333 results about "Parameter error" patented technology

A method for controlling a photolithography process includes providing a wafer having a first grating structure and a second grating structure overlying the first grating structure; illuminating at least a portion of the first and second grating structures with a light source; measuring light reflected from the illuminated portion of the first and second grating structures to generate a reflection profile; determining an overlay error between the first and second grating structures based on the reflection profile; and determining at least one parameter of an operating recipe for a photolithography stepper based on the determined overlay error. A processing line includes a photolithography stepper, a first metrology tool, and a controller. The photolithography stepper is adapted to process wafers in accordance with an operating recipe. The first metrology tool is adapted to receive a wafer having a first grating structure and a second grating structure overlying the first grating structure. The metrology tool includes a light source, a detector, and a data processing unit. The light source is adapted to illuminate at least a portion of the first and second grating structures. The detector is adapted to measure light reflected from the illuminated portion of the first and second grating structures to generate a reflection profile. The data processing unit is adapted to determine an overlay error between the first and second grating structures based on the reflection profile. The controller is adapted to determine at least one parameter of the operating recipe of the photolithography stepper based on the determined overlay error.

The invention discloses a current-magnitude-based open-circuit failure online-diagnosis method for a power tube of an inverter, belongs to the field of motor control, and aims to solve the problem of poor robustness of a current-magnitude-based open-circuit failure diagnosis technology for the power tube of the inverter. The method comprises the following steps of establishing a current observer model of a permanent magnet synchronous motor driving system in a failure-free state, comparing an observed current value with detection current to obtain a three-phase current residual, converting the three-phase current residual to a two-phase coordinate system in a coordinate conversion way to obtain a current residual vector, standardizing the current residual vector, and diagnosing and positioning an open-circuit failure of the power tube of the inverter according to the amplitude and the phase of the standardized current residual vector. The current-magnitude-based open-circuit failure online-diagnosis method for the power tube of the inverter is free of influence of a system closed-loop control algorithm and insensitive to loads, and has higher robustness to parameter errors, measurement errors, system disturbance and the like.

The invention discloses an industrial robot calibration method based on distance error models. The method comprises: establishing a robot MDH (modified Denavit-Hartenberg) kinematic model; subjecting the errors of a matrix to homogeneous transformation; establishing a robot distance error calibration model; measuring the end actual pose of a robot; calibrating geometrical parameter errors of every connecting rod of the robot; and performing experimental verification. The industrial robot calibration method based on the distance error models has the advantages of being simple, practical, high-efficiency and rapid, is applicable to any series articulated robots, has a strong commonality, and can improve the positioning accuracy and the distance accuracy of an industrial robot simultaneously.

The invention relates to a time-domain ground-air electromagnetic detection system and a calibration method, in particular to a system consisting of an induction signal recording device connected with a ground recording device global position system (GPS) synchronization unit, a closed abnormal ring and a data quality evaluation system, and a calibration method for the time-domain ground-air electromagnetic detection system. The closed abnormal ring and the induction signal recording device are adopted, the induction current and induction voltage are simultaneously recorded, and the 24-bit 200Hz sampling rate, a bandwidth of 0-13KHz and a dynamic range of an amplifier of 160dB are achieved. Moreover, the system is synchronous with a ground transmitter and an air receiver GPS, and during measurement, by removing earth background field data, a pure closed abnormal ring electromagnetic signal containing a geometric error is extracted, is input into the data quality evaluation system, andis compared and fitted with the computed closed abnormal ring theoretical value, the system error, the geometric parameter error and the detection resolution of the time-domain ground-air electromagnetic detection system are determined, and the performance of the electromagnetic detection system is tested and calibrated.

In processing an external function for which source code is not available, such as an application program interface (API), a model is used to evaluate whether the external function is properly invoked. An error potentially resulting from improper invocation of the external function and at least one condition that will result in the potential error are identified. The model is created to test for the condition that will result in the potential error. When the condition is found, generation of an error message is triggered. The model is associated with a source code analyzer such that when the source code is analyzed by the source code analyzer, the model is applied to evaluate invocation of the external function. The potential error and conditions that result in the error, such as input/output parameter errors and dependency errors, may be derived from documentation describing the operation of the external function or API.

The invention relates to an industrial robot kinematics calibration system. The industrial robot kinematics calibration system comprises a measuring device arranged at the tail end of a robot and further comprises a calibration device and a data processing device which are arranged in the robot work space. According to the device, cost is reduced, carrying and using are convenient, and the devicecan be applied to online rapid calibration of a robot on the work site. A measuring coordinate system is established on the measuring device, and the robot is calibrated; and through a method, calibration of robot body geometric parameter errors, and the conversion relation among a robot coordinate system, the measuring coordinate system and a calibration coordinate system can be achieved at the same time.

The invention relates to a printed circuit board (PCB) virtual manufacturing system of the electronic design automation (EDA) of the electronic product and a realization method thereof. The realization method comprises the following steps: all types of EDA design files can be extracted and converted to an EDA simulation file with the same format and data are input in a database; the PCB static (three-dimensional) 3D simulation and assembly 3D simulation are performed under the VC++ 6.0 environment; and finally PCB manufacturability analysis is performed to extract the simulation information and the judgement parameters of each element, the judgement parameters of each element are detected one by one according to the manufacturability design criteria in a rule database, and the PCB physical parameter error and assembly error of the EDA of the electronic product are displayed and filed instantly. By adopting the method of the invention, the relationship between the PCB design and the manufacture of the isolated island can be built and the visual basis can be provided for the data modification of the EDA optimal deign in the shortest time, thus the aim of optimizing the development cycle and the cost and maximizing the production efficiency can be achieved.

The invention discloses an online calibrating method of a ship-based rotary strapdown inertial navigation system. The method comprises the following steps: establishing an inertial component output error model and an inertial navigation system error equation, and researching the calibration of inertial component parameter errors and determining the quantity of state and the quantity of measuration; determining the position and weight of a cubature point according to dimension of the quantity of state, deducing a state equation and a one-step state prediction and state prediction covariance matrix related to the cubature point, and introducing a multiple time-varying fading factor modified state prediction covariance matrix; and deducing a measuring equation related to the cubature point and the fading factors, a self-correlated covariance matrix, a cross-correlated covariance matrix, a gain matrix, a state estimated value and a state error covariance estimated value, and designing a strong tracking volume Kalman filtering method with strong tracking performance and strong robustness. The method disclosed by the invention estimates the inertial component parameter errors by a filtering algorithm and carries out online calibration and compensates the inertial component parameter errors, so that the navigation precision is effectively improved. The method has strong parameter-varying robustness.

The invention discloses a PCB simulation system with error detection function and the realization method. The simulation system comprises an information extraction module, an error detection module, a simulation module, an error output module and a rule base. The realization method of the system comprises: reading in an EDA design document, extracting simulation information and the discriminant parameter of each element; gradually detecting the discriminant parameter of each element one by one according to the manufacturability design norm in a self built rule base, and leading error messages to be registered; displaying physical parameter error before posting simulation; carrying out real-time alarming for assembling error during simulation process; keeping all the error information in the archives after the simulation. The method can carry out detection and real-time hint for errors on a PCB design board during simulation process or output a complete detection report after simulation is finished, thereby providing amending advice for a designer and basis for amending design in shortest time.

The invention discloses a modulation type identification method based on sparse stack self-coding. The method comprises the following steps: step 1, processing down-converted signals to obtain baseband signals of modulation signals; step 2, performing one-dimensional vectorization and normalization on the baseband signals; step 3, reforming a self-coder to obtain a sparse self-coder, and then constructing a stack sparse self-coder network using the reformed sparse self-coder to extract signal features; introducing a soft max regression model, and taking the signal features extracted by the stack sparse self-coder network as an input; step 4, training the stack sparse self-coder network; and step 5, judging whether the adjustment of network parameters meets the requirement, if so, ending the training, otherwise, repeating step 4 to continuously train the network. The method does not need to artificially extract signal feature parameters, thereby solving the problem of large parameter error in artificial extraction; and the method has good modulation type identification performance in a network having low signal-to-noise ratio and excellent anti-noise performance.

A method and corresponding apparatus for diagnosing problems on a time division multiple access (TDMA) optical distribution network (ODN) is provided. An example method may include: (i) measuring no-input signal power level on a communications path configured to carry upstream communications between multiple optical network terminals (ONTs) and an optical line terminal (OLT) in a passive optical network (PON) at a time no upstream communications are on the communications path from the ONTs to the OLT; (ii) comparing the measured no-input signal power level to a threshold; and (iii) generating a notification in an event the threshold is exceeded. Through the use of this method, faults in optical transmitters, such as bad solder joints, can be determined. Such faults may cause errors in parameters, such as ranging or normalization parameters, associated with communications. By determining the faults, the time required to resolve communications errors can be reduced.

The invention provides an MEMS pedestrian navigation method based on ZIHR heading angle correction algorithm. The method includes: 1. conducting initial alignment on an MEMS pedestrian navigation system with an accelerometer and a magnetometer at a static moment; 2. working out an inertial navigation calculation equation and an error equation of the MEMS pedestrian navigation system; 3. conductingzero velocity state detection with the output values of a gyroscope and the accelerometer; 4. working out the relationship between the heading angle difference of adjacent moments under a zero velocity state, gyroscopic drift and a heading error angle in ZIHR (zero integrated heading rate) correction algorithm; and 5. establishing a simplified MEMS pedestrian navigation UKF filter model, and performing UKF filtering. The method provided by the invention maximumly utilizes the information of static moment, has uncomplicated calculation amount, and can well inhibit the divergence of the headingerror angle. Use of the UKF filter for real-time feedback correction at a zero velocity moment can well inhibit the problem of navigation parameter error divergence after long-time operation of a low-precision MEMS sensor, and improve the positioning precision of a pedestrian navigation system.

The invention discloses a brushless direct current motor electromagnetic torque observation method based on a self-adapting slip-form observer, belonging to the control field of permanent magnet motors. The observation method comprises the following steps of: constructing a state space equation of a brushless direct current motor in an alpha-beta coordinate system based on easily-observing signals, such as motor rotating speed, each phase current of a stator, each ground voltage of the stator, rotor position, and the like; observing a counter emf (Electromotive Force) of the brushless direct current motor in the alpha-beta coordinate system in real time by using the slip-form observer; meanwhile online identifying a stator resistance parameter of the brushless direct current motor to eliminate the influence of a resistance parameter error on counter emf observation; and finally calculating the electromagnetic torque of the brushless direct current motor in real time according to the counter emf, the current and the rotating speed. In the invention, when the stator resistance parameter is unknown or a stator resistance changes due to the influences of temperature and skin effect, the counter emf and the electromagnetic torque of the brushless direct current motor can be accurately observed, the problem of the traditional method influenced by the resistance parameter is solved, and an accurate torque feedback value can be provided for the torque close loop control of the brushless direct current motor.

The invention relates to a robot self-calibration method based on plane constraint and vision-assisted positioning. The robot self-calibration method based on plane constraint and vision-assisted positioning is used for obtaining real connection rod parameters of a robot. Firstly, a robot kinematic model combining a D-H method and a MD-H method is established; secondly, a robot terminal position error model is established; thirdly, a robot connection rod parameter error model based on plane constraint is established; fourthly, images, of a constraint plane, in a left camera and a right camera are obtained through binocular vision, target point information in each image is extracted, the three-dimensional position information of the constraint plane under a basic coordinate system of the robot is positioned through three-dimensional matching; the position information is input into a robot control system, and the robot is driven to measure the constraint plane; and finally the measured data are substitute into the plane constraint error model, the real geometric connection rod parameters of the robot are recognized, and after correction, measurement of the constraint plane and recognition are repeatedly conducted until a precision requirement is met. The robot self-calibration method based on plane constraint and vision-assisted positioning has the advantages of being low in cost and high in precision and efficiency.

The present invention provides an application data processing method of a spaceborne microwave radiometer. According to the application processing method, by inputting the global or regional profile data and the radiation brightness-temperature values in a matrix, adopting a wavelet neural network algorithm to train the data, and comparing the outputted atmosphere humiture profile and ground/sea surface parameters with the preset threshold indexes, the back propagation of the atmosphere humiture profile and ground/sea surface parameter errors is implemented; by correcting each layer of weights in an error gradient descent manner, the work of utilizing a data set to correct the inversion parameters locally is realized, the local correction capabilities of the equipment developers and users to the inversion software parameters are improved, and further the detection and inversion precision is improved further.

The invention provides a Stokes polarization meter error calibration and compensation method based on a wave plate rotating method. The Stokes polarization meter error calibration and compensation method includes the specific steps that horizontal line polarization light generated by a PSG is used as standard reference light; the standard reference light is measured through a to-be-calibrated Stokes polarization meter N times to obtain N light intensity values; Fourier analysis is carried out on the obtained N light intensity values to obtain corresponding Fourier coefficients; the fast axis azimuth angle error and the phase delay amount error of a quarter-wave plate are calculated through the relation between device parameter errors and the Fourier coefficients according to the Fourier coefficients; error compensation is carried out on the Stokes polarization meter through the relation between Stokes parameters and the parameter errors according to the two parameter errors of the quarter-wave plate. The Stokes polarization meter error calibration and compensation method is easy to operate, high in feasibility and high in calibration accuracy.

The present invention provides a variable speed constant frequency doubly-fed wind power generation system, characterized in that the system includes a stator grid connected device, a motor, a controlling plate, a dual pwm converter, a code disc; the stator of the motor is connected with the power network by the stator grid connected device; the rotor of the motor is connected with the power network by the dual pwm converter; the controlling plate is connected with the power network, the motor, the dual pwm converter and the stator grid connected device; the controlling plate is also connected with the rotor via the code disc. The system eliminates some influence caused by some parameter error of the generating system according to designing a voltage amplitude compensator and a rotor position angle compensator in the controlling plate.

The invention discloses a mechanical arm kinematics parameter calibration method based on measuring of a laser tracker, and belongs to the field of industrial mechanical arm kinematics, and relates to the mechanical arm kinematics parameter calibration method based on measuring of the laser tracker. The method is based on the mechanical arm joint construction. An improved DH parameter method is adopted for building a mechanical arm kinematics model, a kinematics modeling result is used for building a mechanical arm kinematics parameter error calibration model, in consideration with the mechanical arm three-dimensional space work range, the laser tracker is adopted for measuring N absolute position coordinates of the tail end of the mechanical arm, on the basis of the kinematics parameter error calibration model, through repeated iteration, the mechanical arm kinematics parameter error is solved, a corrected kinematics parameter is input into a mechanical arm controller, and offline calibration of the mechanical arm is achieved; the mechanical arm tail end position measuring method is high in robustness, high in speed, and high in process automation degree, the adopted error solving method is high in speed, high in precision and simple in process, and the high-precision rapid calibration of joint type mechanical arm kinematics parameters can be achieved.

The invention discloses an aspheric surface parameter error interference measuring method combining laser differential confocal positioning and belongs to the field of aspheric surface measurement. Animplementation method comprises the following steps: acquiring nominal parameters of a measured aspheric surface, and by utilizing the acquired nominal parameters of the measured aspheric surface andcombining optical design software, designing and processing a part-compensating lens and aplanatic lenses; according to the part-compensating lens and the aplanatic lenses, establishing an aspheric surface parameter error interference measuring system combining the laser differential confocal positioning; obtaining an optimal compensation position change by utilizing the system; measuring a surface figure change between the measured aspheric surface and an ideal aspheric surface, and calculating a coefficient of a quartic component of the surface figure change; and according to a simultaneousequation set, calculating a surface figure parameter error of the aspheric surface, thus measurement on the surface figure parameter error of the aspheric surface is realized. The method disclosed bythe invention can improve accuracy of measurement on the surface figure parameter error of the aspheric surface, realizes non-contact, full-aperture, fast and high-accuracy measurement and has the advantages of no scanning device and simple structure.

One or more modules configured to cause a network diagnostic component to perform the following: an act of selecting first specific sampling parameters at which the SERDES is to receive network traffic; an act of determining a number of errors included in a signal output by the SERDES at the selected first specific sampling parameters; an act of repeating for a specified number of the remaining sampling parameters the acts of selecting specific sampling parameters and determining the number of errors in a signal output by the SERDES at the selected specific sampling parameter; an act of recording the number of errors for each selected specific sampling parameter in an output record, and an act of applying an optimization solution on the output record to thereby determine the specific sampling parameters that will cause the SERDES to output a signal with the lowest value of errors.

The invention belongs to the technical field of information measurement, and discloses a robot kinematics parameter calibration method based on a laser range finder. The method comprises the followingsteps that the laser range finder is connected to a to-be-calibrated robot, and a test flat plate is placed in the working space of the robot; (2) a mapping relation between a robot tail end coordinate system and a base coordinate system of the roboy and the mapping relation between a laser range finder coordinate system and the robot tail end coordinate system of the robot are determined; (3) ajoint angle value corresponding to each time of movement of the robot and a reading value of the laser range finder are gathered; (4) a plurality of points are obtained, and a kinematic parameter error is determined according to a coplane condition; and (5) compensation calibration is carried out on the kinematics parameters of the robot, the kinematics parameter error is acquired again after thecalibration is completed, the kinematics parameter error is compared with the value of the last time, and then calibration completion or re-calibration is determined. According to the method, the measuring efficiency is high, the operation is simple, the implementation is easy, and the accuracy is high.

The invention discloses a robot positioning error graded compensation method. The method includes: calculating terminal pose errors before compensation; building a kinematic model and a kinematic error model; calculating the optimal solution of each kinematic parameter error, the corrected kinematic model and the terminal pose under the corrected kinematic model; calculating input compensation quantity after positioning error compensation; calculating actual arrival pose to obtain residual errors after parameter calibration; building a residual error estimation model, and performing expected target point compensation; predicting positioning errors; acquiring predicted target point residual errors; calculating input compensation quantity; calculating terminal actual arrival pose to completethe compensation. By the method, industrial absolute positioning precision can be increased effectively, and the anisotropy of positioning errors in the space can be shown by using the residual errormodel based on space similarity.