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84 results about "Observed information" patented technology

In statistics, the observed information, or observed Fisher information, is the negative of the second derivative (the Hessian matrix) of the "log-likelihood" (the logarithm of the likelihood function). It is a sample-based version of the Fisher information.

Method for evaluating fatigue life of aged reinforced concrete bridge

ActiveCN105825030AThe prediction method is reasonableGeometric CADForecastingStress concentrationCrazing
The invention discloses a method for evaluating the fatigue life of an aged reinforced concrete bridge. The method comprises the following steps of obtaining initial corrosion time of reinforcement in concrete based on the second diffusion law of Fick, and considering the influence of concrete cracking due to corrosion expansion in a corrosion rate model; adopting a small crack growth and near threshold growth analysis and determining relevant parameters of fatigue crack propagation rate of materials by developing a fatigue crack propagation test of reinforced concrete materials; performing a corrosion fatigue test or finite element analysis on corroded reinforcement to obtain stress concentration factors at different corrosion levels, and integrating into a stress intensity factor model to obtain the fatigue crack propagation rate of the reinforcement under the influence of corrosion; comparing the magnitude of a corrosion pit growth rate and the fatigue crack propagation rate and gradually converting into a single growth analysis on fatigue cracks of the reinforcement; meanwhile, combining with vehicle load observing information to realize life evaluation of a bridge at different service stages. The prediction method disclosed by the invention is reasonable and high in popularization, and can provide technical support for evaluating the life of the concrete bridges.
Owner:CHANGSHA UNIVERSITY OF SCIENCE AND TECHNOLOGY

Noise suppression device and noise suppression method

Disclosed is a noise suppression device capable of better noise suppression by means of a simpler structure and with a lighter computational load. A noise suppression device (100) has a noise suppression processor (150) to estimate the required information only from the observed information, which is the required information corrupted by noise. A correlator (154) calculates the correlation of the estimation error when the state quantity, which contains the required information, of the system at time n+1 was estimated from the information until time n or time n+1 for the observed information at only time n. A weighting coefficient calculator (156) uses the correlation calculated by the correlator (154) for the observed information at only time n to calculate the weighting coefficients for specifying the relationships of the optimum estimate of the state quantity at that time based on the information until time n+1, the optimum estimate of the state quantity at time n+1 based on the information until time n, and the estimation error of the observed quantity including the observed information. An optimum estimate calculator (158) uses the weighting coefficients calculated by the weighting coefficient calculator (156) for the observed information only at time n to calculate the optimum estimate of the state quantity at that time based on the information until time n or time n+1.
Owner:TOKYO UNIVERSITY OF SCIENCE

Deep space autonomous navigation method based on observability degree analysis

The invention discloses a deep space autonomous navigation method based on observability degree analysis, which relates to the field of aerospace. The invention solves the problems that when the current autonomous navigation systems comprehensively use different observing models to provide measuring information, different types of measuring information of different sensors need to be processed, thereby reducing the utilization ratio of the observed information and simultaneously reducing the adaptive ability and reliability of the autonomous navigation systems. The method of the invention is established on the basis of a dynamic model of an earth-moon transfer orbit deep space probe, obtains the observability degree of the deep space autonomous navigation system under two observing models of a geocentric sight line vector and a selenocentric sight line vector by a nonlinear system observability degree analyzing method, and acquires the orbit parameters of the deep space probe by a UKF based federal filtering algorithm. The invention is suitable for determining the orbit parameters of deep space separated section and transfer section probes. The invention can be used for improving the accuracy and reliability of the deep space autonomous navigation system, and is especially suitable for the information fusion autonomous navigation technologies under various observing models.
Owner:HARBIN INST OF TECH

Correlation method for flight tracks of airborne radar and infrared sensor

InactiveCN102798867AMeasurement Origin Uncertainty Problem SolvingElectromagnetic wave reradiationRadarMulti target tracking
The invention discloses a correlation method for flight tracks of an airborne radar and an infrared sensor. According to the method, angle information observed by the airborne radar and the infrared sensor is fully utilized, wherein the angle information comprises an azimuth angle and a pitch angle. The correlation method comprises the steps of: on the basis of ambiguous comprehensive functions, establishing comprehensive discrimination functions by utilizing the observed information of the airborne radar and the infrared sensor; formulating a decision criterion; and finally determining judgment thresholds through counting characteristics and a correlation rate of the comprehensive judgment functions and then carrying out related judgment. The correlation method for the flight tracks of the airborne radar and the infrared sensor has the positive effect that on the basis of researching the sensor measurement origin uncertainty problem, by taking the airborne radar and the infrared sensor as examples, a driving/driven sensor flight track correlation method is disclosed on the basis of an ambiguous comprehensive theory; and the driving/driven sensor flight track correlation method not only can be used for solving the measurement origin uncertainty problem of multi-sensor observed information, but also can be applied to the flight track correlation problems related to multi-sensor multi-target tracking in the military or civil field.
Owner:UNIV OF ELECTRONICS SCI & TECH OF CHINA

Robot positioning precision evaluating method based on monocular vision

The invention discloses a robot positioning precision evaluating method based on monocular vision. A calibration plate is arranged at any position in a robot motion space, in the motion process, a robot observes the same calibration plate for many times at the different positions in the working environment of the robot, multiple times of sampling is conducted through an observing method in this way, and according to all observing information collected in the one-time motion process and statistical characteristics of the observing information, quantitative comparison of the positioning precision of different positioning algorithms in the same working environment is realized. According to the robot positioning precision evaluating method, the real position and posture of the robot are obtained without other precision instruments, a large number of repeated experimental tests are not needed, and the working efficiency is improved while the using cost is saved; in addition, the calibrationplate with the unknown environmental position and posture is adopted, thus the evaluating method is simpler and more convenient, and the motion environment and the motion space of the robot are not limited; and finally, the precision of a robot positioning algorithm is described by expression positively correlated with the positioning error, and the positioning precision between the different algorithms is compared.
Owner:九天创新(广东)智能科技有限公司

Spectral plane or focal plane installation and debugging method of hyperspectral imager

The invention relates to a spectral plane or focal plane installation and debugging method of a hyperspectral imager, relates to the field of imaging optical systems, and solves the problems that the existing hyper spectrometer imaging system is complex in the installation and debugging process and can not accurately adjust the position of a CCD (charge coupled device) focal plane component and frequent assembly and disassembly of the CCD focal plane component can easily result in damage to the CCD. The method comprises the following steps of: realizing equivalence between the position of a scribed line surface of a reticle in the bright background in a calibrated focal plane installation and debugging module and the position of a CCD light sensitive plane of the CCD focal plane component; replacing the CCD focal plane component by the installation and debugging module to debug an optical system; observing information, which is projected to the reticle by a camera, by using a microscope; figuring a CCD focal plane component adjustment pad to realize coincidence between a spectral line and the scribed line surface of the reticle; installing the CCD focal plane component and the calibrated CCD focal plane component adjustment pad in a matching mode; and replacing the installation and debugging module by the CCD focal plane component to finely adjust the position of the CCD focalplane. The method provided by the invention reduces frequent operations in the installation and debugging process of the CCD focal plane component and improves the reliability and stability of installation and debugging quality.
Owner:CHANGCHUN INST OF OPTICS FINE MECHANICS & PHYSICS CHINESE ACAD OF SCI

GPS (Global Position System) double-frequency real-time satellite borne data processing method

The invention relates to the technical field of satellite borne data processing, in particular to a GPS (Global Position System) double-frequency real-time satellite borne data processing method. The method comprises the following steps of: smoothing the motion states of all epoch satellites in the whole window by utilizing an observed value of an epoch position at the tail end of the window; integrating and forecasting a state-transition matrix from a tail end epoch of the window to a next epoch and the motion states of the epoch satellites by utilizing the motion states of all the epoch satellites in the window and a given state-transition matrix by adopting a multistep method; updating the window epoch, i.e. backwards moving the window to a novel epoch; and smoothing the motion states of all the epoch satellites in the window by utilizing novel observing information of forecasted epochs, and the like. In the method, the multistep method is adopted during updating the epochs, and a single-step method is used for intersection, thus the method has high numerical precision and better stability; the calculating times of integrating a right function is fewer, which can effectively improve the calculating speed; and a window moving method is adopted, thus the window length can be changed according to different calculation precision requirements, flexibility and variability are realized and the integrating precision is guaranteed.
Owner:WUHAN NAVIGATION & LBS INC

Mobile internet big data analysis sample information display device

ActiveCN111161649AWith dustproof functionReduce cleaning and maintenance frequencyIdentification meansDisplay deviceInformation quantity
The invention discloses a mobile internet big data analysis sample information display device, which comprises a bottom plate, a supporting column is fixedly connected to the top surface of the bottomplate, and a display box is arranged at the top end of the supporting column; a contrastive analysis device is matched with a reinforcing device; a worker can quickly disassemble and assemble a small-size writing board; further, the worker can conveniently move information needing to be compared and analyzed to an adjacent position for analysis and discrimination; the amount of information observed by the workers in the comparative analysis process is reduced; time and labor are saved, the rotating device is matched with the driving device; the contrastive analysis device can do circular motion; according to the information display device, key information sorted from different sample information can be conveniently displayed, the information display capacity is high, multiple pieces of key information are displayed at the same time, a decision maker can be helped to obtain unique changes of the sample information, the decision maker can make a decision which has a positive effect on enterprise development, and the practicability of the information display device is improved.
Owner:四川蜀天信息技术有限公司

Satellite borne rapid multi-step integration method for track in real-time precise orbit determination

The invention relates to the technical field of navigation satellite application, in particular to a satellite borne rapid multi-step integration method for a track in real-time precise orbit determination. The method comprises the following steps: selecting an integration window, and then smoothening the motion state of all epoch satellites in the whole window by virtue of the observed value at an epoch position at the tail end of the window; transferring matrix integration according to the updated motion state and the given state of all the epoch satellites in the window to calculate the new motion state of the epoch satellites; and finally updating a window epoch, i.e. moving backwards one epoch from the initial epoch of the window, and then smoothening the motion state of all the epoch satellites in the smoothening window by means of updating the observed information on the epoch at the tail end of the window. In the method, a multi-step method is adopted while updating the epoch and a single-step method while intersecting the epoch, thus achieving high numerical precision, better stability and smaller integral right-function calculation, transferring matrix information by the given state, avoiding updating state for matrix transfer while updating the state, reducing times for calculating integral right function, effectively improving calculating speed, transforming window length according to different calculation accuracy, and ensuring integral precision.
Owner:WUHAN UNIV
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