Patents
Literature
Patsnap Copilot is an intelligent assistant for R&D personnel, combined with Patent DNA, to facilitate innovative research.
Patsnap Copilot

60results about How to "Improve position estimation accuracy" patented technology

Multi-target DOA estimation method and underwater sound vertical vector array system

ActiveCN109283492ARealize a full range of estimatesImprove position estimation accuracyPosition fixationWeighted spaceFrequency spectrum
The invention relates to a multi-target DOA estimation method and an underwater sound vertical vector array system; the method comprises the following steps: receiving a multi-target signal based on the vertical vector hydrophone array; converting the received multi-target signal to obtain a frequency spectrum and a power spectrum, and extracting a line spectrum; using a vector regular correlationalgorithm to estimate a target sound source number; using a vector weighted space smooth algorithm to obtain a MUSIC space spectrum according to the extracted line spectrum; carrying out two dimensional searching decision for a space spectrum peak corresponding to the multi-target according to the estimation result of the target sound source number and the MUSIC space spectrum, and respectively obtaining a multi-target horizontal angle and a pitching angle; step6, integrating the horizontal angles and pitching angles calculated for each line spectrum, thus obtaining the multi-target DOA estimation result. The method uses the three-dimensional vertical vector hydrophone array to realize all-dimensional estimation of the target signal horizontal angle and pitching angle, thus improving theDOA estimation accuracy of the coherent multi-target signal.
Owner:THE THIRD RES INST OF CHINA ELECTRONICS TECH GRP CORP

Doppler frequency deviation correction method and system

The invention relates to a Doppler frequency deviation correction method. The method comprises performing characteristic analysis on target radiation noise; building a receiving model and establishing a rectangular coordinate system for a towed line array; presetting the frequency point compensation total; performing Fast Fourier Transformation (FFT) and frequency domain beam forming on signals at certain initial moment and after the towed line array moves for certain time, and accumulating output results of frequency domain beam forming at the current frequency point; calculating a space moving compensation and a time delay compensation to obtain the total phase correction compensation, and obtaining the virtual array expansion output result according to the previous compensation result and the total phase correction compensation; obtaining a time azimuth course diagram, detecting the target signals through the time azimuth course diagram, determining if current frequency point compensation times reach the frequency point compensation total, changing the amplitude of the current frequency point if the compensation times do not reach the frequency point compensation total, and performing sampling again till the current frequency point compensation times reach the frequency point compensation total.
Owner:INST OF ACOUSTICS CHINESE ACAD OF SCI

Approach section flight technology error estimation method based on multi-source information fusion

The invention provides an approach section flight technology error estimation method based on multi-source information fusion. According to the method, the measurement information of main navigation sources of an aircraft in a current approach section is acquired, wherein the main navigation sources includes an inertial navigation system, a satellite navigation system and an instrument landing system; time registration and space registration are performed on the acquired measurement information; information fusion is carried out by taking federated filtering as a framework, different filteringmethods are selected according to the characteristics of the different navigation sources, and position information with relatively high accuracy is obtained; sensor fault detection is carried out, isolation processing is carried out on fault signals, and the integrity of signals is guaranteed; and finally, vector calculation is conducted on the due flight path of the aircraft and the position information of the aircraft obtained through filtering according to the position information of the aircraft, so that a flight technology error estimation value is obtained. With the method of the invention adopted, flight technology error real-time estimation can be realized; the precision of an estimation result is higher, and the precise approaching operation of the aircraft can be ensured.
Owner:NORTHWESTERN POLYTECHNICAL UNIV

Compensation method for position estimation of permanent magnet linear motor rotor by high-frequency injection method

ActiveCN111371362AImprove position estimation accuracyAccurate Compensation for Position Estimation ErrorsAC motor controlVector control systemsElectric machineRegulator
The invention discloses a compensation method for position estimation of a rotor of a permanent magnet linear motor by a high-frequency injection method, which comprises the following steps of: filtering a current response signal to obtain a first current signal and a second current signal, and designing a first compensation vector and a second compensation vector according to included position estimation error information; multiplying the first compensation vector by the first current signal and the second current signal respectively to obtain a first current vector and a second current vector; carrying out low-pass filtering on the second current vector, subtracting the second current vector from the first current vector, and multiplying the second current vector by the second compensation vector to obtain a second current difference vector; sending the imaginary part of the second current difference vector to a PI regulator for integration to obtain a mover estimation position; andtaking the mover angular frequency estimated value and the mover position estimated value as feedback signals, and controlling the difference between the actual position of the motor mover and the mover estimated position to converge to zero, so that the motor operates stably. The method can obviously inhibit the position estimation error caused by the end effect, effectively improves the precision of estimating the position of the linear motor rotor by adopting a high-frequency injection method, and is simple and easy to implement.
Owner:JINCHENG COLLEGE NANJING UNIV OF AERONAUTICS & ASTRONAUTICS

Surface-mounted permanent magnet synchronous motor sensorless segmented delay compensation strategy

The invention discloses a surface-mounted permanent magnet synchronous motor sensorless segmented delay compensation strategy, which specifically comprises the following steps of: when the fundamental frequency of a motor is less than 47Hz, carrying out PI (Proportional-Integral) regulation on a predicted q-axis voltage error by using carrier modulation, and then eliminating the influence of total time delay of a system by compensating the conduction time of an IGBT (Insulated Gate Bipolar Translator); and after the fundamental wave frequency is greater than 47Hz, along with the increase of the rotating speed, adopting a SHEPWM + square wave modulation mode, and elimiating the delay effect by predicting a voltage vector angle, modulating the depth and estimating the rotor position. The invention provides a system delay segmentation compensation strategy aiming at the sensorless driving of the surface-mounted permanent magnet synchronous motor under hybrid pulse width modulation, meanwhile, a high-frequency square wave voltage signal injection method is adopted at zero low speed, a nonsingular terminal sliding-mode observer is adopted at medium high speed, the non-singular terminal sliding-mode observer is adopted at low speed, the influence of system delay on position sensorless control can be eliminated in the full-speed domain, and the control performance is improved.
Owner:XIAN UNIV OF TECH

Switched reluctance motor sensorless method based on difference inductance vector method

The invention discloses a switched reluctance motor sensorless method based on a difference inductance vector method, and belongs to the field of switched reluctance motor sensorless control, and the method comprises the following steps: calculating a three-phase inductance value of a switched reluctance motor in real time; delaying a three-phase inductance value expressed in a Fourier series form by pi degrees; carrying out mutual subtraction on the three-phase inductance difference values to obtain three-phase-difference-value inductance; carrying out unitization on the obtained three-phase difference value inductance; performing logic partitioning on the three-phase difference value inductor; estimating to obtain rotor position angle information at any moment in a single period by utilizing an arc tangent function and combining with three-phase difference inductance logic partitioning; according to the rotor position angle information at any moment, outputting a corresponding control signal to the switched reluctance motor to control the on and off of a power switch tube of a power converter so as to realize the sensorless control of the switched reluctance motor; the method can improve the estimation precision of the rotor position, achieves the high-precision control of the switched reluctance motor, and has a wide application prospect.
Owner:DALIAN MARITIME UNIVERSITY

Switched reluctance motor sensorless control method

The invention belongs to the field of motor control, and particularly relates to a switched reluctance motor sensorless control method. The method comprises: establishing a simplified incremental inductance model based on the simplified Fourier series expression of switched reluctance motor inductance and the relational expression of incremental inductance and inductance; measuring the incrementalinductances of three special rotor positions of a switched reluctance motor under different phase currents so as to obtain a relation that an incremental inductance model coefficient changes along with the phase currents, and establishing the nonlinear incremental inductance model of the switched reluctance motor; deducing an analytic expression for estimating the rotor position of the switched reluctance motor according to the phase increment inductance and the coefficient thereof according to the increment inductance model; and when the motor operates, detecting phase current and bus voltage, estimating excitation phase increment inductance by adopting a current slope difference method, calculating the current rotor position by utilizing the derived rotor position analytical formula, and achieving the sensorless operation control of the switched reluctance motor according to the estimated rotor position. The control method is simple, small in calculation amount, easy to realize digitalization and high in position estimation precision.
Owner:湖南贝加尔动力科技有限公司
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Try Eureka
PatSnap group products