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68 results about "Time-invariant system" patented technology

A time-invariant (TIV) system has a time-dependent system function that is not a direct function of time. Such systems are regarded as a class of systems in the field of system analysis. The time-dependent system function is a function of the time-dependent input function. If this function depends only indirectly on the time-domain (via the input function, for example), then that is a system that would be considered time-invariant.

FEXT determination system

Operational data is utilized to determine the FEXT interference induced by one line into the other DSL line. FEXT interference can be calculated using the NEXT interference measured between the two lines at the upstream ends of the loops and the downstream channel transfer function of one of the loops. Because the NEXT and transfer function constitute a linear time-invariant system, as does the FEXT interference between the lines, the NEXT interference and line transfer function can be multiplied (if in linear format) or added (if in logarithmic format) to approximate the FEXT interference between the lines. The collection of data, calculations and other functions performed in these techniques may be performed by a system controller, such as a DSL optimizer. An Xlog(u,n) quantity is a decibel-magnitude representation of the insertion-loss equivalent of FEXT transfer functions and is defined as the ratio of (1) a line u's source power into a matched load of 100 Ohms when no binder is present to (2) the power at the output of the subject line when line u is excited with the same source and the binder is present. Xlin(u,n) is the linear equivalent of Xlog(u,n). The Xlog(u,n) and Xlin(u,n) quantities may be represented in specific formats that assist in their use in DSL and other systems. When defined as a line's insertion loss, Xlin (or equivalently Xlog) does not include the effect of any transmit filter.
Owner:ASSIA SPE LLC CO THE CORP TRUST CO

FEXT determination system

Operational data is utilized to determine the FEXT interference induced by one line into the other DSL line. FEXT interference can be calculated using the NEXT interference measured between the two lines at the upstream ends of the loops and the downstream channel transfer function of one of the loops. Because the NEXT and transfer function constitute a linear time-invariant system, as does the FEXT interference between the lines, the NEXT interference and line transfer function can be multiplied (if in linear format) or added (if in logarithmic format) to approximate the FEXT interference between the lines. The collection of data, calculations and other functions performed in these techniques may be performed by a system controller, such as a DSL optimizer. An Xlog(u,n) quantity is a decibel-magnitude representation of the insertion-loss equivalent of FEXT transfer functions and is defined as the ratio of (1) a line u's source power into a matched load of 100 Ohms when no binder is present to (2) the power at the output of the subject line when line u is excited with the same source and the binder is present. Xlin(u,n) is the linear equivalent of Xlog(u,n). The Xlog(u,n) and Xlin(u,n) quantities may be represented in specific formats that assist in their use in DSL and other systems. When defined as a line's insertion loss, Xlin (or equivalently Xlog) does not include the effect of any transmit filter.
Owner:ASSIA SPE LLC CO THE CORP TRUST CO

Fault detectable degree analytical method for unmanned aerial vehicle flight control system

The invention relates to a fault detectable degree analytical method for an unmanned aerial vehicle flight control system. Unmanned aerial vehicle fault detection algorithm design and sensor configuration need to quantitatively analyze the difficulty level of fault detection. An unmanned aerial vehicle flight control system model is established according to an unmanned aerial vehicle closed loop nonlinearity flight control system and fault types; the flight process is segmented according to different flight states of an unmanned aerial vehicle, and small perturbation linearized models are established at all periods; faults and derivatives of the faults serve as extension states, and a dimension expansion piecewise linear time-invariant system model is established; a state observable degree index based on singular value decomposition serves as a quantitative evaluation index of fault detectable degree, according to the quantitative evaluation index, the difference of detectable degrees of the faults of the unmanned aerial vehicle in different flight states is quantitatively analyzed from the fault estimation view, and a reference basis is provided for the fault detection algorithm design and unmanned aerial vehicle sensor configuration.
Owner:SHANDONG UNIV OF SCI & TECH

Linear time-varying structure modal shape identification method

The invention discloses a linear time-varying structure modal shape identification method, and belongs to the technical field of structural dynamics. On the condition that the linear time-varying structure model frequency and model damping are known, a parameterized model describing a time correlation time division form of a linear time-varying structure is built; a time orthogonal polynomial basefunction is introduced, the parameterized model is unfolded on the basis of the base function, and a time correlation power spectrum defined in the description is decomposed in a time-invariant system in the traditional frequency domain; the linear time-varying structure-based time correlation power spectrum is unfolded, and a parameter estimation method is adopted for solving the linear time-varying structure modal shape. The technical purpose of providing the method for integrally estimating the linear time-varying structure modal shape in the whole time within the time-frequency domain isachieved; in addition, the integrity of the model shape on a time shaft is improved, the identification effect is improved by assigning a bandwidth mode, multiple experiments can be conducted, a random error is reduced by taking the average value, and the identification capacity of the low-order model shape is improved.
Owner:BEIJING INSTITUTE OF TECHNOLOGYGY

FEXT determination system

Operational data is utilized to determine the FEXT interference induced by one line into the other DSL line. FEXT interference can be calculated using the NEXT interference measured between the two lines at the upstream ends of the loops and the downstream channel transfer function of one of the loops. Because the NEXT and transfer function constitute a linear time-invariant system, as does the FEXT interference between the lines, the NEXT interference and line transfer function can be multiplied (if in linear format) or added (if in logarithmic format) to approximate the FEXT interference between the lines. The collection of data, calculations and other functions performed in these techniques may be performed by a system controller, such as a DSL optimizer. An Xlog(u,n) quantity is a decibel-magnitude representation of the insertionloss equivalent of FEXT transfer functions and is defined as the ratio of (1) a line u's source power into a matched load of 100 Ohms when no binder is present to (2) the power at the output of the subject line when line u is excited with the same source and the binder is present. Xlin(u, n) is the linear equivalent of Xlog(u, n). The Xlog(u, n) and Xlin(u,n) quantities may be represented in specific formats that assist in their use in DSL and other systems. When defined as a line's insertion loss, Xlin (or equivalently Xlog) does not include the effect of any transmit filter.
Owner:ADAPTIVE SPECTRUM & SIGNAL

Method for Determining an Averaged Frequency-Dependent Transmission Function for a Disturbed Linear Time-Invariant System, Evaluation Device and Computer Program Product

The invention relates to a process for determining an averaged frequency-dependent transfer function for a perturbed linear time-invariant system by means of an evaluation device, wherein the process comprises providing frequency-dependent reference signals derived from excitations input in a linear time-invariant system, providing frequency-dependent measuring signals for the linear time-invariant system associated with the frequency-dependent reference signals, and determining an averaged frequency-dependent transfer function for the linear time-invariant system, in that, using signal deconvolution of mutually associated measuring and reference signals, frequency-dependent transfer functions are determined and the frequency-dependent transfer functions are averaged, and wherein during determination of the averaged frequency-dependent transfer function at least a part of the determined frequency-dependent transfer functions is included in the averaging corresponding to a respectively associated frequency-dependent weighting. Furthermore the invention comprises an evaluation device for determining an averaged frequency-dependent transfer function for a perturbed linear time-invariant system and a computer program product.
Owner:SDA SOFTWARE DESIGN AHNERT

Retransmission times dynamic adjustment method based on real-time packet loss information triggering

The invention provides a retransmission times dynamic adjustment method based on real-time packet loss information triggering. The method comprises the steps of collecting a system state of a discretelinear time invariant system, carrying out Kalman filtering on the system state and then transmitting the system state to a remote estimator; on the basis of the feature that a remote state estimation error covariance is converged or sharply enlarged according to whether a data packet arrives or is lost, designing a retransmission demand degree index, and automatically selecting a change functionof the index, thereby adjusting increase and decrease amplitude of the index; designing retransmission times increase and decrease triggering thresholds for the discontinuously changing demand degreeindex; and in a transmission process, when the demand degree index reaches the increase and decrease triggering thresholds, increasing and decreasing the retransmission times, and updating the transmission times for next-time data transmission. According to the algorithm provided by the invention, under the same energy consumption, compared with a retransmission times equal distribution algorithm, the retransmission times dynamic adjustment algorithm has the advantage that the remote estimation performance can be optimized well.
Owner:SOUTHEAST UNIV

Dimmable differential equation solver based on interference couplers and silica-based micro-ring resonant cavity

InactiveCN104375354AUniversalThe coefficient can be adjustedNon-linear opticsWaveguideConstant coefficients
Provided is a dimmable differential equation solver based on interference couplers and a silica-based micro-ring resonant cavity in the field of multi-light-path multiplexing systems. A to-be-processed-signal generating module generates a light signal to be processed, and the light signal to be processed is input from the input end of a dimmable differential equation solving module; an output signal obtained by solving the dimmable differential equation solving module is output from the output end to a signal observation and analysis module to be displayed and observed. The dimmable differential equation solving module comprises the silica-based micro-ring resonant cavity, and micro-rings of the silica-based micro-ring resonant cavity are coupled with direct waveguides at a transmission end and a reflection end to form two interference couplers. The equivalent coupling strength between the micro-rings and the direct waveguides by changing outer arm phase shifts of the two interference couplers, and therefore dynamic adjustment on coefficients of constant-coefficient differential equations to be solved can be achieved. The dimmable differential equation solver is applied to simulation and analysis of linear time invariant systems and provides a solution for solving linear constant-coefficient differential equations of general types.
Owner:SHANGHAI JIAO TONG UNIV

Intermittent fault detection method of linear discrete time-delay system

The invention relates to an intermittent fault detection method of a linear discrete time-delay system. The intermittent fault detection method comprises the steps that virtual input and virtual output are introduced according to the characteristics of the linear discrete time-delay system, a linear dimensionless discrete time-delay system is constructed, and the linear dimensionless discrete time-delay system is transformed into a linear dimensionless discrete time-invariant system by using a lifting method; on the basis of designing a state observer, truncated residual is constructed by introducing a sliding time window, and the statistical characteristics of the truncated residual are analyzed; and two hypothesis tests are used for setting detection thresholds of the intermittent faultoccurrence moment and vanishing moment respectively, amplitude of an intermittent fault is estimated, and the detectability problem of the intermittent fault is analyzed. The intermittent fault detection method of the linear discrete time-delay system is based on the lifting method and the designed state observer, the new truncated residual is designed by introducing the sliding window, the intermittent fault detection process can be quantitatively described, intermittent fault detection can be timely and effectively detected, the fault detection rate is increased, and the fault false alarm rate and missing report rate are decreased.
Owner:CHINA UNIV OF PETROLEUM (EAST CHINA) +1

Cabin structure vibration response reproduction method

The invention discloses a cabin structure vibration response reproduction method, and belongs to the technical field of cabin structure vibration and noise reduction. The method comprises the following steps of firstly, assuming that the impact response between a measured vibration exciter or actuator and each receiving position is a linear time-invariant system, based on the hypothetical, measuring the impulse responses of the plurality of vibration exciters and the receiving positions by using a linear sweep method; after the impulse response is obtained, taking the collected data of the multiple vibration sensors installed on the surface of the structural wall as the input, and through a deconvolution model matched with the acceleration, solving the driving signals of all the vibrationexciters during vibration reproduction. According to the method, the plurality of excitation devices are arranged outside the structure to equivalently reproduce the structural vibration condition ofa sound field of the original cabin so as to better reproduce the original sound field. According to the theory of vibration and sound radiation, in a low-frequency range, the method can accurately reproduce the vibration distribution of the sound field of the original cabin.
Owner:NORTHWESTERN POLYTECHNICAL UNIV
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