CN117092668B - System and method for testing generic and conductive fusion application terminal - Google Patents
System and method for testing generic and conductive fusion application terminal Download PDFInfo
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S19/00—Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
- G01S19/01—Satellite radio beacon positioning systems transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
- G01S19/13—Receivers
- G01S19/23—Testing, monitoring, correcting or calibrating of receiver elements
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- H04B17/391—Modelling the propagation channel
- H04B17/3912—Simulation models, e.g. distribution of spectral power density or received signal strength indicator [RSSI] for a given geographic region
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- H—ELECTRICITY
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- H04B17/00—Monitoring; Testing
- H04B17/40—Monitoring; Testing of relay systems
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
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Abstract
The application relates to a system and a method for testing a generic and conductive fusion application terminal, wherein the system comprises: the control software subsystem is used for sending the first configuration information to the navigation signal simulation subsystem and sending the second configuration information to the communication signal simulation subsystem; the navigation signal simulation subsystem is used for generating a GNSS navigation message based on the first configuration information and sending the GNSS navigation message to a to-be-tested lead fusion application terminal; the communication signal simulation subsystem is used for generating a low-rail communication signal based on the second configuration information and sending the low-rail communication signal to a to-be-tested generic fusion application terminal; the terminal test subsystem is used for receiving navigation and communication processing results generated by the to-be-tested navigation fusion application terminal based on the GNSS navigation message and the low-rail communication signal, and testing the to-be-tested navigation fusion application terminal based on configuration information and processing results obtained from the control software subsystem.
Description
Technical Field
The application relates to the field of terminal testing, in particular to a system and a method for testing a generic and conductive fusion application terminal.
Background
Along with the increasing demands of people on high-precision positioning and high-efficiency communication, low-rail lead fusion has become an important solution, but the test on the low-rail lead fusion application terminal does not exist at present so as to ensure the positioning accuracy of the low-rail lead fusion application terminal.
Disclosure of Invention
The application provides a system and a method for testing a lead-through fusion application terminal, which are used for solving the problem that the technical scheme for testing a low-rail lead-through fusion application terminal does not exist in the prior art.
In a first aspect, the present application provides a system for testing a generic fusion application terminal, including: the system comprises a control software subsystem, a navigation signal simulation subsystem, a communication signal simulation subsystem and a terminal test subsystem; the control software subsystem is used for sending first configuration information to the navigation signal simulation subsystem and sending second configuration information to the communication signal simulation subsystem; wherein the first configuration information and the second configuration information each include at least one of the following configurations: constellation configuration information, terminal configuration information, error configuration information, and communication configuration information; the navigation signal simulation subsystem is used for generating a GNSS navigation message based on the first configuration information and sending the GNSS navigation message to a to-be-tested lead fusion application terminal; the communication signal simulation subsystem is used for generating a low-rail communication signal based on the second configuration information and sending the low-rail communication signal to the to-be-tested conductance fusion application terminal; wherein the low rail communication signal comprises at least one of: SPT navigation data and navigation precision correction data; the SPT navigation data and the navigation precision correction data in the communication signals come from a navigation simulation module in the navigation signal simulation subsystem or are obtained from the outside by the communication signal simulation subsystem; the terminal test subsystem is used for receiving navigation and communication processing results generated by the to-be-tested generic and conductive fusion application terminal based on the GNSS navigation message and the low-rail communication signal, and testing the to-be-tested generic and conductive fusion application terminal based on configuration information and the processing results obtained from the control software subsystem.
In a second aspect, the present application provides a method for testing a generic fusion application terminal based on the system in the first aspect, including: the control software subsystem sends first configuration information to the navigation signal simulation subsystem and sends second configuration information to the communication signal simulation subsystem; wherein the first configuration information and the second configuration information each include at least one of the following configurations: constellation configuration information, terminal configuration information, error configuration information, and communication configuration information; the navigation signal simulation subsystem generates a GNSS navigation message based on the first configuration information and sends the GNSS navigation message to a to-be-tested lead fusion application terminal; the communication signal simulation subsystem generates a low-rail communication signal based on the second configuration information and sends the low-rail communication signal to the to-be-tested conductance fusion application terminal; wherein the low rail communication signal comprises at least one of: SPT navigation data and navigation precision correction data; the SPT navigation data and the navigation precision correction data in the communication signals come from a navigation simulation module in the navigation signal simulation subsystem or are obtained from the outside by the communication signal simulation subsystem; and the terminal testing subsystem receives navigation and communication processing results generated by the navigation fusion application terminal based on the GNSS navigation message and the low-rail communication signal, and tests the processing results based on configuration information acquired from the control software subsystem.
In a third aspect, the present application provides an electronic device, including: at least one communication interface; at least one bus connected to the at least one communication interface; at least one processor coupled to the at least one bus; and at least one memory connected with the at least one bus, wherein the processor is configured to execute the method for testing the conductive fusion application terminal according to the first aspect of the present application.
In a fourth aspect, the present application further provides a computer storage medium, where computer executable instructions are stored, where the computer executable instructions are configured to perform the method for testing a generic converged application terminal according to the first aspect of the present application.
Compared with the prior art, the technical scheme provided by the embodiment of the application has the following advantages: according to the system for testing the lead-through fusion application terminal, after the GNSS navigation message and the low-rail communication signal are sent to the lead-through fusion application terminal to be tested, the lead-through fusion application terminal can be tested based on the processing result of the lead-through fusion application terminal based on the GNSS navigation message and the low-rail communication signal, so that the research and development test and network access application test requirements of the terminal are met, and the stable operation of the lead-through fusion application terminal in the practical application process is ensured.
Drawings
The accompanying drawings, which are incorporated in and constitute a part of this specification, illustrate embodiments consistent with the invention and together with the description, serve to explain the principles of the invention.
In order to more clearly illustrate the embodiments of the invention or the technical solutions of the prior art, the drawings which are used in the description of the embodiments or the prior art will be briefly described, and it will be obvious to a person skilled in the art that other drawings can be obtained from these drawings without inventive effort.
One or more embodiments are illustrated by way of example and not limitation in the figures of the accompanying drawings, in which like references indicate similar elements, and in which the figures of the drawings are not to be taken in a limiting sense, unless otherwise indicated.
Fig. 1 is a schematic structural diagram of a system for testing a generic fusion application terminal according to an embodiment of the present application;
fig. 2 is a schematic structural diagram of an alternative conductive fusion application terminal test system according to an embodiment of the present application;
FIG. 3 is a second schematic diagram of an alternative system for testing a conductive fusion application terminal according to an embodiment of the present disclosure;
fig. 4 is a third schematic structural diagram of an alternative system for testing a fusion application terminal according to an embodiment of the present application;
fig. 5 is a schematic structural diagram of a communication signal simulation subsystem provided in an embodiment of the present application to simulate a plurality of virtual conductance fusion application terminals;
fig. 6 is a schematic structural diagram of testing a plurality of conductive fusion application terminals according to an embodiment of the present application;
fig. 7 is a flowchart of a method for testing a generic fusion application terminal according to an embodiment of the present application;
fig. 8 is a schematic structural diagram of an electronic device according to an embodiment of the present application.
Detailed Description
For the purposes of making the objects, technical solutions and advantages of the embodiments of the present application more clear, the technical solutions of the embodiments of the present application will be clearly and completely described below with reference to the drawings in the embodiments of the present application, and it is apparent that the described embodiments are some embodiments of the present application, but not all embodiments. All other embodiments, which can be made by one of ordinary skill in the art without undue burden from the present disclosure, are within the scope of the present application based on the embodiments herein.
The following disclosure provides many different embodiments, or examples, for implementing different structures of the invention. In order to simplify the present disclosure, components and arrangements of specific examples are described below. They are, of course, merely examples and are not intended to limit the invention. Furthermore, the present invention may repeat reference numerals and/or letters in the various examples. This repetition is for the purpose of simplicity and clarity and does not in itself dictate a relationship between the various embodiments and/or configurations discussed.
Firstly, explaining a generic fusion application terminal in the embodiment of the application;
the navigation fusion application terminal is a terminal device combining low-orbit satellite communication and navigation technologies. The system utilizes a low orbit satellite network to provide a communication function and combines a navigation technology to realize position location and navigation service. Through the communication fusion application terminal, the user can realize the communication functions of voice and video communication with other people, short message sending, mail sending and the like. Meanwhile, the low-orbit satellite communication technology is adopted, so that the coverage range is wide, the communication in the global scope can be realized, and the communication is not limited by geographic positions.
In addition, the navigation fusion application terminal can also provide navigation service. By utilizing the built-in navigation system and the capability of receiving the low-orbit satellite signals, a user can accurately obtain own position information, and can obtain path planning and navigation guidance through a navigation function so as to help people find a destination. The advantage of the converged application terminal is its global covered communication capability and accurate navigation services. Communication and navigation operations can be performed wherever the user is. This is of great convenience to persons who need to frequently cross different territories. In summary, the converged communication application terminal is a terminal device combining low-orbit satellite communication and navigation technology, can realize communication and accurate navigation service in the global scope, and provides convenient and efficient communication and navigation experience for users.
Fig. 1 is a schematic diagram of a system for testing a generic fusion application terminal according to an embodiment of the present application, where, as shown in fig. 1, the system for testing a generic fusion application terminal includes: the system comprises a control software subsystem, a navigation signal simulation subsystem, a communication signal simulation subsystem and a terminal test subsystem; wherein,
the control software subsystem is used for sending the first configuration information to the navigation signal simulation subsystem and sending the second configuration information to the communication signal simulation subsystem; wherein the first configuration information and the second configuration information each include at least one of the following configurations: constellation configuration information, terminal configuration information, error configuration information, and communication configuration information;
in a specific embodiment, the information content carried in the first configuration information and the second configuration information may be consistent or inconsistent; the consistent condition means that the first configuration information and the second configuration information carry all configuration information which can be configured by the control software subsystem, which is equivalent to that the control software subsystem sends two identical configuration files to the navigation signal simulation subsystem and the communication signal simulation subsystem, and the navigation signal simulation subsystem and the communication signal simulation subsystem acquire the configuration information required by themselves after receiving the configuration files. The inconsistent situation means that the control software subsystem respectively sends the required configuration information to the navigation signal simulation subsystem and the communication signal simulation subsystem, for example, the navigation signal simulation subsystem needs to send the GNSS navigation message to the navigation fusion application terminal, so that time information, constellation information, frequency point information, user track information and communication interaction configuration information in the configuration information are needed; the communication signal simulation subsystem needs to send a low-rail communication signal to the lead fusion application terminal, and needs communication node configuration information, navigation data configuration information and time synchronization information.
The constellation configuration information at least comprises constellation and frequency point information; the terminal configuration information at least comprises user track information; the error configuration information includes at least: navigation data and time synchronization information; the communication configuration information includes at least communication node information. The configuration information in the control software subsystem in the embodiments of the present application is used to control and configure the navigation signal simulation subsystem and the communication signal simulation subsystem.
The navigation signal simulation subsystem is used for generating a GNSS navigation message based on the first configuration information and sending the GNSS navigation message to a to-be-tested lead fusion application terminal;
the communication signal simulation subsystem is used for generating a low-rail communication signal based on the second configuration information and sending the low-rail communication signal to a to-be-tested generic fusion application terminal; wherein the low rail communication signal includes at least one of: SPT navigation data and navigation precision correction data. The SPT navigation data and the navigation precision correction data in the communication signal come from a navigation simulation module in a navigation signal simulation subsystem, or are obtained from the outside by the communication signal simulation subsystem;
the terminal test subsystem is used for receiving navigation and communication processing results generated by the to-be-tested navigation fusion application terminal based on the GNSS navigation message and the low-rail communication signal, and testing the to-be-tested navigation fusion application terminal based on configuration information and processing results obtained from the control software subsystem.
Therefore, through the system for testing the lead-through fusion application terminal, after the GNSS navigation message and the low-rail communication signal are sent to the lead-through fusion application terminal to be tested, the lead-through fusion application terminal can be tested based on the processing result of the lead-through fusion application terminal based on the GNSS navigation message and the low-rail communication signal, so that the research and development test and network access application test requirements of the terminal are met, and the stable operation of the lead-through fusion application terminal in the practical application process is ensured.
In an alternative implementation manner of the embodiment of the present application, on the basis of fig. 2, the navigation signal simulation subsystem of the embodiment of the present application may further include, as shown in fig. 2: the system comprises a navigation simulation module, a navigation signal generation module and a first radio frequency module;
the navigation simulation module is used for generating a navigation message and observation data based on the first configuration information and sending the navigation message and the observation data to the navigation signal generation module;
in specific examples the navigation messages include satellite ephemeris, clock bias, ionosphere parameters, etc.; the observed data may include pseudoranges, carrier phases, doppler shifts. The observation data is used for channel delay simulation and simulates a signal transmission process of transmitting real satellite signals to a ground receiver terminal.
The navigation signal generation module is used for generating a navigation intermediate frequency signal from the navigation message and the observed data and transmitting the navigation intermediate frequency signal to the radio frequency module;
it should be noted that, the navigation intermediate frequency signal is generated by the navigation message and the observation data, so that the navigation intermediate frequency signal can be sent to the navigation fusion application terminal after up-conversion through the radio frequency module, that is, the navigation intermediate frequency signal or the GNSS navigation signal after up-conversion processing is carried substantially.
The radio frequency module is used for carrying out up-conversion processing on the navigation intermediate frequency signal to obtain a GNSS navigation message, and sending the GNSS navigation message to the navigation fusion application terminal.
Therefore, the navigation signal simulation subsystem in the embodiment of the application provides the GNSS navigation message for the lead fusion application terminal so that the lead fusion application terminal can perform navigation positioning, and prepares for subsequent test of the lead fusion application terminal.
In general, in an optional implementation manner of this embodiment of the present application, the navigation simulation module in the navigation signal simulation subsystem may be further configured to generate simulated SPT (Security Positioning and Timing, secure positioning time service) information and simulated navigation precision correction data based on the first configuration information, and send the simulated SPT information and the simulated navigation precision correction data to the communication signal simulation subsystem in combination with the visible ephemeris synchronization of the lead fusion application terminal.
The simulated SPT information is used for assisting the GNSS to perform navigation positioning and is used for GNSS navigation positioning backup information, that is, the simulated SPT information not only can assist the GNSS to perform navigation positioning so as to achieve the purpose of rapid convergence, but also can be used as low-precision backup information of GNSS navigation positioning, and can also realize low-precision positioning when no GNSS navigation signal exists. In addition, the navigation precision correction data in the embodiments of the present application include track and clock correction, code deviation and carrier phase deviation, and troposphere and ionosphere corrections. The navigation precision correction data in the embodiment of the application is used for testing the high-precision positioning function and performance index of the lead fusion terminal.
It can be seen that, in the embodiment of the present application, the SPT information and the navigation precision correction data required by the communication signal simulation subsystem may be provided by the navigation simulation module in the navigation signal simulation subsystem, and in other examples, the communication signal simulation subsystem may also obtain the required SPT information and the navigation precision correction data from the outside (such as a ground base station data center).
In an alternative implementation manner of the embodiment of the present application, on the basis of fig. 2, a communication signal simulation subsystem of the embodiment of the present application includes, as shown in fig. 3: the system comprises a communication simulation module, an intermediate frequency signal processing module and a second radio frequency module;
the second radio frequency module is used for receiving the communication request signal of the lead fusion application terminal, performing down-conversion on the communication request signal and then sending the communication request signal to the intermediate frequency signal processing module;
the intermediate frequency signal processing module is used for processing the communication request signal after the down-conversion processing and transmitting the communication request signal to the communication simulation module;
the communication simulation module is used for sending a low-rail communication signal to the intermediate-frequency signal processing module based on the received processed communication request signal;
the intermediate frequency signal processing module is also used for processing the low-rail communication signal and then sending the low-rail communication signal to the second radio frequency module;
the second radio frequency module is also used for carrying out up-conversion processing on the processed low-rail communication signals and then sending the processed low-rail communication signals to the lead fusion application terminal.
It can be seen that the communication signal simulation subsystem of the embodiment of the present application may receive a communication request signal from the fusion application terminal, where the communication request signal is used to request corresponding data (precision correction data for requesting positioning navigation or communication data for performing voice or text). The communication simulation module processes the low-rail communication data through the intermediate frequency signal processing module based on the communication request signal, and then up-converts the low-rail communication data into a low-rail communication signal to be output to the lead fusion application terminal, so that full-duplex communication test is realized.
Combining the SPT information and the navigation precision correction data required by the communication signal simulation subsystem provided by the navigation simulation module in the navigation signal simulation subsystem, or acquiring the required SPT information and the navigation precision correction data from the outside by the communication signal simulation subsystem, processing the voice, the data, the SPT navigation information and the navigation precision correction data into digital information by the communication simulation module in the communication signal simulation subsystem, transmitting the digital information to the intermediate frequency signal processing module, generating a communication intermediate frequency signal by the intermediate frequency signal processing module according to a communication request signal, and outputting a low-rail communication to a communication fusion application terminal by the radio frequency module.
Thus, the low rail communication signal in the practice of the present application includes at least one of the following: SPT navigation data and navigation precision correction data.
In an alternative implementation manner of the present application, on the basis of fig. 3, the terminal test subsystem in the embodiment of the present application may further include, as shown in fig. 4: the system comprises a navigation positioning test module, a communication test module and a navigation fusion application test module;
the navigation positioning test module is used for respectively testing positioning precision, signal power and navigation integrity based on configuration information and processing results;
the positioning accuracy can be evaluated by comparing the measured positioning result of the lead fusion application terminal with the actual position of the true calibration. And comparing, analyzing and evaluating the signal power according to the power of the signal received by the lead fusion application terminal in real time and the power requirement required by navigation positioning. Navigation integrity refers to the assessment from receiver sensitivity, accuracy and reliability of receiving and processing navigation signals.
The communication test module is used for testing the connection performance of the communication link, the quality of communication data and the transmission performance of the communication data based on the configuration information and the processing result; the communication data in the embodiment of the application comprises SPT navigation data and navigation precision correction data and other data used for communication.
The connection performance of the communication link may refer to evaluating the communication transmission speed and stability, among other things. The audio and speech quality assessment may be assessed from speech intelligibility, volume, noise suppression functions. The data transmission performance can evaluate the speed, reliability and delay of data receiving and transmitting of the lead fusion application terminal.
And the navigation fusion application testing module is used for testing the navigation positioning mode of the navigation fusion application terminal based on the configuration information and the processing result.
It should be noted that, the conducting fusion application terminal in the embodiment of the present application may perform positioning in three modes of PPP (Precise Point Positioning, precise single-point positioning), RTK (Real-Time Kinematic), ppp+rtk, so that the conducting fusion application test module may test indexes such as convergence Time, positioning precision, dynamic performance, robustness of positioning performance, etc. of the PPP, RTK, PPP +rtk positioning function.
In a specific example, the fusion application terminal is used for performing PPP positioning based on navigation precision correction data (which may also be referred to as GNSS precision correction data), that is, satellite signals (low-orbit satellites and medium-high-orbit satellites) are received through a GNSS receiver and transmitted to a server for data processing and calculation, and then, the factors such as star position and clock error information, delay of an earth ion layer and the like are utilized, precision calculation is performed through multi-frequency observation data, and a more accurate position result can be obtained under the correction of the navigation precision correction data.
In a specific example, the navigation fusion application terminal for performing RTK positioning based on navigation precision correction data refers to real-time calculation and correction by using differential signals between a reference station (or base station) and a mobile station (subscriber station). The reference station accurately measures the position thereof and transmits differential data to the mobile station, the mobile station performs real-time calculation and correction through differential observation data between the mobile station and the reference station, and more accurate position calculation can be obtained under correction of navigation precision correction data.
Furthermore, the high precision of PPP and the real-time property of RTK are combined in the PPP+RTK mode, after the initial position is obtained by using single-point PPP positioning, the RTK technology is utilized for real-time dynamic satellite signal correction and updating, and the positioning precision and the position stability are further improved.
In an optional implementation manner of the embodiment of the present application, the communication signal simulation subsystem in the embodiment of the present application is further configured to simulate a plurality of virtual converged application terminals, where a plurality of virtual converged application terminals (simulation terminal 1, simulation terminal 2, … … and simulation terminal N) are in communication and interconnection with a converged application terminal to be tested, so as to test a converged performance index of a converged application terminal channel to be tested, as shown in fig. 5.
In an optional implementation manner of the embodiment of the application, the system for testing the generic fusion application terminal in the embodiment of the application includes multiple groups of subsystems, each group of subsystems including a control software subsystem, a navigation signal simulation subsystem and a communication signal simulation subsystem; each group of subsystems is connected with a to-be-tested lead fusion application terminal; the terminal test subsystem may be connected to a plurality of to-be-tested generic and converged application terminals to test the plurality of to-be-tested generic and converged application terminals, as shown in fig. 6.
That is, the multiple on-off application terminal test systems are used to test the multiple on-off application terminals respectively, and the communication signal simulation subsystem of the multiple on-off application terminal test systems can realize communication simulation networking and realize mutual transmission of communication signals between actual terminals. And the terminal test evaluation subsystem in one of the lead fusion application terminal test systems is used for evaluating and analyzing the test results of all the lead fusion application terminals, so that the performance index of a single terminal can be analyzed, the networking test performance index can be analyzed, and the requirements of various test scenes can be met.
Based on the above system for testing the generic and generic fusion application terminal in fig. 1 to fig. 4, the embodiment of the present application further provides a method for testing the generic and generic fusion application terminal, as shown in fig. 7, where the steps of the method include:
step 701, the control software subsystem sends first configuration information to the navigation signal simulation subsystem and sends second configuration information to the communication signal simulation subsystem; wherein the first configuration information and the second configuration information each include at least one of the following configurations: constellation configuration information, terminal configuration information, error configuration information, and communication configuration information;
step 702, the navigation signal simulation subsystem generates a GNSS navigation message based on the first configuration information, and sends the GNSS navigation message to the generic and generic fusion application terminal to be tested;
step 703, the communication signal simulation subsystem generates a low-rail communication signal based on the second configuration information, and sends the low-rail communication signal to the to-be-tested generic fusion application terminal; wherein the low rail communication signal includes at least one of: SPT navigation data and navigation precision correction data; the SPT navigation data and the navigation precision correction data in the communication signal come from a navigation simulation module in a navigation signal simulation subsystem, or are obtained from the outside by the communication signal simulation subsystem;
and step 704, the terminal testing subsystem receives navigation and communication processing results generated by the navigation fusion application terminal based on the GNSS navigation message and the low-rail communication signal, and tests the processing results based on configuration information acquired from the control software subsystem.
Through the steps 701 to 704 in the embodiment of the present application, after sending the GNSS navigation message and the low-rail communication signal to the to-be-tested generic fusion application terminal, the generic fusion application terminal may be tested based on the processing result of the generic fusion application terminal based on the GNSS navigation message and the low-rail communication signal, so as to meet the requirements of research and development test and network access application test of the terminal, and ensure the stable operation of the generic fusion application terminal in the practical application process.
As shown in fig. 8, the embodiment of the present application provides an electronic device, which includes a processor 811, a communication interface 812, a memory 813, and a communication bus 814, wherein the processor 811, the communication interface 812, the memory 813 complete communication with each other through the communication bus 814,
a memory 113 for storing a computer program;
in an embodiment of the present application, the processor 811 is configured to implement the method for testing a generic fusion application terminal provided in any of the foregoing method embodiments when executing the program stored in the memory 813, and the functions of the method are similar, and are not repeated herein.
The embodiment of the application also provides a computer readable storage medium, on which a computer program is stored, the computer program implementing the steps of the method for testing the lead fusion application terminal provided in any one of the method embodiments described above when being executed by a processor.
The apparatus embodiments described above are merely illustrative, wherein the elements illustrated as separate elements may or may not be physically separate, and the elements shown as elements may or may not be physical elements, may be located in one place, or may be distributed over a plurality of network elements. Some or all of the modules may be selected according to actual needs to achieve the purpose of the solution of this embodiment.
From the above description of embodiments, it will be apparent to those skilled in the art that the embodiments may be implemented by means of software plus a general purpose hardware platform, or may be implemented by hardware. Based on such understanding, the foregoing technical solution may be embodied essentially or in a part contributing to the related art in the form of a software product, which may be stored in a computer readable storage medium, such as ROM/RAM, a magnetic disk, an optical disk, etc., including several instructions for causing a computer device (which may be a personal computer, a server, or a network device, etc.) to perform the method described in the respective embodiments or some parts of the embodiments.
It is to be understood that the terminology used herein is for the purpose of describing particular example embodiments only, and is not intended to be limiting. As used herein, the singular forms "a", "an" and "the" are intended to include the plural forms as well, unless the context clearly indicates otherwise. The terms "comprises," "comprising," "includes," "including," and "having" are inclusive and therefore specify the presence of stated features, steps, operations, elements, and/or components, but do not preclude the presence or addition of one or more other features, steps, operations, elements, components, and/or groups thereof. The method steps, processes, and operations described herein are not to be construed as necessarily requiring their performance in the particular order described or illustrated, unless an order of performance is explicitly stated. It should also be appreciated that additional or alternative steps may be used.
The foregoing is only a specific embodiment of the invention to enable those skilled in the art to understand or practice the invention. Various modifications to these embodiments will be readily apparent to those skilled in the art, and the generic principles defined herein may be applied to other embodiments without departing from the spirit or scope of the invention. Thus, the present invention is not intended to be limited to the embodiments shown herein but is to be accorded the widest scope consistent with the principles and novel features disclosed herein.
Claims (9)
1. The utility model provides a lead integration application terminal test system which characterized in that includes: the system comprises a control software subsystem, a navigation signal simulation subsystem, a communication signal simulation subsystem and a terminal test subsystem; wherein,
the control software subsystem is used for sending the first configuration information to the navigation signal simulation subsystem and sending the second configuration information to the communication signal simulation subsystem; wherein the first configuration information and the second configuration information each include at least one of the following configurations: constellation configuration information, terminal configuration information, error configuration information, and communication configuration information; the navigation signal simulation subsystem is used for generating a GNSS navigation message based on the first configuration information and sending the GNSS navigation message to a to-be-tested lead fusion application terminal;
the communication signal simulation subsystem is used for generating a low-rail communication signal based on the second configuration information and sending the low-rail communication signal to the to-be-tested conductance fusion application terminal; wherein the low rail communication signal comprises at least one of: SPT navigation data and navigation precision correction data; the SPT navigation data and the navigation precision correction data in the communication signals come from a navigation simulation module in the navigation signal simulation subsystem or are obtained from the outside by the communication signal simulation subsystem;
the terminal test subsystem is used for receiving navigation and communication processing results generated by the to-be-tested generic and conductive fusion application terminal based on the GNSS navigation message and the low-rail communication signal, and testing the to-be-tested generic and conductive fusion application terminal based on configuration information and the processing results obtained from the control software subsystem.
2. The system of claim 1, wherein the navigation signal simulation subsystem comprises: the system comprises a navigation simulation module, a navigation signal generation module and a first radio frequency module;
the navigation simulation module is used for generating a navigation message and observation data based on the first configuration information and sending the navigation message and the observation data to the navigation signal generation module;
the navigation signal generation module is used for generating a navigation intermediate frequency signal from the navigation message and the observed data and sending the navigation intermediate frequency signal to the radio frequency module;
the radio frequency module is used for carrying out up-conversion processing on the navigation intermediate frequency signal to obtain the GNSS navigation message, and sending the GNSS navigation message to the navigation fusion application terminal.
3. The system of claim 2, wherein the navigation simulation module is further configured to generate simulated secure positioning time service SPT information and simulated navigation precision correction data based on the first configuration information, and to send the simulated secure positioning time service SPT information and the simulated navigation precision correction data to the communication signal simulation subsystem in conjunction with the navigation fusion application terminal visible ephemeris synchronization; the simulation SPT information is used for assisting the GNSS in navigation positioning and is used for GNSS navigation positioning backup information; the analog navigation precision correction data includes track and clock correction, code bias and carrier phase bias, troposphere and ionosphere corrections.
4. The system of claim 1, wherein the communication signal simulation subsystem comprises: the system comprises a communication simulation module, an intermediate frequency signal processing module and a second radio frequency module;
the second radio frequency module is used for receiving the communication request signal of the conductance fusion application terminal, performing down-conversion on the communication request signal and then sending the communication request signal to the intermediate frequency signal processing module;
the intermediate frequency signal processing module is used for processing the communication request signal after the down-conversion processing and then sending the communication request signal to the communication simulation module;
the communication simulation module is used for sending the low-rail communication signal to the intermediate-frequency signal processing module based on the received processed communication request signal;
the intermediate frequency signal processing module is further used for processing the low-rail communication signal and then sending the low-rail communication signal to the second radio frequency module;
the second radio frequency module is further configured to up-convert the processed low-rail communication signal and send the up-converted low-rail communication signal to the generic and conductive fusion application terminal.
5. The system of claim 4, wherein the communication simulation module is further configured to obtain actual SPT navigation information and actual navigation precision correction data from outside.
6. The system of claim 1, wherein the terminal test subsystem comprises: the system comprises a navigation positioning test module, a communication test module and a navigation fusion application test module;
the navigation positioning test module is used for respectively testing positioning precision, signal power and navigation integrity based on the configuration information and the processing result;
the communication test module is used for testing the connection performance of the communication link, the quality of communication data and the transmission performance of the communication data based on the configuration information and the processing result;
and the navigation fusion application testing module is used for testing the navigation positioning mode of the navigation fusion application terminal based on the configuration information and the processing result.
7. The system of claim 1, wherein the communication signal simulation subsystem is further configured to simulate a plurality of virtual converged application terminals, and the plurality of virtual converged application terminals are communicatively interconnected with the converged application terminal to be tested, so as to test a channel converged performance index of the converged application terminal to be tested.
8. The system of claim 1, wherein the lead fusion application terminal test system comprises a plurality of sets of subsystems, each set of subsystems comprising one of the control software subsystems, one of the navigation signal simulation subsystems, and one of the communication signal simulation subsystems; each group of subsystems is connected with a to-be-tested lead fusion application terminal; the terminal test subsystem is connected with a plurality of to-be-tested lead fusion application terminals so as to test the to-be-tested lead fusion application terminals.
9. A method for testing a generic fusion application terminal based on the system of any one of claims 1 to 8, comprising:
the control software subsystem sends first configuration information to the navigation signal simulation subsystem and sends second configuration information to the communication signal simulation subsystem; wherein the first configuration information and the second configuration information each include at least one of the following configurations: constellation configuration information, terminal configuration information, error configuration information, and communication configuration information;
the navigation signal simulation subsystem generates a GNSS navigation message based on the first configuration information and sends the GNSS navigation message to a to-be-tested lead fusion application terminal;
the communication signal simulation subsystem generates a low-rail communication signal based on the second configuration information and sends the low-rail communication signal to the to-be-tested conductance fusion application terminal; wherein the low rail communication signal comprises at least one of: SPT navigation data and navigation precision correction data; the SPT navigation data and the navigation precision correction data in the communication signals come from a navigation simulation module in the navigation signal simulation subsystem or are obtained from the outside by the communication signal simulation subsystem;
and the terminal testing subsystem receives navigation and communication processing results generated by the navigation fusion application terminal based on the GNSS navigation message and the low-rail communication signal, and tests the processing results based on configuration information acquired from the control software subsystem.
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| CN110737010A (en) * | 2019-09-19 | 2020-01-31 | 西安空间无线电技术研究所 | safe positioning time service signal generation system based on low-orbit communication satellite |
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| CN115941413A (en) * | 2022-10-19 | 2023-04-07 | 西安空间无线电技术研究所 | High-power conduction fusion navigation signal generation and receiving method |
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| CN110737010A (en) * | 2019-09-19 | 2020-01-31 | 西安空间无线电技术研究所 | safe positioning time service signal generation system based on low-orbit communication satellite |
| CN115941413A (en) * | 2022-10-19 | 2023-04-07 | 西安空间无线电技术研究所 | High-power conduction fusion navigation signal generation and receiving method |
| CN115630537A (en) * | 2022-12-21 | 2023-01-20 | 长沙北斗产业安全技术研究院股份有限公司 | Navigation signal simulation method and system based on-chip simulation |
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