230 results about "Time domain response" patented technology

A stimulation strategy for cochlear implants seeks to approximate the time domain response of a patient's neural system to electrical stimuli, to the time domain response of a normal hearing person to a corresponding acoustic stimulus. The strategy is designed to induce in the neurons of a patient a time domain response to an acoustic signal which is similar to, or approximates the time domain response induced by the normal processes in a healthy person. Various implementations are disclosed.

A Deep Belief Network (DBN) feature extraction-based analogue circuit fault diagnosis method comprises the following steps: a time-domain response signal of a tested analogue circuit is acquired, where the acquired time-domain response signal is an output voltage signal of the tested analogue circuit; DBN-based feature extraction is performed on the acquired voltage signal, wherein learning rates of restricted Boltzmann machines in a DBN are optimized and acquired by virtue of a quantum-behaved particle swarm optimization (QPSO); a support vector machine (SVM)-based fault diagnosis model is constructed, wherein a penalty factor and a width factor of an SVM are optimized and acquired by virtue of the QPSO; and feature data of test data are input into the SVM-based fault diagnosis model, and a fault diagnosis result is output, where the feature data of the test data is generated by performing the DBN-based feature extraction on the test data.

Synthetic circuit elements and amplifier applications for synthetic circuit elements are provided. The synthetic circuit elements disclosed herein may be configured to compensate for some or all of the parasitic capacitance normally associated with circuit elements disposed on a substrate providing a selectable impedance characteristic. Amplifier circuit constructed using such synthetic circuit elements exhibit improved performance characteristics such as improved recovery time, frequency response, and time domain response.

The present invention provides a method of characterizing a frequency response of a transmission channel between a transceiver and a subscriber unit. The method includes once per predetermined interval of time, the transceiver transmitting a signal including multiple carriers, a plurality of the carriers including training symbols, a plurality of the carriers including information symbols. The subscriber unit generates frequency response estimates at the frequencies of the carriers including training symbols, each interval of time. The frequency response estimates are converted into a time domain response generating an impulse response once per interval of time. The impulse responses are filtered over a plurality of intervals of time. A channel profile is determined from the filtered impulse responses. The channel profile is converted to the frequency domain generating a channel interpolator. The characterized frequency response is generated from the channel interpolator and the frequency response estimates. The filtering can include averaging the impulse responses over a plurality of intervals of time, accumulating the impulse responses over a plurality of intervals of time, or weighted averaging of the impulse responses over a plurality of intervals of time. The weighted averaging can be dependent upon a phase error between the impulse responses, and/or an amplitude error between the impulse responses.

The invention provides an MIMO-OFDM system channel estimation method based on compressed sensing. The MIMO-OFDM system channel estimation method based on compressed sensing is mainly applied to channel estimation when a receiving terminal is provided with a two-dimensional antenna array. According to the MIMO-OFDM system channel estimation method based on compressed sensing, the time delay, incidence angle and gain of each path of a space channel are estimated in sequence, and channel estimation accuracy can be improved effectively. The MIMO-OFDM system channel estimation method based on compressed sensing comprises the following steps that 1, an initially-estimated value of a channel frequency domain response vector of each pilot frequency sub-carrier is obtained according to the least square criterion; 2, by means of the sparsity of the channel frequency domain response vectors in a time delay domain, the time delay of each path of the channel and an estimated value of a channel time domain response vector of each path of the channel are estimated on the basis of the compressed sensing theory; 3, by means of the sparsity of the channel time domain response vectors in a two-dimensional angle domain, the incidence angle of each path of the channel is estimated on the basis of the compressed sensing theory; 4, the gain coefficient of each path of the channel is estimated according to the least square criterion; 5, estimated values of channel frequency domain responses of all the sub-carriers and antennas are obtained.

The invention provides a vector measurement method for passive intermodulation interference. The vector measurement method for the passive intermodulation interference comprises the steps that firstly a computer module adjusts the output frequency of a frequency reference unit, and a frequency reference signal is output; the frequency reference signal is used by a first signal source, a second signal source and a local oscillator source module after power division is conducted on the frequency reference signal, and then a testing signal with a frequency F1, a testing signal with a frequency F2 and a local oscillator signal L0 are generated; a part of the testing signal F1 and a part of the testing signal F2 are amplified by an amplifier module after power division is conducted on the testing signal F1 and the testing signal F2, then the signals are combined to generate a +43dBm dual-tone signal used for testing, reciprocal mixing is conducted on the other part of the testing signal F1 and the other part of the testing signal F2 after the other part of the testing signal F1 and the other part of the testing signal F2 pass through a frequency multiplication module, the frequency of an obtained signal is 2F1-F2 after filtering, and the signal is received by a reference receiver to serve as a PIM reference signal. By the adoption of the vector measurement method for the passive intermodulation interference, self-intermodulation and self-calibration of an instrument can be achieved, vector compensation for the self-intermodulation of the instrument can be achieved, the self-intermodulation of a system is greatly reduced, the measurement range of the system is widened, and the uncertainty of measurement is reduced; the time-frequency conversion technology can be directly adopted by a measurement result, and the time domain response to a PIM product can be observed.

The invention discloses a pilot signal transmitting method in an OFDM system, which is used for carrying out frequency domain windowing processing to pilot sequences and then transmitting. The invention also discloses a channel estimation method and a noise power estimation method, comprising the following steps of: receiving pilot signals processed by frequency domain windowing, carrying out channel estimation according to pilot sequences without windowing to determine an initial value HLS-W(k) of frequency domain channel response on each subcarrier corresponding to a user, and utilizing HLS-W(k) to determine corresponding channel time domain response hW(n); calculating signal power of channel time domain response with the index value of larger than NCP-W in the channel time domain response hW(n) as noise power of the system; setting the channel time domain response valve with the index value of larger than NCP-W in the channel time domain response hW(n) to be 0, completing denoising processing of channel estimation, carrying out Fourier transformation and dewindowing processing to CIR by denoising processing and obtaining the final frequency domain channel response of each subcarrier. The invention can improve accuracy of noise power estimation and channel estimation.

The invention relates to a method for testing random vibration structure damage based on cross-correlation function peak value vector. It uses the relation between the frequency respond function of the cross-correlation function of the two points respond signal of the vibration structure and the structure out-exiting frequency spectrum to collect the respond signal of a period times of a plurality of measuring points, it dose cross-correlation function computing to one point respond signal with other points respond signals, it uses the largest peak of each cross-correlation function to construct the cross-correlation function peak value vector, it compares the relative factor of the intact structure and the current structure cross-correlation function peak value vector to quote weather the structure is damaged, it analyzes the content change of the corresponding elements to ascertain the damaged location.

The invention discloses a PID hydraulic turbine governor parameter optimization method based on multi-working-condition time domain response. The method includes the following steps that (1) a hydraulic turbine regulating system model is built, wherein the hydraulic turbine regulating system model particularly comprises a PID hydraulic turbine governor model, a hydraulic turbine-water diversion pipeline model and a generator model; (2) parameters of the hydraulic turbine regulating system model are obtained in a field test and parameter recognition mode; (3) a comprehensive fitness function based on multi-working-condition time domain response is designed, and the optimization objectives of finding out an optimum PID control parameter and enabling a comprehensive fitness function value to be minimum are determined; (4) the optimal PIC control parameter is obtained through an intelligent optimization algorithm. The control parameters obtained through the method enable a system to keep satisfying dynamic characteristics under different working conditions, and robustness of the system is enhanced.

The invention relates to an integrated surface acoustic wave (SAW) wireless temperature sensor, comprising an interdigital transducer with an EWC/SPUDT structure and 11 reflectors with short-circuit gate structures, which are manufactured on a piezoelectric substrate, wherein, the EWC/SPUDT receives an electromagnetic wave signal transmitted from a wireless reading unit by a wireless antenna and transforms the signal into surface acoustic wave which is propagated along the reflectors on the surface of the piezoelectric substrate and is respectively reflected by the reflectors, the reflected acoustic wave is retransformed into the electromagnetic wave signal by an EWC/SPUDT2, the signal is returned to the wireless reading unit by the wireless antenna, and finally temperature detection is realized by evaluation on a phase change of time-domain response via a signal processing method. In the sensor, the 11 reflectors of a SAW reflection delay line are divided into two paths for reducing multiple reflection among the reflectors, wherein, 8 reflectors on one path are used for 8-bit electronic tags, and 3 reflectors on the other path are used for temperature detection; and a reflection peak of a time domain S11 with even response is obtained by adjusting electrode number of the reflectors.

The method includes steps: transmitting end (TE) determines length value of Chu sequence as training sequence; estimating out noise power at each relay end and receiving end, and determining maximal number of nonzero tap in time domain response of channel between nodes, and determining power distribution coefficient (PDC) of each node; after determining value of length and PDC, and selecting corresponding Chu sequence and adding circular prefix (CP), TE carries out transmission at first time slot (TS); after receiving signal, each relay end carries out linear processing on the received signal based on PDC and unitary matrix, and then adds CP, and transmits them in second TS; the receiving end receives signals at first TS and second TS, and unites the received signals with CP being removed, further, carries out channel estimation (CE) by minimum mean-square value. Thus, the invention realizes CE in high precision and low complexity in cooperation comm containing multiple relay nodes.

The invention relates to an integrated surface acoustic wave wireless pressure sensor applied to a TPMS, comprising two SAW reflection delay lines which are encapsulated for integration with a JSR membrane by a nickel conducting cylinder and a conducting adhesive, and a matched network connected with a wireless antenna, wherein, the first SAW reflection delay line comprises a single-phase unidirectional energy converter for controlling electrode width, and 3 short-circuit gate reflectors applied to pressure detection; and the second SAW reflection delay line comprises 11 short-circuit gate reflectors, wherein, 8 reflector are used for 8-bit electronic tags, and the other 3 reflectors are used for temperature detection. In the sensor, an EWC/SPUDT receives an electromagnetic wave signal from a wireless reading unit by the wireless antenna and transforms the signal into an SAW signal which is propagated along the surface of a piezoelectric substrate and is respectively reflected by the reflectors, the reflected acoustic wave is retransformed into the electromagnetic wave signal by the EWC/SPUDT and is returned to the wireless reading unit by the wireless antenna, and finally temperature and pressure detection in a tire is realized at the same time by evaluation of a phase change of time-domain response via a signal processing method.

The invention provides an avionic device operating modal measuring method for vibration finite element model correction. The method includes the following steps that firstly, response test points are arranged, and piezoelectric acceleration transducers are pasted, wherein the n response test points are arranged on a circuit board, and the piezoelectric acceleration transducers are pasted on the response test points respectively; secondly, an avionic device and a test device are installed, and an operating modal test platform is built; thirdly, time domain response data of the avionic device under the random vibration condition are acquired; fourthly, data processing is conducted through modal recognition software, and operating modal parameters of the avionic device are acquired. Through the steps, an avionic device operating modal measuring system for vibration finite element model correction is established, and the overall process from generation of random vibration signals to acquisition of the time domain response data and from generation of a time domain response data sample and a cross-spectrum function to recognition of the operating modal parameters of the avionic device is finished. According to the method, online modal recognition is achieved, and test time is saved and test cost is reduced.

A method is provided for de-embedding the S-parameter response of an electrical DUT embedded in an electrical network. The method comprises making first and second S-parameter measurements in the frequency domain at a port or measurement reference plane to the network containing the DUT. For the second measurement, a known impedance condition is created at the embedded location of the DUT. The first and second measurements are transformed to the time domain, and then gated to select portions of the time-domain-transformed responses that correspond to paths that include the DUT and known impedance condition, respectively. The gated time domain responses are then transformed back into the frequency domain, yielding first and second selected S-parameter measurement responses M1 and M2, respectively. A reflection S-parameter for the DUT is then determined as a function of the first and second selected S-parameter measurement responses and the known impedance condition.

The invention relates to a surface acoustic wave (SAW) electric current sensor which comprises a piezoelectric substrate, a first line of reflectors, a second line of reflectors and a thin film layer. The piezoelectric substrate serves as a vibrating membrane, the first line of reflectors comprise the first interdigital reflector serving as a reference and the second interdigital reflector used for measuring electric currents, the second line of reflectors serve as electronic tags, and the first line of reflectors and the second line of reflectors are coated with the thin film layer. First electromagnetic wave signals sent by a reading module are received through a wireless antenna, the first electromagnetic wave signals are converted into SAWs spread along the surface of the piezoelectric substrate through an EWC/SPUDT, the SAWs are converted into second electromagnetic wave signals through the EWC/SPUDT after being reflected by the first line of reflectors and the second line of reflectors, the second electromagnetic wave signals are transmitted back to the reading unit through the wireless antenna, through a signal processing method, the current detection is carried out by obtaining the signal transformation of the time-domain response of the SAW electric current transducer.

The invention belongs to the technical field of transducers, and provides an ultrasonic transducer and a manufacturing method thereof. The ultrasonic transducer comprises a piezoelectric layer, a matching layer, a tuning layer and a backing layer. The piezoelectric layer is used for radiating ultrasonic wave signals forwards or backwards, and electrodes are plated on the two sides of the piezoelectric layer respectively. The matching layer is arranged at the front end of the piezoelectric layer and used for transmitting the ultrasonic wave signals radiated forwards. The tuning layer is arranged at the rear end of the piezoelectric layer located between the tuning layer and the matching layer. The backing layer is used for absorbing the ultrasonic wave signals radiated backwards by the piezoelectric layer and located on the side, deviating from the piezoelectric layer, of the tuning layer. Through arranging the tuning layer between the piezoelectric layer and the backing layer, the ultrasonic wave signals radiated backwards by the piezoelectric layer are effectively utilized, it is avoided that part of the ultrasonic wave signals enter the backing layer to be attenuated in a heat energy mode, meanwhile, the tuning layer is used for tuning pulse reverb of an ultrasonic probe, and therefore the time-domain response and frequency-domain response of the ultrasonic transducer are improved to a certain degree.

A method for calculating vehicle interior noise comprises steps as follows: finite element models of a vehicle frame, a transmission shaft and a rear axle of an automobile are established respectively, and benchmarking is performed between the finite element models and corresponding actually measured modes; modal calculation is performed on the finite element models of the vehicle frame, the transmission shaft and the rear axle after benchmarking, and modal calculation results are imported into a pure rigid multi-body model of a vehicle for establishment of a rigid-flexible coupled model; the rigid-flexible coupled model is subjected to time-domain response analysis, so that loads at connecting points during engine mounting are acquired; a transfer function from each connecting point to a target position in the vehicle is acquired; the noise pressure level from each connecting point to the target position is calculated according to the load of the corresponding connecting point and the corresponding transfer function. The accurate load data of each connecting point is extracted through the rigid-flexible coupled model of the vehicle, and the accurate noise pressure level in the vehicle is acquired in real time in the time domain of each connecting point during engine mounting in combination with the corresponding transfer function.

A method for obtaining time domain response of channel includes carrying out filter set treatment on channel frequency domain response corresponding to symbol of orthogonal frequency division multiplexing to obtain corresponding channel time domain response, setting resolution ratio of channel time domain response to be greater than time resolution ratio of channel time domain response obtained by using channel frequency domain as IFFT transform and regulating position of fast Fourier transform window according to said channel time domain response.

An equivalent time sampling system employs two clock frequency sources, phase locked, wherein an analog to digital converter sampling clock is derived from one source and a pulse generator clock is derived from the other. Choice of the clock frequencies determines minimum time step and the set of available time steps, and pulse repetition period determines the time step size, for equivalent time sampling. The system is suitably implemented in a time domain reflectometer, optical time domain reflectometry system, or other systems for obtaining time domain responses to a periodic stimulus of a system under test, with stimulus rate and the sampling intervals varying over a wide range.

The invention discloses a transient electromagnetic forward modeling method applicable to an irregular transmitting loop. The method comprises the steps of using a ground point corresponding to the center of a receiving coil as an original point, building a cylindrical-coordinate system, and building a frequency domain expression of the vortex electric field component at a receiving point; presenting the frequency domain expression of the vortex electric field component as a Hankel integral form, and working out the response magnitude of the frequency domain of the vortex electric field component; working out the response magnitude of the time domain of the vortex electric field component; recording coordinates of inflection points of the irregular transmitting loop, and obtaining a function expression of a segmented loop between every two adjacent inflection points; conducting integration on the segmented loops by using time domain response of the vortex electric field component so as to obtain the voltage value of each segmented loop, and calculating the sum of the voltage values of all the segmented loops so as to obtain transient response of the irregular transmitting loop. The method is applicable to a ground, ocean and aviation transient electromagnetic method one-dimensional forward modeling algorithm of the irregular transmitting loop.

The invention discloses a method for testing fault modes of an integrated switching current circuit. The method includes the following steps: S1, establishing a switching current test circuit, and applying an excitation signal to the test circuit, S2, defining the fault modes of the switching current circuit, S3, collecting testable node time-domain response signals of the switching current circuit, S4, preprocessing time-domain response data, calculating fault characteristic parameters of the signals, extracting information entropy and kurtosis of the signals, and calculating a fuzzy set of the information entropy, and S5, constructing a neural network classifier according to the information entropy and the kurtosis, and acquiring the fault modes of the switching current test circuit. The method for testing the fault modes of the integrated switching current circuit is suitable for tests on a large-scale and complicated integrated switching current circuit with a large number of fault categories and is high in accuracy rate of fault diagnosis.