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174 results about "Nonlinear filtering" patented technology

Nonlinear Filtering. Nonlinear filtering is the branch of statistical signal processing concerned with recursively estimating the state xk in (7.1) based on the measurements up to time k,y1:k≜{y1,…,yk} from sample 1 to k.

Airborne distributed POS transfer alignment method based on H infinity and CKF hybrid filtering

The invention relates to an airborne distributed POS transfer alignment method based on H infinity and CKF (Capacity Kalman Filtering) hybrid filtering. The method comprises the following steps: first, incorporating a deflection deformation error into measurement noise, determining a speed match measurement equation and an attitude match measurement equation, and primarily establishing a transfer alignment model of a system; designing nonlinear filtering, namely a CKF algorithm with high precision based on Kalman filtering; finally, achieving the purposes of weakening and eliminating the deflection deformation and a dynamic lever arm by utilizing good robust adaptive ability of H infinity filtering, designing an H infinity filtering algorithm, combining an H infinity filtering module and the CKF filtering, and designing a new H infinity and CKF hybrid filtering algorithm so as to estimate more accurate position, speed and attitude information of a slave inertial navigation system to complete transfer alignment. According to the airborne distributed POS transfer alignment method based on the H infinity and CKF hybrid filtering, the problem that the position, speed and attitude information of the slave inertial navigation system cannot be estimated accurately under the situation that the deflection deformation is difficult to model is solved, so that the airborne distributed POS transfer alignment method based on the H infinity and CKF hybrid filtering has the characteristics of high precision and strong anti-interference capacity.
Owner:BEIHANG UNIV

Application method of improved trackless Kalman filtering algorithm to underwater integrated navigation

The invention provides an application method of an improved trackless Kalman filtering algorithm to underwater integrated navigation. The application method comprises the following steps: defining a coordinate system required to be used; establishing a state equation of an SINS/DVL subsystem at the underwater submersible stage; establishing a measurement equation of the SINS/DVL subsystem at the underwater submersible stage; establishing a state equation of the SINS/DVL subsystem at the water surface position correction stage; establishing a measurement equation of the SINS/DVL subsystem at the water surface position correction stage; establishing a nonlinear filtering equation at the underwater submersible stages; after a period of underwater diving, an AUV emerges from the water surface,the nonlinear filtering equation at the water surface position correction stages is established, an improved unscented Kalman filter solution is performed, the time update, the measurement update andthe filter update are completed, and the timing position information correction is completed. The application method provided by the invention has the benefits that the filtering settlement efficiency and the navigation accuracy of an underwater integrated navigation system can be improved, the complexity of filtering algorithm calculation is reduced, and the real time and the stability are ensured.
Owner:SOUTHEAST UNIV

Earth-Lagrange combined constellation autonomous orbit determination method based on inter-satellite ranging

ActiveCN107421550AImproving the accuracy of long-term autonomous orbit determinationSolve the "deficit rank" problemInstruments for comonautical navigationNavigation by astronomical meansSatellite laser rangingNonlinear filter
The invention discloses an earth-Lagrange combined constellation autonomous orbit determination method based on inter-satellite ranging. The method includes following steps: step 1, establishing a state equation of an earth-Lagrange combined constellation autonomous orbit determination system; step 2, establishing a measurement equation of the earth-Lagrange combined constellation autonomous orbit determination system; step 3, determining a filtering method for realizing orbit parameter estimation; step 4, specifically realizing the earth-Lagrange combined constellation autonomous orbit determination method based on a selected filtering algorithm. By introducing a Lagrange satellite, the problem of deficient range when only inter-satellite ranging information is utilized for autonomous orbit determination is solved effectively, and complexity of system equipment is lowered; statistical characteristics of system noise are estimated online in real time through a self-adaptive nonlinear filtering algorithm, so that requirements on noise prior information are low, stability of the autonomous orbit determination filtering algorithm is improved, and autonomous orbit determination accuracy is improved.
Owner:BEIHANG UNIV

Low-precision inertial navigation initial alignment method based on quaternion CKF

The invention provides a low-precision inertial navigation initial alignment method based on a quaternion CKF. The low-precision inertial navigation initial alignment method comprises the following steps: carrying out coarse alignment by utilizing measured values of an accelerometer and a magnetometer to obtain a coarse attitude matrix; taking a position and a speed error as value measurement by using accurate outside information provided by a GPS (Global Position System); carrying out nonlinear filtering by the quaternion CKF to obtain an attitude error matrix; and finally, correcting by using the attitude error matrix to obtain an accurate attitude matrix. According to the low-precision inertial navigation initial alignment method, the value measurement of the gravitational acceleration and the magnetic force, which is carried out by the accelerometer and the magnetometer, is subjected to the coarse alignment. The problems that the gyroscope performance is low under the condition of a low-precision inertial device, the rotation angle speed of the earth can not be accurately sensed and a traditional coarse alignment method can not be applied are solved; furthermore, the quaternion CKF provided by the method can be used for a non-linear model of a large angle error, can still finish alignment under the condition of a large orientation misalignment angle and has high alignment precision.
Owner:HARBIN ENG UNIV

Mars final approaching section autonomous navigation method based on relative measurement information

The invention discloses a Mars final approaching section autonomous navigation method based on relative measurement information, and belongs to the technical field of deep space exploration. For achieving Mars final approaching section autonomous navigation, a final approaching and surrounding dynamic model is established. According to differential information of X-ray pulsar arrival time and Doppler velocity measurement information of a Mars orbiter, based on nonlinear filtering algorithm, the states of an approaching detector and the Mars orbiter undergo joint estimation, absolute navigation is achieved through utilization of two kinds of relative measurement information including the differential information of X-ray pulsar arrival time and the Doppler velocity measurement information of the Mars orbiter, and the accuracy of Mars final approaching section autonomous navigation and the accuracy of entry point state estimation are improved. The method has the following advantages: introduction of a planet ephemeris error is avoided, the adverse effect on navigation performance due to nondeterminacy of pulsar parameters is limited, the problem of state divergence resulting from long observation time of pulsars is overcome, the navigation performance of two detectors is improved at the same time, and the navigation filter accuracy and the convergence speed are increased.
Owner:BEIJING INSTITUTE OF TECHNOLOGYGY

No-gyro satellite gesture determination method based on tensor product multi-cell robust heavy hydrogen (H2) filtering

The invention relates to a no-gyro satellite gesture determination method based on tensor product multi-cell robust heavy hydrogen (H2) filtering, and belongs to the technical field of aircrafts. As for the nonlinear characteristics of satellite gesture dynamic equations and kinematical equations, the no-gyro satellite gesture determination method based on the tensor product multi-cell robust H2 filtering provides the multi-cell robust H2 filtering based on tensor product conversion to transform a nonlinear filtering problem into a linear filtering problem. The no-gyro satellite gesture determination method based on the tensor product multi-cell robust H2 filtering includes the steps of first establishing a state equation and a star sensor measurement equation of a gesture determination system and transforming a nonlinear system into a linear variable parameter error system by utilizing Jacobian linearization, then establishing linear parameter varying (LPV) system multi-cell model description according to tensor product model transformation and acquiring state estimation correction amount of the gesture determination system through combining with the robust H2 filtering, and last correcting gesture single-step pre-measurement acquired through a extended Kalman filter (EKF) method by utilizing the estimation correction amount to obtain a gesture estimation value. Accordingly, real-time updated filtering gain in the EKF method is avoid, and filtering calculated amount is reduced greatly.
Owner:BEIJING INSTITUTE OF TECHNOLOGYGY

Nonlinear filtering method based on polytope differential inclusion

The invention relates to a nonlinear filtering method based on polytope differential inclusion, which belongs to the technical field of system filtering and control. The method comprises the steps of describing a nonlinear filtering error system with a PLDI (Programming Language Design And Implementation) model, converting a nonlinear filtering algorithm design problem to a linear uncertain system robust filtering algorithm design problem, designing a dynamic equation for estimated error correction solving by a hybrid robust H2/H-to-infinity filtering method, then designing a discrete nonlinear filtering equation by combining an EKF (Extended Kalman Filter) one-step prediction equation, and applying the discrete nonlinear filtering equation to a nonlinear discrete system to obtain the state estimation of the nonlinear discrete system in real time. According to the method, the nonlinear filtering design is simplified, the filtering gain is not required to be updated in real time, and the jacobian matrix is not required to be computed in real time in the implementation process, so that the computation amount is reduced greatly, the real-time performance of the nonlinear filtering is improved effectively, and the method is applicable to the design of a nonlinear filter.
Owner:BEIJING INSTITUTE OF TECHNOLOGYGY

Nonlinear-filtering-based satellite navigation tracking loop lock loss detection method

The invention discloses a nonlinear-filtering-based satellite navigation tracking loop lock loss detection method, which comprises the following steps of: (1) determining the state quantity and observed quantity of a satellite signal tracking loop; (2) establishing a state equation and an observation equation corresponding to the state quantity and the observed quantity obtained by the step (1) respectively; (3) establishing a satellite navigation tracking loop filter based on the state equation and the observation equation obtained by the step (2); (4) setting a false alarm probability according to the counting characteristics of a fault detectable quantity, and determining a detection threshold under the condition of the false alarm probability; (5) setting a loop updating cycle, and calculating a covariance matrix of information in loop updating of each time; (6) setting a lock loss detection cycle to be integrally times the loop updating cycle and not less than the loop updating cycle; (7) calculating the fault detectable quantity in detection of each time, and comparing the fault detectable quantity with the detection threshold; and (8) if the fault detectable quantity is greater than the threshold, resetting the loop filter. By the nonlinear-filtering-based satellite navigation tracking loop lock loss detection method provided by the invention, tracking loop lock loss caused by the sudden change of the observed quantity can be effectively detected, and the filter can be timely reset, thereby improving the fault tolerance and robustness of the nonlinear-filtering-based satellite navigation tracking loop.
Owner:天宇航空数据科技(合肥)有限责任公司

Failure detection method for gas circuit part of aero-engine based on adaptive particle filtering

ActiveCN105389427AFully exploit nonlinear characteristicsSolve problems with limitations in fault diagnosisInternal-combustion engine testingSpecial data processing applicationsNonlinear filterAviation
The present invention relates to a failure detection method for a gas circuit part of an aero-engine based on adaptive particle filtering. Compared with linear filtering and a linear model method, gas circuit health diagnosis based on a nonlinear filtering algorithm and a nonlinear component level model solves the diagnostic problem of failures of component performances in a transition state of the engine, is capable of fully mining nonlinear characteristics of the engine and improves the precision and the reliability of diagnosis, and solves the problem of limitation of performing gas circuit component failure diagnosis by using a centralized structure according to a standard particle filtering algorithm; and furthermore, the method provided by the present invention takes a fused filtering structure as a basis, and by virtue of two steps of estimating noise standard deviation in real time and adding inequality constraints, defects of the standard particle filtering, such as heavy calculation burden of a central processing unit, ignorance of effective prior information and low robustness of measured noise, can be effectively avoided, so that the filtering precision is improved, and the accuracy of gas circuit health diagnosis is ensured.
Owner:上海航数智能科技有限公司

Flexible direct-current high-frequency resonance suppression method based on voltage feedforward nonlinear filtering

The invention discloses a flexible direct-current high-frequency resonance suppression method based on voltage feedforward nonlinear filtering. According to the invention, during the inner loop controlling process of a flexible direct-current current, the nonlinear filtering is carried out for a voltage feedforward link. The method specifically comprises the following steps: extracting each sequence component of an alternating-current voltage amplitude; calculating the N sampling point average values of the sequence components; comparing a current average value with the output result of a nonlinear filter in a previous period; and correcting the output result of the nonlinear filter in a current period. The output result is a fixed value which changes in a gradient mode and acts on the voltage feedforward link of the inner loop. The beneficial effects of the invention are as follows: the high-frequency resonance of a flexible direct-current and alternating-current system caused by impedance matching can be effectively inhibited. Meanwhile, the rapidity is achieved and the adjustment can be carried out along with alternating voltage when voltage disturbance such as alternating current faults occurs. The over-current risk of the converter valve is reduced. The method only needs to be achieved in the flexible direct-current secondary control software link, wherein no primary device needs to be additionally arranged. The method is low in cost, free of land occupation and convenient for engineering practice.
Owner:BEIJING SIFANG JIBAO AUTOMATION +1

Target tracking method under arbitrary linear constraints

The invention relates to a target tracking method under arbitrary linear constraints, comprising: acquiring target position measurement information from an observation radar to construct a measurementvector, wherein the measurement vector comprises distance measurement and azimuth measurement of a target relative to the original of an observation radar coordinate system; performing state augmentation of the state vector of the target at the current time point using the state vector of the target at previous time points to obtain an augmented state vector and its corresponding state equation,wherein the augmented state includes states of the k time point and the previous d consecutive time points, and d represents the time span of the augmented part; constructing pseudo-measurement according to the linear trajectory shape of the target motion to describe the arbitrary linear constraint relationship, and augmenting the pseudo-measurement into the measurement vector to obtain an augmented measurement equation; and using a nonlinear filtering method, and performing filtering by using the augmented state equation and the augmented measurement equation. The method constructs the pseudo-measurement, uses the linear trajectory shape information to improve the filtering precision, and provides a new solution for the target tracking problem under any linear constraints.
Owner:HARBIN INST OF TECH
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