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34results about How to "Reduce truncation error" patented technology

Novel INS (inertial navigation system)/ GPS (global position system) combined position and orientation method

The invention provides a novel INS (inertial navigation system) / GPS (global position system) combined position and orientation method. The novel INS / GPS combined position and orientation method includes adopting a linear Kalman filter to perform filtering estimation to GPS original measurement data, and outputting optimal GPS navigation estimation value; according to the optimal position estimation value, providing initial position information to the INS, according to the optimal speed estimation value, providing initial speed information to the INS and solving INS initial measuring data to acquire INS navigation information; adopting a dynamic error model to establish a 9-order extended Kalman filter, integrating the INS navigation information with an optimal GPS navigation estimation value, performing feedback rectification to all INS navigation information at the same moment, and outputting optimal position data and orientation data after rectification and integration. The novel INS / GPS combined position and orientation method has such advantages as high precision, fast data processing speed and low hardware requirement and is applicable to low-cost INS / GPS combined position and orientation plan.
Owner:CHINA UNIV OF GEOSCIENCES (BEIJING)

Double-rate Kalman filtering method based on GNSS/INS deep integrated navigation

The invention discloses a double-rate Kalman filtering method based on GNSS/INS deep integrated navigation. The method comprises the following steps of 1, building a state equation according to the initial position, the rate and the attitude information of a carrier, and initializing the parameters of the Kalman filtering; 2, performing state prediction updating on M step lengths and obtaining a predicted value of a prior state quantity which is described in the specification; 3 correcting the prior state quantity which is described in the specification to obtain a predicted value of a posterior state quantity which is described in the specification; 4, adaptively updating the errors of the state quantities and a systematic error covariance matrix, and compensating an inertial navigation result by using the predicted value of the posterior state quantity which is described in the specification to obtain the position, the rate and attitude information of the carrier; and 5, updating thepredicted value of a posterior state quantity which is described in the specification after the compensation. The method can reduce a truncation error caused by the low update frequency of GNSS satellite data or the losing lock of the satellite data during a data fusion algorithm of the GNSS/INS deep integrated navigation, and simultaneously solve a navigation positioning error caused by the non-synchronization of INS data and GNSS data.
Owner:SOUTHEAST UNIV

State estimation method based on high-order unscented Kalman filtering

The invention relates to a state estimation method based on high-order unscented Kalman filtering. A high-order unscented Kalman filter is used for finishing the state estimation task in the target tracking process. According to the state estimation method based on the high-order unscented Kalman filtering, the state estimation task in the target tracking process is finished by the high-order unscented Kalman filter. In the target tracking process, the state equation and the measurement equation of target tracking are established; a sigma point required for the target tracking filter is obtained by high-order unscented transformation, and the weight of the sigma point is calculated; and the state estimation is obtained by iterating the sigma point and the weight of the sigma point to realize the real-time tracking of the target. The tracking precision of the state estimation method is higher than those of the existing target tracking methods based on other filters, a proper performance parameter k is selected to further improve the precision of the proposed high-order unscented Kalman filtering (UKF) target tracking method, and the high-precision real-time tracking to the target is realized. The state estimation method disclosed by the invention is applied to the technical field of the target tracking.
Owner:HARBIN ENG UNIV

Electromagnetic transient simulation method containing switching characteristic sub-network

InactiveCN105260516AEliminate numerical oscillationsEliminate numerical oscillation problemsSpecial data processing applicationsCapacitanceTransient analysis
The invention relates to an electromagnetic transient simulation method containing a switching characteristic sub-network, and belongs to the technical field of electromagnetic transient analysis in electric power systems. According to the simulation method, a breaker and electronic power switching elements are designed into an independent switching sub-network; the network only comprises an electronic power sub-switch, the breaker and related elements (resistors, inductors, capacitors and the like); the network performs modeling through a rational polynomial approximation based exponential fitting method provided by the invention; and the rest of networks perform modeling by a conventional method (an implicit trapezoid method, a backward Euler method, a damping trapezoidal method or a modified combining form thereof). In offline/real-time calculation, only the switching sub-network performs iteration or interpolation calculation, and the rest of networks do not participate in iteration or interpolation. The switching sub-network adopts a high-order algorithm provided by the invention, so that numerical oscillation can be immunized; and meanwhile, the workload of model modification is relatively low, so that engineering promotion is facilitated.
Owner:TSINGHUA UNIV +3

Wave-absorbing material reflection measuring device and method

The invention provides a wave-absorbing material reflection measuring device. The wave-absorbing material reflection measuring device comprises a transmitting antenna, a receiving antenna, an arched frame, a time-domain pulse generator, a time-domain pulse receiver and a good conductor board, wherein the receiving antenna and the transmitting antenna are symmetrically placed on the arched frame; positions and actinal surface normal directions of the transmitting antenna and the receiving antenna are adjustable; the time-domain pulse generator generates a time-domain pulse to excite the transmitting antenna; the time-domain pulse receiver receives a time-domain signal; a wave-absorbing material is laid on the surface, facing the transmitting antenna and the receiving antenna, of the good conductor board to obtain a wave-absorbing material board. A wave-absorbing material reflection measuring method comprises the following steps: enabling included angles between the actinal surface normals of the receiving antenna and the transmitting antenna and the normal of the measured wave-absorbing material board to be equal; transmitting the time-domain pulse signal, and receiving a time-domain received signal waveform; selecting a time-domain reflected signal of the measured wave-absorbing material by using a time window, and performing time domain and frequency domain processing to obtain a frequency-domain reflected waveform of the wave-absorbing material. Through the wave-absorbing material reflection measuring device and the wave-absorbing material reflection measuring method, a test error caused by time domain-frequency domain conversion is reduced.
Owner:BEIJING INST OF RADIO METROLOGY & MEASUREMENT

New WENO (Weighted Essentially Non-oscillatory) format construction method under trigonometric function framework

The invention discloses a new WENO (Weighted Essentially Non-oscillatory) format construction method under a trigonometric function framework. Compared with a classic essentially non-oscillatory format constructed through utilization of an algebraic polynomial, a weighted essentially non-oscillatory format constructed through utilization of a trigonometric function polynomial has the advantage that the weighted essentially non-oscillatory format is easier to simulate wave or high frequency oscillation problems, can obtain high order numerical precision can be obtained in a smooth area, and keeps essentially non-oscillatory property at shock wave and contact discontinuity locations. Even if the new TWENO format and the classic five-order WENO format employ information at the same five points, according to the new TWENO format, the lower global L<1> and L<infinite> norm truncation errors can be obtained. According to linear weights employed by the new TWENO format, the optimum solutiondoes not need to be obtained through burdensome numerical calculation, the linear weights can be set as any positive numbers satisfying the fact that the sum is 1. Compared with the classic WENO format, the new TWENO format has the advantages that the new TWENO format is simpler, has higher robustness and is easier to popularize to a high-dimensional space. According to the new TWENO format, a plurality of classic Euler problems are effectively and numerically simulated, and the effectiveness is sufficiently verified.
Owner:NANJING UNIV OF AERONAUTICS & ASTRONAUTICS

0+ error immune electromagnetic transient simulation algorithm used under sudden change of input quantity

ActiveCN104375876ASolve the problem of state quantity jump numerical oscillationImmune non-prototypical oscillationsSoftware simulation/interpretation/emulationSpecial data processing applicationsTransient analysisElectric power system
The invention relates to a 0+ error immune electromagnetic transient simulation algorithm used under the sudden change of input quantity and belongs to the technical field of electromagnetic transient analysis of an electric system. According to the method, by means of the impulse response invariable principle, numerical sampling of a continuous signal of the system corresponds to Z conversion of a discrete signal, and the fundamental form of an element based on operation conductance and a history current item is given. Based on the form, a system network equation is obtained according to the node analysis method, and a system electromagnetic transient simulation result is obtained according to the same steps. The method has the advantages that the truncation error is smaller than that generated through currently adopted methods and the 0+ error purpose is realized under the sudden change of the immune input quantity, achieves non-linear load modeling of the electric system, solves the problem of oscillation of an electronic power switch model state variable outburst value, and provides a new way for electromagnetic transient branch-level modeling of the electric system.
Owner:TSINGHUA UNIV +1

Finite difference multi-resolution trigonometric function WENO format simulation method

The invention discloses a finite difference multi-resolution trigonometric function WENO format simulation method which comprises the following steps: S1, discretizing a hyperbolic conservation law equation into a space semi-discrete ordinary differential equation, and reconstructing a high-order approximation value of numerical flux by adopting a novel finite difference multi-resolution trigonometric function WENO format; S2, adopting a four-order TVB Runge-Kutta time discrete formula to discretize the space semi-discrete finite difference format into a space-time full-discrete high-precisionfinite difference format; S3, obtaining an approximate value on the next time layer according to the space-time full-discrete high-precision finite difference format; and sequentially iterating to obtain a numerical result of the flow field at the termination moment in the calculation area. According to the method, high-precision numerical simulation can be carried out on various compressible flow field problems, especially the low-pressure low-density problem and the high-frequency oscillation problem, numerical simulation of the compressible flow field problems and the low-pressure low-density problem of waves and high-frequency oscillation is achieved, robustness is higher, and the method is easier to popularize to a high-dimensional space.
Owner:NANJING UNIV OF AERONAUTICS & ASTRONAUTICS

Method applied to unmanned aerial vehicle for improving navigation calculating precision

The invention discloses a method applied to an unmanned aerial vehicle for improving navigation calculating precision, and belongs to the field of aerial automation control. The method specifically comprises the following steps: 1, acquiring starting point information, destination point information and current position information of the unmanned aerial vehicle; 2, splitting longitude data, latitude data and height data of forty floating point types in the starting point, the destination point and the current position, so as to obtain a trigonometric function equation of the data of the forty floating point types; and 3, acquiring laterodeviation distance and laterodeviation speed according to the starting point information, the destination point information and the current position information obtained in step 1 of the unmanned aerial vehicle, and rectifying the deviation of a track route of the unmanned aerial vehicle according to the laterodeviation distance and the laterodeviation speed. According to the method applied to the unmanned aerial vehicle for improving navigation calculating precision, the navigation calculation of the forty floating point types is carried out, thus the intercepting error occurring in the operation can be reduced, and the calculation precision can be improved; once the position precision of a DGPS (Differential Global Positioning System) is 0.1m, the laterodeviation distance output precision under the navigation calculation of the forty floating point types can reach 0.3m, and thus the purposes of precise guiding, taking off and landing control can be met.
Owner:BEIHANG UNIV

Sine windowing electromagnetism band gap band-stop filter

The invention discloses a sine windowing electromagnetism band gap band-stop filter which comprises an upper-layer microstrip line structure, a middle-layer medium substrate and a lower-layer grounding metal face. The upper-layer microstrip line structure is attached to the upper surface of the middle medium substrate and the grounding metal face is attached to the lower surface of the middle medium substrate. The upper-layer microstrip line structure comprises an input port, an output port and a periodical microstrip line which is modulated by a windowing function, wherein the input port and the output port are formed in the two ends of the upper-layer microstrip line structure. The weighting technology with a grounded flaw face is directly applied to microstrip transmission line design of the one-dimension sine EBG band-stop filter. A signal is weighted through a window function, thus, truncation errors generated when limited truncation is carried out on an infinite time-domain signal are reduced. Thus, under the condition that performances of the device are not changed, the device can be miniaturized through a small sine periodical amount. Passband ripples and reflected sidelobe performances of the band-stop filter are improved, thus, the manufacturing technology of the sine windowing electromagnetism band gap band-stop filter is simpler.
Owner:RES INST OF XIAN JIAOTONG UNIV & SUZHOU

A dual-rate Kalman filter method based on gnss/ins deep integrated navigation

The invention discloses a double-rate Kalman filtering method based on GNSS / INS deep integrated navigation. The method comprises the following steps of 1, building a state equation according to the initial position, the rate and the attitude information of a carrier, and initializing the parameters of the Kalman filtering; 2, performing state prediction updating on M step lengths and obtaining a predicted value of a prior state quantity which is described in the specification; 3 correcting the prior state quantity which is described in the specification to obtain a predicted value of a posterior state quantity which is described in the specification; 4, adaptively updating the errors of the state quantities and a systematic error covariance matrix, and compensating an inertial navigation result by using the predicted value of the posterior state quantity which is described in the specification to obtain the position, the rate and attitude information of the carrier; and 5, updating thepredicted value of a posterior state quantity which is described in the specification after the compensation. The method can reduce a truncation error caused by the low update frequency of GNSS satellite data or the losing lock of the satellite data during a data fusion algorithm of the GNSS / INS deep integrated navigation, and simultaneously solve a navigation positioning error caused by the non-synchronization of INS data and GNSS data.
Owner:SOUTHEAST UNIV

An Adaptive Interference Source Location Flight Verification Method

The invention discloses an adaptive interference source positioning flight verification method, the monitoring and positioning of all kinds of radio interference sources can be realized, and the radio safety of civil aviation is ensured. The basic principle of flight verification of radio interference positioning is that airborne radio detection equipment is used to obtain a direction of arrival wave of an interference source, combined with flight parameters of position, speed, flight attitude and height of an aircraft, the single station cross positioning principle is applied, an adaptive filtering method is used, and the position information of the interference source can be accurately obtained. The method comprises a step of establishing a state equation of verifying an aircraft interference detection system, a step of establishing a nonlinear measurement equation of verifying the aircraft interference detection system, a step of discretizing the system state equation and the measurement equation, and a step of using an adaptive interference source positioning algorithm to solve the discretized equations, and outputting the position of the interference source. According to the method, the adaptive interference source positioning algorithm is used, and the positioning precision of the positioning algorithm and the stability of a positioning process are improved.
Owner:BEIHANG UNIV

State estimation method based on high-order unscented Kalman filtering

The invention relates to a state estimation method based on high-order unscented Kalman filtering. A high-order unscented Kalman filter is used for finishing the state estimation task in the target tracking process. According to the state estimation method based on the high-order unscented Kalman filtering, the state estimation task in the target tracking process is finished by the high-order unscented Kalman filter. In the target tracking process, the state equation and the measurement equation of target tracking are established; a sigma point required for the target tracking filter is obtained by high-order unscented transformation, and the weight of the sigma point is calculated; and the state estimation is obtained by iterating the sigma point and the weight of the sigma point to realize the real-time tracking of the target. The tracking precision of the state estimation method is higher than those of the existing target tracking methods based on other filters, a proper performance parameter k is selected to further improve the precision of the proposed high-order unscented Kalman filtering (UKF) target tracking method, and the high-precision real-time tracking to the target is realized. The state estimation method disclosed by the invention is applied to the technical field of the target tracking.
Owner:HARBIN ENG UNIV

A 0+ Error Immune Electromagnetic Transient Simulation Method in the Case of Sudden Input Quantity

ActiveCN104375876BSolve the problem of state quantity jump numerical oscillationImmune non-prototypical oscillationsSpecial data processing applicationsTransient analysisElectric power system
The invention relates to a 0+ error immune electromagnetic transient simulation algorithm used under the sudden change of input quantity and belongs to the technical field of electromagnetic transient analysis of an electric system. According to the method, by means of the impulse response invariable principle, numerical sampling of a continuous signal of the system corresponds to Z conversion of a discrete signal, and the fundamental form of an element based on operation conductance and a history current item is given. Based on the form, a system network equation is obtained according to the node analysis method, and a system electromagnetic transient simulation result is obtained according to the same steps. The method has the advantages that the truncation error is smaller than that generated through currently adopted methods and the 0+ error purpose is realized under the sudden change of the immune input quantity, achieves non-linear load modeling of the electric system, solves the problem of oscillation of an electronic power switch model state variable outburst value, and provides a new way for electromagnetic transient branch-level modeling of the electric system.
Owner:TSINGHUA UNIV +1

Apparatus and method for measuring reflection of absorbing material

The invention provides a wave-absorbing material reflection measuring device. The wave-absorbing material reflection measuring device comprises a transmitting antenna, a receiving antenna, an arched frame, a time-domain pulse generator, a time-domain pulse receiver and a good conductor board, wherein the receiving antenna and the transmitting antenna are symmetrically placed on the arched frame; positions and actinal surface normal directions of the transmitting antenna and the receiving antenna are adjustable; the time-domain pulse generator generates a time-domain pulse to excite the transmitting antenna; the time-domain pulse receiver receives a time-domain signal; a wave-absorbing material is laid on the surface, facing the transmitting antenna and the receiving antenna, of the good conductor board to obtain a wave-absorbing material board. A wave-absorbing material reflection measuring method comprises the following steps: enabling included angles between the actinal surface normals of the receiving antenna and the transmitting antenna and the normal of the measured wave-absorbing material board to be equal; transmitting the time-domain pulse signal, and receiving a time-domain received signal waveform; selecting a time-domain reflected signal of the measured wave-absorbing material by using a time window, and performing time domain and frequency domain processing to obtain a frequency-domain reflected waveform of the wave-absorbing material. Through the wave-absorbing material reflection measuring device and the wave-absorbing material reflection measuring method, a test error caused by time domain-frequency domain conversion is reduced.
Owner:BEIJING INST OF RADIO METROLOGY & MEASUREMENT
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