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

107 results about "Software receiver" patented technology

Real-time software receiver

A real-time software receiver that executes on a general purpose processor. The software receiver includes data acquisition and correlator modules that perform, in place of hardware correlation, baseband mixing and PRN code correlation using bit-wise parallelism.
Owner:CORNELL RES FOUNDATION INC

Missile-borne deep integrated ARCKF (Adaptive Robust Capacity Kalman Filtering) method under strong maneuvering condition

The invention discloses a missile-borne deep integrated ARCKF (Adaptive Robust Capacity Kalman Filtering) method under a strong maneuvering condition. The missile-borne deep integrated ARCKF method comprises the following steps: generating a ballistic trajectory and corresponding IMU (Inertial Measurement Unit) data of a simulated strong maneuvering missile through a trajectory generator; inputting the generated ballistic trajectory into a satellite signal simulator, and generating a GNSS (Global Navigation Satellite System) intermediate-frequency signal; then inputting the generated GNSS intermediate-frequency signal into a software receiver and carrying out inertial navigation calculation on the IMU data; establishing a state equation and an observation equation of a GNNS / SINS (Strapdown Inertial Navigation System) deep integrated navigation system under a launch inertial coordinate system; simultaneously integrating a robust M-estimation algorithm in a robust estimation theory and adaptive factors to a CFK (Capacity Kalman Filtering) algorithm, forming an ARCKF algorithm, and carrying out filtering correction on a system state. The missile-borne deep integrated ARCKF method disclosed by the invention can be used for GNSS / SINS deep integrated navigation of a carrier under strong maneuvering and high dynamic conditions, and the anti-jamming capability of navigation and the navigation accuracy are effectively increased.
Owner:NANJING UNIV OF SCI & TECH

Method for capturing full bit of GPS weak signal

A whole bit acquisition method for GPS weak signals relates to the acquisition treatment of a receiver in GNSS, and solves the problems that the prior software receiver can not forecast the information bit reversal, thereby easily causing the failure of the acquisition, and the better acquisition effect is difficult to achieve by adopting the differential coherent cumulative method. 20 sequences which are compressed into 4096 sampling points are acquired after satellite signals are subjected to the treatments related to frequency mixing, sampling, quantifying and time-domain averaging; the IFFT calculation is carried out after multiplying the 20 sequences with the sequences which are conjugated with the local stored pseudo-code FFT sequences through the FFT calculation; the maximum value which is obtained by the extraction after the mod squaring of the 20 two-dimensional pseudo-code auto-correlation value matrix is compared with a threshold value sigma 1, if the maximum value is larger than the sigma 1, the acquisition is successful; if the maximum value is smaller than the sigma 1, the whole bit algorithm is utilized to seek a peak value of the extracted related values by carrying out the coherent accumulation and the non-coherent accumulation of the 20 two-dimensional pseudo-code auto-correlation value matrix after the information bit reversal, the peak value is compared with the threshold value sigma 2, if the peak value is larger than the sigma 2, the acquisition is successful; and if the peak value is smaller than the sigma 2, the re-acquisition is carried out.
Owner:HARBIN INST OF TECH

GPS (global positioning system) software receiver signal tracking method based on FPGA (field programmable gate array) and system of GPS software receiver signal tracking method

InactiveCN102621563ASolve real-timeSolve the problem of volatile locksSatellite radio beaconingDiscriminatorCarrier signal
Disclosed is a GPS (global positioning system) software receiver tracking method based on an FPGA (field programmable gate array). Inputted digital intermediate-frequency signals are transmitted into a code correlator after multiplying two channels I and Q of a carrier generator to obtain six channels of relevant results; in a carrier tracking loop, IP and QP in six channels of relevant outputs are transmitted into a phase decision device, frequency discrimination computation is carried out by a carrier frequency discriminator when phase deviation meets the condition that delta theta is larger than theta H, phase discrimination computation is carried out by a carrier phase discriminator if the phase deviation meets the condition that delta theta is smaller than theta H, a result is transmitted into the carrier generator after being filtered by a carrier loop filter so that carrier frequency is adjusted; and in a code tracking loop, IE, IL, QE and QL are taken to be transmitted into a code loop discriminator to be in phase discrimination computation, and results are transmitted into a CA (coarse acquisition) code generator after being filtered by a code loop filter so that phase ofCA codes is adjusted. The two loops are cross-coupled, the carrier frequency and the phase of the codes are synchronously tracked, accordingly, locally reproduced carriers and codes are aligned with signals, and navigation data bits are obtained after integral judgment for the IP is carried out by a posterior integral accumulation decision device.
Owner:SOUTHEAST UNIV

Parallel navigation satellite signal tracking method based on GPU (graphics processing unit) and system thereof

ActiveCN103278829APowerful floating-point parallel computing capabilityTake full advantage of hardware performanceSatellite radio beaconingCarrier signalEngineering
The invention discloses a parallel navigation satellite signal tracking method based on GPU (graphics processing unit) and a system thereof. The method comprises the following steps: constructing a multichannel carrier tracking loop and a pseudo code tracking loop on CPU(central processing unit)-GPU, wherein the CPU is in charge of data reading, loop phase discrimination and control functions and the like, and the GPU is in charge of the relevant calculation and integral summation functions of a great quantity of data sequences; after the GPU finishes the integral summation calculation, adopting a two-stage binary tree calculation structure; calculating an error by a carrier phase discriminator and a CA (certification authority) code phase discriminator on the CPU; and controlling a local carrier phase and a CA code phase to correct to realize the tracking. According to the invention, the defects of poor flexibility and black box operation of a hardware receiver system and the defect that various navigation satellite signal systems can not be supported are overcome. Meanwhile, the processing speed and precision of a software receiver can be enhanced, the cost of the software receiver is lowered, and a GNSS (global navigation satellite system) software receiver can track the multichannel navigation satellite signal in real time.
Owner:SOUTHEAST UNIV

Realizing method of multi-mode GNSS (Global Navigation Satellite System) software receiver based on multi-core processor

The invention discloses a realizing method of a multi-mode GNSS (Global Navigation Satellite System) software receiver based on a multi-core processor. One of N available cores is distributed to be used as a scheduling core for scheduling and controlling a multi-mode GNSS receiver, and the rest N-1 cores are used as processing cores for processing intermediate-frequency signals of the receiver. The realizing method comprises the steps of: firstly, distributing all the processing cores to form a related operation module by the scheduling core for completing satellite search of a GNSS, feeding the searched result back to the scheduling core; and then scheduling the processing cores by the scheduling core according to the searched result, reserving partial processing cores to maintain the work of the related operation module, forming a data channel consisting of a satellite tracking channel module and a positioning resolving module through the rest processing cores to complete the processing of the intermediate-frequency signal of the GNSS for realizing positioning navigation. By using strong processing capacity of the multi-core processor, the traditional GNSS hardware baseband chipis replaced with the multi-core processor for processing navigation signals of different types of satellites of multiple systems, and flexible configuration and scheduling can be realized.
Owner:SOUTH CHINA UNIV OF TECH

Miniature positioning, navigation and timing system

The invention provides a miniature positioning, navigation and timing system comprising a chip atomic clock, a micro inertial measurement unit and a global positioning system (GPS) software receiver. The chip atomic clock is used to provide a clock signal for the micro inertial measurement unit and the GPS software receiver, assist the GPS software receiver in navigation positioning operation, and perform correction according to a correction signal sent by the GPS software receiver. The micro inertial measurement unit is used to measure motion information of a measured target according to the clock signal, wherein the motion information includes acceleration and angular speed. The GPS software receiver is used to receive a positioning signal sent by a GPS and perform navigation positioning operation according to the positioning signal and the motion information of the measured target in order to obtain positioning, navigation and timing information. The system of the invention has the advantages of high robustness PNT service, high precision, and strong anti-interference performance.
Owner:TSINGHUA UNIV

Implementation method for self-adaptive GPS software receiver

The invention designs a GPS software receiver, which is suitable for various working environments with low signal to noise ratio, high dynamic, assistance of an inertial navigation system (INS) or independent working and the like, automatically regulates performance as required to adapt to different working environments and achieves the optimal information utilization to the fullest extent as possible. An implementation method for the GPS software receiver comprises the following steps of: independently regulating the tracking bandwidth of each tracking channel according to signal strength; combining the advantages of long-term noncorrelation integral and short-term correlation integral to design a tracking loop with high-sensitivity real-time output; realizing real-time estimation of a receiver crystal frequency error model by using a method for estimating fixed intervals; and finally, based on the deep combination, improving capture velocity and tracking dynamic performance of a weak signal. The implementation method for the GPS software receiver can fully use all detectable satellite signals, can improve the tracking dynamic performance of the weak signal by utilizing auxiliary information of INS information, and also accelerates new star search when INS information assistance exists.
Owner:GUANGZHOU HESHENG TEACHING EQUIP CO LTD

Global position system real-time software receiving machine and real-time processing method thereof

The invention relates to a navigation and position equipment in the electronic technical field and real-time processing thereof, in particular to a real-time software receiver of the global position system, which implements real-time location by using the received GPS signal from the global position satellite system and is used for the signal sampling and the computer software processing, as well as a real-time processing method of the invention. The apparatus consists of a complex programmable logic device and an interface module of serial-to-parallel conversion, etc. The method executes the processing of baseband signal for the computer software under the windows XP environment, the method mainly resolves the related technical problems of how to implement the interfaces of signal sampling and transmission modules and the processing of baseband signal, etc. The invention has the advantages that the apparatus implements the real-time execution in the windows XP system of Microsoft, and the software adopts the bit arithmetic way, which reduces the computation, accelerates the processing speed and achieves real-time location, and higher precision and sensitivity through the rapidity of signal processing.
Owner:SHANGHAI BEIGA NAVIGATION TECH CO LTD

Satellite/ inertial ultra-tight integration system and method based on Beidou/GPS dual-mode software receiver

The invention discloses a satellite/ inertial ultra-tight integration system and method based on a Beidou/GPS dual-mode software receiver. The system comprises an active satellite antenna module, a satellite radio frequency receiving module, a satellite baseband processing module, an inertial navigation module and an integrated navigation module. The method comprises the following steps: after theBeidou/GPS dual-mode software receiver finishes first positioning, carrying out initialization on an inertial navigation system; entering an ultra-tight integration mode, and estimating I,Q information IINS and QINS; serving the difference value between I,Q information obtained by the Beidou/GPS dual-mode software receiver and the IINS and QINS as observed quantity of an EKF; carrying out correction on the inertial navigation system; and estimating carrier Doppler frequency and pseudo code phase of a satellite signal, and feeding the carrier Doppler frequency and the pseudo code phase back toa carrier NCO and a code NCO to form a closed loop. The system and method can improve positioning accuracy of the satellite/ inertial integrated navigation system, improve system robustness, and improve tracking performance of the satellite receiver under high-dynamic weak-signal and strong-interference conditions.
Owner:SOUTHEAST UNIV

Avoiding and stripping method for Neumann-Hoffman codes in navigation messages of Beidou navigation satellite system D1

The invention discloses an avoiding and stripping method for Neumann-Hoffman codes in navigation messages of a Beidou navigation satellite system D1. The method comprises the steps that according to the encoding characteristics of the Neumann-Hoffman (NH) codes in a navigation message signal system of the Beidou navigation system D1, a unique sequence NH code avoiding method based on probability statistics is proposed at the satellite capturing stage, and the influence of jumping of the NH codes on capturing is successfully avoided; through parallel code phase search with the step length decreasing step by step, accurate capturing of the phase position and carrier frequency of spreading codes of a Beidou satellite is successfully achieved; meanwhile, an NH code stripping method for combined codes based on the NH codes and frame synchronization codes (Pre) is proposed in the frame synchronization step, and stripping of the NH codes and output of the navigation messages can be effectively achieved while subframes are synchronized. The avoiding and stripping method for the NH codes in the navigation messages of the Beidou navigation satellite system D1 is applicable to a Beidou satellite navigation receiver and a software receiver, and the same idea is applicable to other navigation satellite systems for which fixed sequence secondary encoding is adopted.
Owner:NANJING UNIV OF AERONAUTICS & ASTRONAUTICS

System for testing performance of GPS hardware receiver based on GPS software receiver in dynamic environment

The invention discloses a system for testing the performance of a GPS hardware receiver based on a GPS software receiver in a dynamic environment. The system provides dynamic environment parameters Din through a three-axle table, then outputs medium frequency information R(tk) after sampling the satellite information acquired by an antenna installed on the three-axle table by using a medium frequency sampler, and finally analyzes the information by the GPS software receiver, a D-PLL-P model and a D-PLL-F model, thereby reproducing the problems of lock loss and low output accuracy of the GPS hardware receiver caused in the dynamic environment; and the reproduced parameters can provide a guide for the design of the GPS hardware receiver.
Owner:BEIHANG UNIV

System for estimating influence of interference signal on GPS performance

The invention discloses a system for estimating influence of interference signal on GPS performance based on a GPS software receiver. The system comprises a GPS antenna module and radio frequency module subsystem, an interference signal simulation subsystem, a GPS software receiver subsystem, and a GPS software receiver estimation subsystem, wherein the GPS antenna module and radio frequency module subsystem is used for converting the received GPS signal from the radio frequency to the intermediate frequency by down-frequency conversion, and outputting the digital intermediate frequency signal obtained by sampling to the GPS software receiver subsystem; the interference signal simulation subsystem is used for generating the digital interference signal, and outputting the generated digital interference signal to the GPS software receiver subsystem; the GPS software receiver subsystem is used for performing signal acquisition, signal tracking, bit synchronization and frame synchronization, pseudo range computation and computation of a satellite position and a user position on the inputted digital intermediate frequency signal and digital interference signal, and outputting the results to the GPS software receiver estimation subsystem; and the GPS software receiver estimation subsystem is used for performing error analysis on the received results to realize estimation of the influence of the interference signal on GPS performance. The system can determine which aspects in the interference signal are main factors of influencing the GPS performance.
Owner:NAT ASTRONOMICAL OBSERVATORIES CHINESE ACAD OF SCI

Software receiver-based distributed deep integrated navigation method and system

The invention provides a software receiver-based distributed deep integrated navigation method and system. According to the software receiver-based distributed deep integrated navigation method and system, a GNSS software receiver adopts Doppler frequency shift calculated by Doppler frequency shift estimation; an auxiliary receiver tracking loop performs carrier tracking and code tracking, and filters outputted GNSS pseudo-range and pseudo-range rate information and provides the filtered information to an integrated navigation module; a carrier tracking loop adjusts a carrier NCO according to the Doppler frequency shift and carrier frequency errors outputted by a carrier loop filter; a code tracking loop adjust a code NCO according to frequency provided by the carrier tracking loop and code frequency errors outputted by a code loop filter; and therefore, two-way assistance of a GNSS and an SINS can be realized. With the software receiver-based distributed deep integrated navigation method and system of the invention adopted, the influence of the dynamic condition of a carrier on the carrier tracking loop can be decreased, and the tracking errors of the GNSS receiver can be decreased under a high dynamic environment, and the dynamic tracking performance of the GNSS receiver under the high dynamic environment can be improved, and therefore, the navigation and positioning accuracy of the integrated navigation system can be further improved.
Owner:NANJING UNIV OF SCI & TECH

Weak signal capturing method based on overlapping difference cycle coherent integration

The invention provides a weak signal capturing method based on overlapping difference cycle coherent integration. The weak signal capturing method based on overlapping difference cycle coherent integration comprises the steps that firstly, a section of medium-frequency signal data lasting for 20M ms+10 ms is taken, carrier-removal processing is carried out, a Doppler frequency shift range, a searching stepped frequency and a detection threshold are set; secondly, the data after carrier-removal processing are segmented according to the length that L= 10 ms, self-overlapping processing is carried out on each data block, and FFT conversion is carried out; thirdly, FFT conversion is carried out a locally generated C / A code, a conjugate is taken and is multiplied by each result finally obtained in the step 2, and IFFT processing is carried out; fourthly, conjugate complex number multiplication is carried out each data block processed in the step 3 and the adjacent data blocks whose data are overlapped with those of the data block, then grouping correlation summation is carried out, and whether the signals are successfully captured is judged. The weak signal capturing method based on overlapping difference cycle coherent integration is applied to weak signal capturing of a single-frequency civil software receiver in a global positioning system.
Owner:HARBIN ENG UNIV

Navigation signal pseudo-range deviation correction method

PendingCN112180410AWeaken the impact of rangingHigh positioning accuracySatellite radio beaconingEngineeringRanging
The invention relates to a navigation signal pseudo-range deviation correction method. The method comprises the following steps: S1, calibrating pseudo-range deviation characteristic parameters: measuring a satellite-ground distance between a satellite and an antenna; accurately measuring the transmission time delay of a receiving terminal of the large-aperture antenna; analyzing error characteristics of pseudo-range measurement of a receiver; S2, calibrating inter-satellite difference: calibrating the time delay of a receiving channel of the receiver; measuring the inter-station distance; measuring a satellite-ground distance; carrying out synchronous measurement testing of the antenna and an omnidirectional receiving antenna; synchronously calibrating inter-satellite differences of satellite navigation signals in a visual range; synchronously calibrating the inter-satellite difference of GNSS satellites; S3, testing and verifying: analyzing the positioning error of the receiver, andverifying the correction precision of the pseudo-range measurement correction parameter; and adjusting the pseudo-range measurement correlator interval of a software receiver and the filter bandwidthkey parameters, and researching the quantitative relation between the parameters of the software receiver and the signal ranging deviation. The method has the advantages that the influence of pseudo-range deviation on distance measurement of the software receiver is weakened, and the system positioning precision is improved.
Owner:NAT TIME SERVICE CENT CHINESE ACAD OF SCI
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