ABMs) / multi-agent systems (MASs) are one of the most widely used modeling-simulation-analysis approaches for understanding the dynamical behavior of complex systems. These models can be often characterized by several parameters with nonlinear interactions which together determine the global system dynamics, usually measured by different conflicting criteria. One problem that can emerge is that of tuning the controllable system parameters at the local level, in order to reach some desirable global behavior. According to one exemplary embodiment t of the present invention, the tuning of an ABM for emergency response planning can be cast as a multi-objective optimization problem (MOOP). Further, the use of multi-objective evolutionary algorithms (MOEAs) and procedures for exploration and optimization of the resultant search space can be utilized. It is possible to employ conventional MOEAs, e.g., the Nondominated Sorting Genetic Algorithm II (NSGA-II) and the Pareto Archived Evolution Strategy (PAES), and their performance can be tested for different pairs of objectives for plan evaluation. In the experimental results, the approximate Pareto front of the non-dominated solutions is effectively obtained. Further, a conflict between the proposed objectives can be seen. Additional robustness analysis may be performed to assist policy-makers in selecting a plan according to higher-level information or criteria which is likely not present in the original problem description.
Owner:NEW YORK UNIV

Decomposition method and calculation method for structure mechanism failure probability sensitivity, and application

The invention relates to the technical field of reliability and robustness analysis, and puts forward a decomposition method for structure mechanism failure probability sensitivity on the basis of a Copula function. The method comprises the following steps that: showing a multidimensional variable joint distribution function as a Copula function form so as to establish a relational expression, which is disclosed in the following diagram, of the multidimensional random variable joint distribution function and a marginal probability density function, wherein fX(x) is a joint probability densityfunction, C(u1,...,un) is the Copula function, and fXi(xi) is the marginal probability density function; and on the basis of the relational expression, decomposing the structure mechanism failure probability sensitivity into a sum of independent sensitivity and relevant sensitivity. By use of the method, the Copula function is introduced to describe the joint probability distribution of an input variable, the failure probability sensitivity is decomposed into the independent sensitivity and the relevant sensitivity so as to separate the influences of variable dependency and independence independently for the calculation of the failure probability sensitivity, and a technical method obtained by searching provides a theoretical basis for design personnel to measure the functions of input variable dependency and independence in the analysis of the failure probability sensitivity.
Owner:NORTHWESTERN POLYTECHNICAL UNIV

Stamping covering part springback analysis and compensation method based on AutoForm software

ActiveCN113333559AAddressing Insufficient AccuracyAccurate Springback Compensation DataShaping toolsDesign optimisation/simulationRobust analysisStructural engineering
The invention relates to the technical field of analogue simulation methods, in particular to a stamping covering part springback analysis and compensation method based on AutoForm software. The stamping covering part springback analysis and compensation method comprises the steps that simulation analysis and sigma robustness analysis are conducted on a covering part tool body, and an optimized full-process scheme and an optimized clamping scheme are obtained through repeated iterative adjustment; a springback compensation result of the tool body is obtained according to the full-process scheme and the clamping scheme; a reconstructed tool body profile is redrawn according to a compensated tool body profile exported by the AutoForm software; and press deflection compensation work is conducted according to the reconstructed tool body profile and press equipment parameters, and final die machining data are obtained after compensation is completed. According to the stamping covering part springback analysis and compensation method based on the AutoForm software, the sigma robustness analysis process is introduced into a traditional springback compensation analysis method, the reasonable fluctuation conditions of various key elements in actual production are fully considered, thus the process scheme closer to the real condition is obtained, and the formability problems of cracking, wrinkling and the like are avoided.
Owner:VOYAH AUTOMOBILE TECH CO LTD

A springback analysis and compensation method for stamping cover parts based on autoform software

ActiveCN113333559BAddressing Insufficient AccuracyAccurate Springback Compensation DataShaping toolsDesign optimisation/simulationRobust analysisSoftware engineering
The invention relates to the technical field of simulation simulation methods, in particular to a springback analysis and compensation method for stamping cover parts based on AutoForm software. The present invention obtains an optimized full-process scheme and a clamping scheme by performing simulation analysis and sigma robustness analysis on the tool body of the cover, and through repeated iterative adjustment, and obtains the springback compensation of the tool body according to the full-process scheme and the clamping scheme As a result, the reconstructed tool body profile was redrawn based on the compensated tool body profile derived from AutoForm software, and the press deflection compensation was carried out according to the reconstructed tool body profile according to the press equipment parameters, and the final mold processing data was obtained after the compensation was completed. In the present invention, the sigma robustness analysis process is introduced into the traditional springback compensation analysis method, and the reasonable fluctuations of various key elements in actual production are fully considered, so as to obtain a process plan that is closer to the real situation, and avoid cracking, Formability problems such as wrinkling.
Owner:VOYAH AUTOMOBILE TECH CO LTD

Flight test determination method of multi-input and multi-output equivalent pneumatic servo elastic robust stability

InactiveCN102081349BFlutter boundary stability stableReduce conservatismAdaptive controlMulti inputDecomposition
The invention discloses a flight test determination method of the multi-input and multi-output equivalent pneumatic servo elastic robust stability, used for solving the technical problems of the conservation and complex calculation of the traditional robust analysis method. Based on the technical scheme, the flight test determination method comprises the following steps of obtaining an open-loop transfer function frequency characteristic matrix of a multi-input and multi-output system through a frequency sweeping flight test and the like; lagging a phase angle through serial gaining at each loop; obtaining a scalar judgment formula of phase and amplitude margin between two adjacent flutter frequency regions according to direct equivalence of the closed-loop frequency characteristics by carrying out characteristic decomposition on the system open-loop transfer function frequency characteristic matrix; and calculating the phase margin and the ASE stability at the flutter frequency in a mode similar to a single-input and single-output system. The invention simplifies the problems through characteristic linear conversion, obtains the scalar judgment formula, gives a calculation methodof the flutter boundary stability, the margin and the safety during elastic flight of a canard wing aircraft and reduces the conservation of the traditional method.
Owner:NORTHWESTERN POLYTECHNICAL UNIV

A Robustness Analysis Method for Spacecraft Orbit Control Strategy

The invention relates to robustness analysis method for a spacecraft orbit control strategy, and belongs to the technical field of the spacecraft orbit dynamics and control. The robustness analysis method comprises the following steps: modeling orbital motion of the spacecraft through a Gauss orbit element perturbation equation; analyzing the non-spherical perturbation of a low-orbit satellite and the atmospheric drag perturbation; designing an orbit maintaining strategy to execute the maintaining control to the spacecraft orbit elements; using a differential correcting algorithm to improve the precision of the orbit maintaining; building a position error, velocity error and engine thrust error model in the running process of the spacecraft; designing a calculation model of spacecraft control error mean, variance and error distribution proportion; and using a Monte Carlo simulation method to execute the simulation analysis to the spacecraft orbit control strategy with the error, and building a robustness evaluation system of the orbit control strategy. In the control strategy design, the actual situation of the satellite orbit control is considered adequately, and the feasibility of the method in the actual project is guaranteed under the precondition of simpliness and convenience and according with the actual situation.
Owner:BEIJING INSTITUTE OF TECHNOLOGYGY
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