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34 results about "Maximally informative dimensions" patented technology

Maximally informative dimensions is a dimensionality reduction technique used in the statistical analyses of neural responses. Specifically, it is a way of projecting a stimulus onto a low-dimensional subspace so that as much information as possible about the stimulus is preserved in the neural response. It is motivated by the fact that natural stimuli are typically confined by their statistics to a lower-dimensional space than that spanned by white noise. Within this subspace, however, stimulus-response functions may be either linear or nonlinear. The idea was originally developed by Tatyana Sharpee, Nicole Rust, and William Bialek in 2003.

Method and system for maximum-informativeness information extraction using a domain-specific ontology

A method transforms unstructured text into structured data in a domain-specific ontology. The method includes recording an input block of text using an information extraction module (IEM), accessing a domain-specific ontology and supplemental data in a knowledge source(s) via the IEM, processing the input text block, and using the IEM to generate a plurality of nodes in the domain-specific ontology. Each node classifies the unstructured text to corresponding objects of interest, thereby transforming the unstructured text into the structured data. An IEM is also provided having a computer device and an algorithm executable thereby to transform unstructured text into structured data in a domain-specific ontology. The IEM is adapted for recording a text phrase using the computer device, accessing and retrieving the domain-specific ontology and supplemental data from a knowledge source(s), and processing the text block using the computer device to generate a plurality of nodes in the domain-specific ontology.
Owner:GM GLOBAL TECH OPERATIONS LLC

Information recording method, information recording device, information recording system, program, and recording medium

An information recording method records information to a multilayer recording medium in which a number of record layers are laminated and recording of information to each record layer is possible. When an amount of the information being recorded to the medium does not exceed a maximum amount of information which can be recorded to the medium, the information being recorded to the medium is divided into data blocks by the number of the record layers. The data blocks are recorded to data areas of the respective record layers so that the recording areas of the record layers where the data blocks are recorded are overlapped each other with respect to a thickness direction of the medium.
Owner:RICOH KK

Cross-age face recognition method

ActiveCN106650650ASolve the problem of low face recognition rate across agesSolve the low recognition rateCharacter and pattern recognitionPattern perceptionCosine Distance
The invention provides a cross-age face recognition method. According to the method, a cross-age face recognition system composed of two modules (a maximum entropy feature description module and an aging perception de-noising automatic coding module) is obtained by training a large amount of face images including four age groups, thereby realizing recognition on any two different age face images. The maximum entropy feature description module allocates codes including maximum information amount by using maximum entropy splitting of a decision tree, the aging perception de-noising automatic coding module reconstructs a feature descriptor of any age group into feature descriptors of four different age groups, the descriptors are integrated to obtain a face integrated feature vector for eliminating aging influencing, and face recognition is finally realized by calculating the cosine distance of integrated feature vectors of different faces. The method can well reduce the information loss problem of some traditional descriptors, eliminates the influence of the aging factor in cross-age face recognition, and has good performance in the cross-age face recognition problem.
Owner:SYSU CMU SHUNDE INT JOINT RES INST +1

Targeted trapping and sequencing kit for lung cancer-related 285 genes and application of targeted trapping and sequencing kit

The invention discloses a targeted trapping and sequencing kit for 285 lung cancer-related genes and application of the targeted trapping and sequencing kit. The kit is based on hybrid trapping of a probe, and can be used for preparing a high-throughput library of the lung cancer-related 285 genes and simultaneously detecting all variation loci on exons of the 285 genes, so that the disadvantagesof high cost, high time consumption, tedious operation and the like of conventional single-gene detection are overcome. Detection of a plurality of genes with a single small sample is implemented in the small sample for aspiration biopsy of lung cancer, and the clinical practice requirements of maximally using the small sample and obtaining a maximum amount of information are met. The kit is basedon an Ion Proton platform, has high accuracy and sensitivity, and has obvious advantages compared with a Sanger sequencing method, and a detection result in a residual DNA (deoxyribonucleic acid) sample of a paraffin sample is stable.
Owner:GUANGDONG GENERAL HOSPITAL

Three-dimension microscopic observation method of plant leaf stoma in vivo

InactiveCN102221347AGuaranteed maximum amount of informationGuaranteed amount of informationUsing optical meansStomaMicroscopic observation
The invention relates to a three-dimension microscopic observation method of plant leaf stoma in vivo. The method comprises the following steps that: firstly, optical amplifier components are connected with a focusing guide rail and a varifocus lens is connected with a CCD image acquisition sensor; the focusing guide rail is connected with a connection plate and the connection plate is connected with a horizontal fine tuning guide rail; then, a measured plant is placed on a measured-object load-bearing platform and a observation area of a measured leaf is fixed; the CCD image acquisition sensor is connected with an upper computer so as to real-timely collecting and observing leaf stomata through image acquisition software; finally, an image of a leaf surface can be acquired through automatically focusing or manually focusing and a three dimensional image of leaf surface stoma states can be obtained after performing image denosing, curve smoothing and curve fitting on collected data. By using the method of the invention, when the plant leaves are not separated with the plant body, stoma state images can be continuously collected, and normal plant growth state can be two-dimensionally observed or leaf stoma change status under a specific experiment state can be two-dimensionally observed. Therefore, maximum information of the leaf stomata can be guaranteed.
Owner:CHINA JILIANG UNIV

Aircraft modeling method based on variable measurement number maximum information criterion

InactiveCN102867130AEasy to set upAvoid incorrect technical questionsSpecial data processing applicationsDiscriminantModel method
The invention discloses an aircraft modeling method based on a variable measurement number maximum information criterion. The aircraft modeling method is used for solving the technical problems of poor proving correctness of pneumatic models and parameters provided by flight tests due to the maximum information criterion when observation vectors of existing different flight tests are not the same. The technical scheme includes that during aircraft model modeling and model validation, different flight test factor amendment modeling and model validation criteria of an aircraft are acquired by analyzing the influence of different observation vectors to the maximum information content criterion, and scalar model selection and testing discriminant is acquired through U-D decomposition of measurement variance estimation Rj and Rj+1. By the method, aerodynamic force models and moment models of the aircraft can be established directly conveniently according to flight test data, the technical problem that the aerodynamic force models are established and tested incorrectly according to different flight test data due to the fact that influence of different observations to the maximum information criterion is not considered directly.
Owner:NORTHWESTERN POLYTECHNICAL UNIV

Aircraft modeling method based on maximum information-reliability online identification criterion

The invention discloses an aircraft modeling method based on a maximum information-reliability online identification criterion. The technical problems that the proving correctness of aerodynamic models and parameters verified by a flight test is poor caused by a simplified model identification criterion are solved. The technical scheme includes that data lengths are considered and reliable parameters are introduced in a maximum information criterion, an online modeling criterion is corrected, the division of U-D of Rj and Rj+1 is evaluated for the measurement variance, and a scalar online model selection and verified discriminant is obtained. The method has the advantages that aerodynamic models and moment models of an aircraft can be established on line directly in accordance with flight test data, and the technical problems of aircraft high attack angle model establishment and verification according to flight tests caused by a simplified model determination criterion are solved.
Owner:NORTHWESTERN POLYTECHNICAL UNIV

Information recording method, information recording device, information system, program, and recording medium

An information recording method records information to a multilayer recording medium in which a number of record layers are laminated and recording of information to each record layer is possible. When an amount of the information being recorded to the medium does not exceed a maximum amount of information which can be recorded to the medium, the information being recorded to the medium is divided into data blocks by the number of the record layers. The data blocks are recorded to data areas of the respective record layers so that the recording areas of the record layers where the data blocks are recorded are overlapped each other with respect to a thickness direction of the medium.
Owner:RICOH KK

Matching method and device of images based on JPEG format

The embodiment of the invention discloses a matching method and device of images based on a JPEG format. The method includes the steps of obtaining a source datum, to be matched, of a source image in the JPEG format, wherein the source datum to be matched are an item located in the first row and the first column in an 8-order matrix of the source image, obtaining a target datum, to be matched, of a target image, wherein the target datum to be matched is an item in the first row and the first column in an 8-order matrix of the target image, judging whether the source datum to be matched and the target datum to be matched meet a preset matching condition, determining that the target image meeting the preset matching condition is matched with the source image if the answer is positive, and determining the target image is not matched with the source image if the answer is negative. Imaging matching can be finished only by comparing the items in the first rows and the first columns of the 8-order matrixes with the largest image information amount, calculation in the image matching process is reduced to the largest extent, and image matching efficiency is improved.
Owner:ANYKA (GUANGZHOU) MICROELECTRONICS TECH CO LTD

Aircraft modeling method based on maximum information content-credibility criterion of variable metrical data

InactiveCN102890452AEasy to set upAvoid incorrect technical questionsSimulator controlGuidelineModel method
The invention discloses an aircraft modeling method based on a maximum information content-credibility criterion of variable metrical data, which is used for solving the technical problem of poor accuracy of parameter calibration of aerodynamic models provided by flight tests caused by the maximum information content criterion when the observation vectors of the conventional different flight tests are different. According to the technical scheme, the method comprises the following steps of: analyzing the influence of the difference of the observation vectors on the maximum information content criterion during modeling and model validation of an aircraft, and introducing a credibility parameter to obtain a criterion on modeling rectification and model verification according to different flight test factors of the aircraft; and decomposing U-D of measured variance estimation Rj and Rj+1 to obtain a scalar model selection and verification discriminant. The method provided by the invention is convenient for directly establishing aerodynamic and moment models of the aircraft according to flight test data, and avoids the technical problem that the aerodynamic model is incorrectly established and verified by different flight test data due to that the different observations are not directly considered in the maximum information content criterion.
Owner:NORTHWESTERN POLYTECHNICAL UNIV

Aircraft modeling method based on variable data length maximum information amount-credibility criterion

InactiveCN102867129AEasy to set upAvoid incorrect technical questionsSpecial data processing applicationsModel methodDecomposition
The invention discloses an aircraft modeling method based on a variable data length maximum information amount-credibility criterion. The method is used for solving the technical problems that the existing maximum information amount criterion does not consider data length so that proving correctness of a pneumatic model and parameters of flying tests is poor. The technical scheme is that by considering the data length in the maximum information amount criterion and introducing credibility parameters, and a modeling criterion is revised according to different flying test factors of an aircraft. U-D decomposition of Rj and Rj+1 is estimated on measuring variance, and scalar model selecting and verification discriminant are obtained. The aircraft modeling method is favorable for building aircraft aerodynamic force and moment models according to flying test data directly, and the technical problems that the maximum information amount criterion does not consider data length directly so as to be wrong to establish and verify pneumatic models with different flying test data are solved.
Owner:NORTHWESTERN POLYTECHNICAL UNIV

Modeling method of aircraft based on maximum information quantity-reliability rule

The invention discloses a modeling method of an aircraft based on a maximum information quantity-reliability rule, to solve the technical problem that an aerodynamic model and parameters provided from a flight test are low in correctness due to the existing maximum information quantity rule. According to the technical scheme, reliability parameters are introduced into the maximum information quantity rule, and a modeling rule can be corrected according to flight test factors of different aircrafts; and measurement variances Rj and Rj+1 are estimated and subjected to U-D decomposition so as to obtain a scalar model selection discriminant. Aerodynamic and moment models of the aircraft can be directly and conveniently established according to flight test data, and the technical problem that the aerodynamic model and the parameters obtained from the flight test are incorrect due to increment of fixed parameters in the maximum information quantity rule can be solved.
Owner:NORTHWESTERN POLYTECHNICAL UNIV

Gene probe composition for detecting idiopathic epilepsy, kit and applications

ActiveCN109439741AAccurately discover genetic informationReduce clinical testing costsNucleotide librariesMicrobiological testing/measurementSmall sampleCLCN2
The invention provides gene probe composition for detecting idiopathic epilepsy, a kit and applications. The gene probe composition for detecting idiopathic epilepsy is different in that the gene probe composition comprises an SCN2A gene probe, an SCN1A gene probe, a KCNQ2 gene probe, a CHRNA4 gene probe, a GABRA1 gene probe, a GABRD gene probe, an LGI1 gene probe, a CLCN2 gene probe and a CACNA1Hgene. The detection kit is based on probe hybridization capture, has the advantages of high throughput and simultaneous detection of high-frequency mutation sites on a plurality of gene exons, and the disadvantages of high cost, long time consumption, complicated operation and the like of traditional single gene detection are changed. Detection of multiple genes in a single small sample is realized, and clinical practice requirements of maximum small sample utilization and maximum information amount acquisition are met.
Owner:合肥新唯基因科技有限公司

Aircraft modeling method based on adjustable parameter maximum information criterion

The invention discloses an aircraft modeling method based on an adjustable parameter maximum information criterion. The method is used for solving a technical problem that an aerodynamic model and parameters given by a flight test are poor in correction due to the existing maximum information criterion. The technical scheme of the invention is as follows: introducing an adjustable parameter through a maximum information criterion, and correcting a modeling criterion according to flight test factors of different aircrafts; and carrying out U-D factorization on measurement variance estimations Rj and R(j+1) to acquire a scalar model selection discriminant. The aircraft modeling method is convenient to directly establish aerodynamic and moment models according to the flight test data, thus avoiding a technical problem that the aerodynamic model and parameters acquired by the flight test are incorrect based on the maximum information criterion due to increased fixed parameters.
Owner:NORTHWESTERN POLYTECHNICAL UNIV

A hierarchical behavioral profile

In a hierarchical profile, each node represents at least one feature of behavioral data collected (300) about an entity (102) profiled, with the topmost node selected (306) as the "statistically most informative" feature of the data. A profile can cover numerous domains and be predictively very powerful in each domain. A number of observations can be "aggregated" (316) together into a single datapoint. In use, the structure of the profile is compared (402) against current information associated with the entity to produce (406) a recommendation or prediction. If the profile represents at least some data aggregation, then new observations (500) are folded (504a, 504b, 504c) into the profile based on statistical weights of the aggregations. Because of the way the profile is created and updated, its hierarchical structure maps the collected observations. Therefore, as new observations are incorporated, if the new observations change (600a) the profile's structure significantly, then it can be hypothesized (602) that something "interesting" has happened to the entity.
Owner:GOOGLE TECH HLDG LLC

A method and a system for information transmission based on graphics encoded data

The invention discloses a method and a system for transmitting information based on graphics encoded data. The method comprises the following steps: obtaining application description information; determining a plurality of applications wishing to transmit information through the graphics encoded data based on the application description information; and determining a plurality of applications wishing to transmit information through the graphics encoded data. According to the information transmission requirements of each application, determining the maximum amount of information needed by eachapplication to transmit information through a single graphic encoded data; parsing a graphical interface of each application for providing graphical encoded data to determine a display range that eachapplication can use to display graphical encoded data; determining an encoding ratio of an image region for graphics encoded data for each application based on a display range and a maximum amount ofinformation; and generating raw graphics encoded data conforming to the encoding scale when a specific application of the plurality of applications desires information transfer, and performing information transfer based on the raw graphics encoded data conforming to the encoding scale.
Owner:BEIJING QIHOO TECH CO LTD

Nighttime image enhancing method with highlight inhibition

The invention discloses a nighttime image enhancing method with high light inhibition, which comprises the following steps: step 1, converting the color system of an image from an RGB color system to an HSV color system, reserving H and S channel information in the color information, and only processing a brightness channel V; step 2, pre-enhancing the image; step 3, determining inhibition parameters including an inhibited template and a shim range, and then inhibiting a highlight area; step 4, widening a histogram, redistributing the grey level of the image pixel by using an empty gray levelgenerated in highlight inhibition to widen the histogram; and step 5, normalizing the image, and then converting from the HSV color system to the RGB color system for displaying to obtain the enhanced nighttime image. The method of the invention can effectively enhance the nighttime image, inhibits highlights in the image, and improves the contrast ratio of the image to the uttermost extent without changing the relation of the original image pixels, so that the image can express the maximum information amount.
Owner:XIAN UNIV OF TECH

Three-dimension microscopic observation method of plant leaf stoma in vivo

InactiveCN102221347BGuaranteed maximum amount of informationGuaranteed amount of informationUsing optical meansStomaMicroscopic observation
The invention relates to a three-dimension microscopic observation method of plant leaf stoma in vivo. The method comprises the following steps that: firstly, optical amplifier components are connected with a focusing guide rail and a varifocus lens is connected with a CCD image acquisition sensor; the focusing guide rail is connected with a connection plate and the connection plate is connected with a horizontal fine tuning guide rail; then, a measured plant is placed on a measured-object load-bearing platform and a observation area of a measured leaf is fixed; the CCD image acquisition sensor is connected with an upper computer so as to real-timely collecting and observing leaf stomata through image acquisition software; finally, an image of a leaf surface can be acquired through automatically focusing or manually focusing and a three dimensional image of leaf surface stoma states can be obtained after performing image denosing, curve smoothing and curve fitting on collected data. By using the method of the invention, when the plant leaves are not separated with the plant body, stoma state images can be continuously collected, and normal plant growth state can be two-dimensionally observed or leaf stoma change status under a specific experiment state can be two-dimensionally observed. Therefore, maximum information of the leaf stomata can be guaranteed.
Owner:CHINA JILIANG UNIV

Aircraft modeling method based on variable data length maximum information amount-credibility criterion

InactiveCN102867129BEasy to set upAvoid incorrect technical questionsSpecial data processing applicationsModel methodDecomposition
The invention discloses an aircraft modeling method based on a variable data length maximum information amount-credibility criterion. The method is used for solving the technical problems that the existing maximum information amount criterion does not consider data length so that proving correctness of a pneumatic model and parameters of flying tests is poor. The technical scheme is that by considering the data length in the maximum information amount criterion and introducing credibility parameters, and a modeling criterion is revised according to different flying test factors of an aircraft. U-D decomposition of Rj and Rj+1 is estimated on measuring variance, and scalar model selecting and verification discriminant are obtained. The aircraft modeling method is favorable for building aircraft aerodynamic force and moment models according to flying test data directly, and the technical problems that the maximum information amount criterion does not consider data length directly so as to be wrong to establish and verify pneumatic models with different flying test data are solved.
Owner:NORTHWESTERN POLYTECHNICAL UNIV

Modeling method of aircraft based on maximum information quantity-reliability rule

The invention discloses a modeling method of an aircraft based on a maximum information quantity-reliability rule, to solve the technical problem that an aerodynamic model and parameters provided from a flight test are low in correctness due to the existing maximum information quantity rule. According to the technical scheme, reliability parameters are introduced into the maximum information quantity rule, and a modeling rule can be corrected according to flight test factors of different aircrafts; and measurement variances Rj and Rj+1 are estimated and subjected to U-D decomposition so as to obtain a scalar model selection discriminant. Aerodynamic and moment models of the aircraft can be directly and conveniently established according to flight test data, and the technical problem that the aerodynamic model and the parameters obtained from the flight test are incorrect due to increment of fixed parameters in the maximum information quantity rule can be solved.
Owner:NORTHWESTERN POLYTECHNICAL UNIV

Aircraft modeling method based on maximum information content-credibility criterion of variable metrical data

InactiveCN102890452BEasy to set upAvoid incorrect technical questionsSimulator controlModel methodModel selection
The invention discloses an aircraft modeling method based on a maximum information content-credibility criterion of variable metrical data, which is used for solving the technical problem of poor accuracy of parameter calibration of aerodynamic models provided by flight tests caused by the maximum information content criterion when the observation vectors of the conventional different flight tests are different. According to the technical scheme, the method comprises the following steps of: analyzing the influence of the difference of the observation vectors on the maximum information content criterion during modeling and model validation of an aircraft, and introducing a credibility parameter to obtain a criterion on modeling rectification and model verification according to different flight test factors of the aircraft; and decomposing U-D of measured variance estimation Rj and Rj+1 to obtain a scalar model selection and verification discriminant. The method provided by the invention is convenient for directly establishing aerodynamic and moment models of the aircraft according to flight test data, and avoids the technical problem that the aerodynamic model is incorrectly established and verified by different flight test data due to that the different observations are not directly considered in the maximum information content criterion.
Owner:NORTHWESTERN POLYTECHNICAL UNIV

Aircraft modeling method based on variable data length maximum information criterion

The invention discloses an aircraft modeling method based on a variable data length maximum information criterion. The technical problems that the proving correctness of aerodynamic models and parameters verified by a flight test is poor caused by the fact that data lengths are not considered in a prior maximum information criterion are solved. The technical scheme includes that data lengths are considered in the maximum information criterion, a modeling criterion is corrected in accordance with various flight test factors of an aircraft, the division of U-D of Rj and Rj+1 is evaluated for the measurement variance, and a scalar model selection and verified discriminant is obtained. The method has the advantages that aerodynamic models and moment models of the aircraft can be established directly in accordance with flight test data, and the technical problem that aerodynamic models established and verified by different flight test data are not correct caused by the fact that data lengths are not considered in the prior maximum information criterion directly is solved.
Owner:NORTHWESTERN POLYTECHNICAL UNIV

Aircraft modeling method based on maximum information amount on-line identification criterion

InactiveCN102866630AEasy to set up onlineRevised Online Modeling GuidelinesAdaptive controlReduced modelModel method
The invention discloses an aircraft modeling method based on a maximum information amount on-line identification criterion. The aircraft modeling method based on the maximum information amount on-line identification criterion is used for solving the technical problem that an existing simplified model identification criterion enables a pneumatic model and parameter calibration correctness given through flight test to be poor. The technical scheme is that the data length is considered and an on-line modeling criterion is revised according to the maximum information amount criterion; and an on-line model selecting and verifying discriminant is obtained through U-D disintegration of measurement variance estimates Rj and Pj+1. The aircraft modeling method facilitates on-line building of an aerodynamic force model and a force moment model of an aircraft according to flight test data directly, and solves the technical problem existing in building and verifying process of an aircraft high-incidence model according to a flight test.
Owner:NORTHWESTERN POLYTECHNICAL UNIV

Aircraft modeling method based on variable measurement number maximum information criterion

InactiveCN102867130BEasy to set upAvoid incorrect technical questionsSpecial data processing applicationsDiscriminantModel method
The invention discloses an aircraft modeling method based on a variable measurement number maximum information criterion. The aircraft modeling method is used for solving the technical problems of poor proving correctness of pneumatic models and parameters provided by flight tests due to the maximum information criterion when observation vectors of existing different flight tests are not the same. The technical scheme includes that during aircraft model modeling and model validation, different flight test factor amendment modeling and model validation criteria of an aircraft are acquired by analyzing the influence of different observation vectors to the maximum information content criterion, and scalar model selection and testing discriminant is acquired through U-D decomposition of measurement variance estimation Rj and Rj+1. By the method, aerodynamic force models and moment models of the aircraft can be established directly conveniently according to flight test data, the technical problem that the aerodynamic force models are established and tested incorrectly according to different flight test data due to the fact that influence of different observations to the maximum information criterion is not considered directly.
Owner:NORTHWESTERN POLYTECHNICAL UNIV

Aircraft modeling method based on maximum information-reliability online identification criterion

The invention discloses an aircraft modeling method based on a maximum information-reliability online identification criterion. The technical problems that the proving correctness of aerodynamic models and parameters verified by a flight test is poor caused by a simplified model identification criterion are solved. The technical scheme includes that data lengths are considered and reliable parameters are introduced in a maximum information criterion, an online modeling criterion is corrected, the division of U-D of Rj and Rj+1 is evaluated for the measurement variance, and a scalar online model selection and verified discriminant is obtained. The method has the advantages that aerodynamic models and moment models of an aircraft can be established on line directly in accordance with flight test data, and the technical problems of aircraft high attack angle model establishment and verification according to flight tests caused by a simplified model determination criterion are solved.
Owner:NORTHWESTERN POLYTECHNICAL UNIV
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