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726 results about "Random error" patented technology

Multi-dimensional data protection and mirroring method for micro level data

The invention discloses a data validation, mirroring and error/erasure correction method for the dispersal and protection of one and two-dimensional data at the micro level for computer, communication and storage systems. Each of 256 possible 8-bit data bytes are mirrored with a unique 8-bit ECC byte. The ECC enables 8-bit burst and 4-bit random error detection plus 2-bit random error correction for each encoded data byte. With the data byte and ECC byte configured into a 4 bit×4 bit codeword array and dispersed in either row, column or both dimensions the method can perform dual 4-bit row and column erasure recovery. It is shown that for each codeword there are 12 possible combinations of row and column elements called couplets capable of mirroring the data byte. These byte level micro-mirrors outperform conventional mirroring in that each byte and its ECC mirror can self-detect and self-correct random errors and can recover all dual erasure combinations over four elements. Encoding at the byte quanta level maximizes application flexibility. Also disclosed are fast encode, decode and reconstruction methods via boolean logic, processor instructions and software table look-up with the intent to run at line and application speeds. The new error control method can augment ARQ algorithms and bring resiliency to system fabrics including routers and links previously limited to the recovery of transient errors. Image storage and storage over arrays of static devices can benefit from the two-dimensional capabilities. Applications with critical data integrity requirements can utilize the method for end-to-end protection and validation. An extra ECC byte per codeword extends both the resiliency and dimensionality.
Owner:HALFORD ROBERT

Error recovery within processing stages of an integrated circuit

An integrated circuit includes a plurality of processing stages each including processing logic 1014 , a non-delayed signal-capture element 1016 , a delayed signal-capture element 1018 and a comparator 1024 . The non-delayed signal-capture element 1016 captures an output from the processing logic 1014 at a non-delayed capture time. At a later delayed capture time, the delayed signal-capture element 1018 also captures a value from the processing logic 1014 . An error detection circuit 1026 and error correction circuit 1028 detect and correct random errors in the delayed value and supplies an error-checked delayed value to the comparator 1024 . The comparator 1024 compares the error-checked delayed value and the non-delayed value and if they are not equal this indicates that the non-delayed value was captured too soon and should be replaced by the error-checked delayed value. The non-delayed value is passed to the subsequent processing stage immediately following its capture and accordingly error recovery mechanisms are used to suppress the erroneous processing which has occurred by the subsequent processing stages, such as gating the clock and allowing the correct signal values to propagate through the subsequent processing logic before restarting the clock. The operating parameters of the integrated circuit, such as the clock frequency, the operating voltage, the body biased voltage, temperature and the like are adjusted so as to maintain a finite non-zero error rate in a manner that increases overall performance.
Owner:ARM LTD +1

Temperature compensation method for denoising fiber-optic gyroscope on basis of time series analysis

A temperature compensation method for denoising a fiber-optic gyroscope on the basis of time series analysis comprises four steps of: step 1, designing an experimental scheme, performing fixed point low and high temperature testing experiment on the fiber-optic gyroscope, and utilizing acquisition software for data acquisition; step 2, performing time series analysis on the zero offset data of the gyroscope, and establishing the mathematical model of the random error of the fiber-optic gyroscope; step 3, adopting a kalman filtering algorithm to filter random noise in the zero offset data of the fiber-optic gyroscope; and step 4, utilizing the data which is de-noised by the kalman filtering to identify the model structure of the temperature shift error of the fiber-optic gyroscope, and calculating the parameters of the identified model. The method establishes the multinomial model of the static temperature shift error of the fiber-optic gyroscope through time series analysis, kalman filtering denoising treatment and identification of the temperature shift error model structure and parameters. The method completely meets the real-time compensation requirement on the project, and has a better practicable value and a wide application prospect in the technical field of aerospace navigation.
Owner:BEIHANG UNIV

Method for detecting mutation information in multiplex amplification sequencing product of genome

The invention discloses a method for detecting mutation information in a multiplex amplification sequencing product of a genome. The method comprises steps as follows: sequencing data are subjected to quality assessment and preprocessing; a recognizable sequencing sequence is selected for sequence assembling; the recognizable sequencing sequence or a sequence obtained through assembling is compared with a reference gene sequence, and preliminary variation information is obtained; fine calibration of sequence variation is performed according to different types of conditions; a calibrated sequencing fragment is obtained; the homozygosis or heterozygosis state of a target fragment is obtained according to the type of the sequencing fragment with the highest abundance; finally, the mutation information in the multiplex amplification sequencing product of the genome is obtained. By means of the method, the amplification product can be rapidly, efficiently and accurately recognized, and the calculation resources are saved; the sequence assembling process is compatible, and the problem of reduction of the quality value of basic groups produced in the sequencing process can be effectively solved; the homozygosis/heterozygosis state of variation information can be more effectively and stably judged, and random errors introduced in the PCR (polymerase chain reaction) process and the sequencing process are eliminated.
Owner:AMOY DIAGNOSTICS CO LTD +1

Encoding method and decoding method for performing information storage by means of DNA

InactiveCN105022935ACoding method is simple and easyConsider efficiencySpecial data processing applicationsDecoding methodsMagnetic media
The present invention relates to an encoding method and an decoding method for performing information storage by means of DNA. Different from a conventional computer magnetic medium, an information write-in mode of DNA storage is that after information is encoded, an oligonucleotide chain with a certain length is synthesized by utilizing an oligonucleotide chain synthesis technology and the synthesized oligonucleotide chain is stored in a powder form; and a reading technology of DNA storage is that the oligonucleotide chain is sequenced by utilizing a high-throughput sequencing technology and after being spliced, sequenced fragments are transcoded, so that an initial computer multimedia file can be restored. Due to the characteristics of the DNA oligonucleotide chain, in the design of an encoding mode, a random error possibly existing in the DNA synthesis and sequencing process can be taken into full consideration, and error authentication and multiple cover segment are performed on the DNA fragments. The encoding method for a DNA storage technology, which is constructed by the present invention, is simple, convenient and easy to operate and can be applied to transform the computer multimedia files in various formats into DNA sequences so as to perform information storage.
Owner:QINGDAO INST OF BIOENERGY & BIOPROCESS TECH CHINESE ACADEMY OF SCI

Method for fusing ocean current observation data of unmanned undersea vehicle (UUV)

InactiveCN102213594AHigh precisionOutlier smoothing correctionOpen water surveyOriginal dataLongitude
The invention provides a method for fusing ocean current observation data of an unmanned undersea vehicle (UUV), which comprises the following steps of: 1, obtaining ocean current profile data, when the UUV underwater navigates at a certain depth, obtaining an ocean current profile with a certain water layer thickness at the upper part or lower part of the UUV; 2, filtering the ocean current profile data, filtering the obtained ocean current original data, eliminating a wild value, carrying out smooth correction on a measured random error; 3, carrying out time registering on the ocean current profile data, reducing asynchronous data into synchronous data under the same time moment; and 4, reducing position information of the UUV, starting from one known coordinate position of the UUV to reduce a coordinate position of the next time according to the navigation direction, the navigation speed and the navigation time of the UUV at the coordinate position; and 5, fusing the ocean current profile data, converting longitude and latitude position information obtained from the reduction of the position information into ASCII (American Standard Code For Information Interchange) codes, and inserting into corresponding positions of an ADCP (Acoustic Doppler Current Profiler) data packet. According to the invention, accurate and complete ocean current profile information can be obtained under a geodetic coordinate system.
Owner:HARBIN ENG UNIV

Triple modular redundancy based satellite-borne comprehensive electronic system

The invention discloses a triple modular redundancy based satellite-borne comprehensive electronic system used for data processing and data storage of a pico-satellite. The triple modular redundancy based satellite-borne comprehensive electronic system comprises a data processing module, a data memory module, an interface extension module and a power supply module, wherein the data processing module is connected with the interface extension module, and is connected with the data memory module; and the output of the power supply module is respectively connected with the input of the data processing module and the input of the data memory module. The data processing module fuses the principle of triple modular redundancy, so as to have high reliability, and avoid influence due to random errors to a certain extent; the data memory module adopts a cache and main memory combined manner, so as to realize high-capacity and long-life targets of a memory module based on the low cost; and the virtue DMA (direct memory access) principle is fused between the data processing module and the interface extension module, so as to simply and effectively solve the problem that the processing capability of the data processing module is wasted because the speed of an external interface of the data processing module is faster than that of an extension interface.
Owner:ZHEJIANG UNIV

Method for calibrating fixed errors of inertial sensor in inertial navigation system in real time

The invention discloses a method for calibrating fixed errors of an inertial sensor in an inertial navigation system in real time. The method comprises the following steps of: firstly, establishing a fixed error model of the inertial sensor during the dynamic flying process of an aircraft, wherein the fixed errors include installation errors and scale factor errors; secondly, establishing a state equation and a position, speed and attitude linear measurement equation of a filter, with the fixed errors of the inertial sensor included, on the basis of a random error model of a traditional IMU (Inertial Measurement Unit) and the established fixed error model; and finally, carrying out real-time dynamic calibration and correction to the fixed errors of the inertial sensor during the dynamic flying process of the aircraft, so as to obtain the navigation result of the inertial navigation system after the fixed errors of the inertial sensor are compensated and corrected. The method can realize the calibration and correction of installation errors and scale factor errors of the inertial sensor used in the inertial navigation system during the dynamic flying process of the aircraft, effectively enhances the performance of the inertial navigation system, and is suitable for engineering application.
Owner:NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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