CN110824509B - Navigation satellite signal generation simulator - Google Patents
Navigation satellite signal generation simulator Download PDFInfo
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- CN110824509B CN110824509B CN201911179348.0A CN201911179348A CN110824509B CN 110824509 B CN110824509 B CN 110824509B CN 201911179348 A CN201911179348 A CN 201911179348A CN 110824509 B CN110824509 B CN 110824509B
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C25/00—Manufacturing, calibrating, cleaning, or repairing instruments or devices referred to in the other groups of this subclass
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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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Abstract
The invention provides a navigation satellite signal generation simulator, which comprises a digital signal generation unit and a downlink signal radio frequency unit, wherein: the digital signal generating unit is used for generating a digital intermediate frequency signal according to the time frequency signal; the downlink signal radio frequency unit is used for converting the digital intermediate frequency signal into an analog intermediate frequency signal, finishing up-conversion of the analog intermediate frequency signal and outputting a radio frequency navigation signal with corresponding power so as to simulate generation of a navigation satellite signal; the digital intermediate frequency signals comprise B1 frequency point navigation signals, B2 frequency point navigation signals and B3 frequency point navigation signals; the GPU in the digital signal generating unit simultaneously generates digital baseband signals of B1 frequency point navigation signals, B2 frequency point navigation signals and B3 frequency point navigation signals, and overcomes the defects of long development period, high cost, complex debugging, difficult upgrading and reconstruction and the like of the traditional architecture of a satellite signal generator combining DSP and FPGA.
Description
Technical Field
The invention relates to the technical field of ground simulation of navigation satellites, in particular to a navigation satellite signal generation simulator based on a GPU.
Background
The satellite simulator is used for carrying out the test verification task of the whole navigation system on behalf of the state of the space section.
The navigation signal generation simulator is one of important components of a satellite simulator, and has the main functions of generating B1, B2 and B3 frequency point navigation signals (determined by Beidou navigation system interface control files, similar to the names of L1, L5 and the like of a GPS), receiving navigation messages and modulating the navigation messages to downlink navigation signals. Meanwhile, the capability of reconstructing downlink signals is required, and specifically includes the capability of reconstructing lookup tables, power ratios, information rates, spreading codes, spreading parameters, channel codes and the like.
In order to ensure the reliability of the test result, the key technical indexes of the satellite simulator and the real satellite are required to be consistent, and meanwhile, the satellite simulator is required to have the characteristics of flexibility and configurability in order to conveniently develop test verification tasks of various new technologies and new systems. The traditional navigation satellite signal generator adopts a structure combining DSP and FPGA, and the structure has the defects of long development period, high cost, complex debugging, difficult upgrading and reconstruction and the like, so that the traditional navigation satellite signal generator is not suitable for being used as a ground test task.
Disclosure of Invention
The invention aims to provide a navigation satellite signal generation simulator, which aims to solve the problem of poor flexibility of the existing signal generation simulator.
In order to solve the above technical problem, the present invention provides a navigation satellite signal generation simulator, which includes a digital signal generation unit and a downlink signal radio frequency unit, wherein:
the digital signal generating unit is used for generating a digital intermediate frequency signal according to the time frequency signal; the downlink signal radio frequency unit is used for converting the digital intermediate frequency signal into an analog intermediate frequency signal, finishing up-conversion of the analog intermediate frequency signal and outputting a radio frequency navigation signal with corresponding power so as to simulate generation of a navigation satellite signal;
the digital intermediate frequency signals comprise B1 frequency point navigation signals, B2 frequency point navigation signals and B3 frequency point navigation signals;
and the GPU in the digital signal generating unit simultaneously generates digital baseband signals of the B1 frequency point navigation signal, the B2 frequency point navigation signal and the B3 frequency point navigation signal.
Optionally, in the navigation satellite signal generation simulator, the digital signal generation unit and the downlink signal radio frequency unit are connected by a high-speed optical fiber.
Optionally, in the navigation satellite signal generation simulator, the digital intermediate frequency signal includes a B1 frequency point navigation signal, a B2 frequency point navigation signal, and a B3 frequency point navigation signal;
and the GPU in the digital signal generating unit simultaneously generates digital baseband signals of the B1 frequency point navigation signal, the B2 frequency point navigation signal and the B3 frequency point navigation signal through streaming, and the digital baseband signals are divided into 13 channels.
Optionally, in the navigation satellite signal generation simulator, the digital signal generating unit includes a digital carrier generating module, a digital signal processing module, and an interface communication module, wherein:
the digital carrier generation module drives the phase accumulation of the digital carrier through a 1PPS signal of an external component, and then takes the phase accumulation value as an address of a digital carrier lookup table to output the carrier through the digital carrier lookup table;
the digital signal processing module is used for generating a spread spectrum code and a channel code of a digital baseband signal layer, generating a B1 frequency point navigation signal, a B2 frequency point navigation signal and a B3 frequency point navigation signal, receiving a navigation message generated by a navigation task processor, and modulating the navigation message to a B1 frequency point navigation signal, a B2 frequency point navigation signal and a B3 frequency point navigation signal;
the interface communication module is used for providing an interface for the digital signal processing module to communicate with the outside.
Optionally, in the navigation satellite signal generation simulator, the digital signal processing module includes a precision ranging code, a C code generator, an amplitude mapper, a baseband shaping filter, and an anti-Sinc filter, where:
the precision ranging code and the C code generator generate corresponding code streams under the control of the 1PPS signals of the external components and the time frequency signals of corresponding frequency points, the code streams are modulated to navigation messages of corresponding channels and then converted into non-return-to-zero codes through the amplitude mapper, the baseband shaping filter filters high-frequency components, then the digital intermediate-frequency signals are modulated to the digital intermediate-frequency signals, and the digital intermediate-frequency signals are filtered through the anti-Sinc filter and then output to the downlink signal radio-frequency unit through the interface communication module.
Optionally, in the navigation satellite signal generation simulator, the downlink signal radio frequency unit includes a DA conversion module, a modulation module, a numerical control attenuation module, and an isolator, where:
the DA conversion module converts the B1 frequency point navigation signal, the B2 frequency point navigation signal and the B3 frequency point navigation signal into the analog intermediate frequency signal;
the modulation module is used for completing frequency point analog orthogonal modulation of the B1 frequency point navigation signal, the B2 frequency point navigation signal and the B3 frequency point navigation signal and switching between a spread spectrum mode and a single carrier mode;
the numerical control attenuation module completes the output power control of the radio frequency signal;
the isolator is used for reducing the influence of the back-end reflected signal on the front-end signal caused by impedance mismatching.
Optionally, in the navigation satellite signal generation simulator, the number of the DA conversion modules is 4, the DA conversion value of each branch is 16bit, and the rate of the DA conversion module is 500 MHz.
Optionally, in the navigation satellite signal generation simulator, the adjustable range of the numerical control attenuation module is 8dB, and the step amplitude is 1 dB.
In the navigation satellite signal generation simulator provided by the invention, the digital intermediate frequency signal is generated by the digital signal generating unit according to the time frequency signal, the downlink signal radio frequency unit is used for converting the digital intermediate frequency signal into the analog intermediate frequency signal and finishing the up-conversion of the analog intermediate frequency signal and outputting the radio frequency navigation signal with corresponding power, so that the software of the digital baseband signal processing function is realized, the flexible and variable upgrading of a signal system, a signal format, a text arrangement, a modulation mode and the like is facilitated, the designability, the expansibility and the maintainability of a system are greatly enhanced, and the test verification of the system and key technology on the ground is facilitated.
Furthermore, the GPU in the digital signal generating unit simultaneously generates digital baseband signals of B1 frequency point navigation signals, B2 frequency point navigation signals and B3 frequency point navigation signals through streams, and the high-speed computing capability of the GPU can ensure the real-time performance of signal processing and the consistency of information receiving and signal generating time delay with real satellites.
In addition, a corresponding code stream is generated by a precise ranging code and C code generator under the control of a 1PPS signal of an external component and a time frequency signal of a corresponding frequency point, and is modulated to a navigation message of a corresponding channel and then converted into a non-return-to-zero code by an amplitude mapper; the hardware function degradation is realized, so that the hardware state does not restrict the system upgrading, and the reconfigurable capability of information processing is improved.
Furthermore, B1 frequency point navigation signals, B2 frequency point navigation signals and B3 frequency point navigation signals are converted into analog intermediate frequency signals through a DA conversion module, a modulation module completes frequency point analog orthogonal modulation of the B1 frequency point navigation signals, the B2 frequency point navigation signals and the B3 frequency point navigation signals, a numerical control attenuation module completes output power control of radio frequency signals, the capacity of storing sampled data in real time and playing back the sampled data to the radio frequency signals off line is achieved, and problem backtracking and troubleshooting are facilitated.
Finally, due to the chip sampling and holding characteristics of the DA conversion module, the DA conversion module has a Sinc filtering effect on signals and inhibits high-frequency components, so that the signal quality is influenced, and therefore reverse Sinc filtering is performed before the digital baseband signals are output to the DA conversion module, and the Sinc effect of the DA chip is compensated.
Drawings
FIG. 1 is a schematic diagram of a navigation satellite signal generation simulator in accordance with an embodiment of the present invention;
FIG. 2 is a schematic diagram of digital IF signal generation of a GNSS signal generation simulator according to an embodiment of the present invention;
shown in the figure: 10-a digital signal generating unit; 11-a digital signal processing module; 12-an interface communication module; 20-a downlink signal radio frequency unit; a 21-DA conversion module; 22-a modulation module; 23-a numerical control attenuation module; 24-an isolator; 30-external components.
Detailed Description
The navigation satellite signal generation simulator proposed by the present invention is further described in detail below with reference to the accompanying drawings and specific embodiments. Advantages and features of the present invention will become apparent from the following description and from the claims. It is to be noted that the drawings are in a very simplified form and are not to precise scale, which is merely for the purpose of facilitating and distinctly claiming the embodiments of the present invention.
The invention provides a navigation satellite signal generation simulator, which aims to solve the problem of poor flexibility of the existing signal generation simulator.
In order to achieve the above idea, the present invention provides a navigation satellite signal generation simulator, which includes a digital signal generation unit and a downlink signal radio frequency unit, wherein: the digital signal generating unit is used for generating a digital intermediate frequency signal according to the time frequency signal; the downlink signal radio frequency unit is used for converting the digital intermediate frequency signal into an analog intermediate frequency signal, finishing up-conversion of the analog intermediate frequency signal and outputting a radio frequency navigation signal with corresponding power so as to simulate generation of a navigation satellite signal; the digital intermediate frequency signals comprise B1 frequency point navigation signals, B2 frequency point navigation signals and B3 frequency point navigation signals; and the GPU in the digital signal generating unit simultaneously generates digital baseband signals of the B1 frequency point navigation signal, the B2 frequency point navigation signal and the B3 frequency point navigation signal through streams.
< example one >
The present embodiment provides a navigation satellite signal generation simulator, as shown in fig. 1, the navigation satellite signal generation simulator includes a digital signal generating unit 10 and a downlink signal rf unit 20, wherein: the digital signal generating unit 10 is configured to generate a digital intermediate frequency signal according to the time-frequency signal; the downlink signal rf unit 20 is configured to convert the digital intermediate frequency signal into an analog intermediate frequency signal, perform up-conversion on the analog intermediate frequency signal, and output an rf navigation signal with corresponding power. The digital signal generating unit 10 and the downlink signal radio frequency unit 20 are connected by a high-speed optical fiber.
Specifically, in the navigation satellite signal generation simulator, the digital intermediate frequency signal includes a B1 frequency point navigation signal, a B2 frequency point navigation signal and a B3 frequency point navigation signal; the digital signal generating unit 10 generates digital baseband signals of the B1 frequency point navigation signal, the B2 frequency point navigation signal, and the B3 frequency point navigation signal simultaneously in a GPU by using a stream (stream) technique, where the digital baseband signals are divided into 13 channels. A Graphics Processing Unit (GPU), also called a display core, a visual processor, and a display chip, is a microprocessor dedicated to image and Graphics related operations on a personal computer, a workstation, a game machine, and some mobile devices (such as a tablet pc and a smart phone). The GPU reduces the dependence of the graphics card on the CPU, and performs part of the original CPU work, and particularly, the core technologies adopted by the GPU in 3D graphics processing include hardware T & L (geometric transformation and illumination processing), cubic environment texture mapping and vertex mixing, texture compression and bump mapping, a dual-texture four-pixel 256-bit rendering engine, and the like, and the hardware T & L technology can be said to be a mark of the GPU. Manufacturers of GPUs have primarily NVIDIA and ATI.
Further, in the navigation satellite signal generation simulator, the digital signal generating unit 10 includes a digital carrier generating module, a digital signal processing module 11 and an interface communication module 12, wherein: the digital carrier generation module drives the phase accumulation of the digital carrier through a 1PPS signal of the external component 30, and then outputs the carrier through the digital carrier lookup table by taking the phase accumulation value as an address of the digital carrier lookup table; the digital signal processing module 11 is configured to generate a spreading code and a channel code of a digital baseband signal layer, generate a B1 frequency point navigation signal, a B2 frequency point navigation signal, and a B3 frequency point navigation signal, receive a navigation message generated by a navigation task processor, and modulate the navigation message onto a B1 frequency point navigation signal, a B2 frequency point navigation signal, and a B3 frequency point navigation signal; the interface communication module 12 is used for providing an interface for the digital signal processing module 11 to communicate with the outside.
As shown in fig. 2, in the navigation satellite signal generation simulator, the digital signal processing module 11 includes a precision ranging code, a C code generator, an amplitude mapper, a baseband shaping filter, and an anti-Sinc filter, wherein: the precision ranging code and the C code generator generate corresponding code streams under the control of the time frequency signal of the corresponding frequency point and the 1PPS signal of the external component 30, and after modulating to the navigation message of the corresponding channel, the code streams are converted into non-return-to-zero codes through the amplitude mapper, and the baseband shaping filter filters out high frequency components, modulates to the digital intermediate frequency signal, and after filtering through the anti-Sinc filter, outputs the digital intermediate frequency signal to the downlink signal radio frequency unit 20 through the interface communication module 12.
In addition, in the navigation satellite signal generation simulator, the downlink signal radio frequency unit 20 includes a DA conversion module 21, a modulation module 22, a digitally controlled attenuation module 23, and an isolator 24, where: the DA conversion module 21 converts the B1 frequency point navigation signal, the B2 frequency point navigation signal, and the B3 frequency point navigation signal into the analog intermediate frequency signal; the modulation module 22 is configured to complete frequency point analog orthogonal modulation of the B1 frequency point navigation signal, the B2 frequency point navigation signal, and the B3 frequency point navigation signal, and switch between a spread spectrum mode and a single carrier mode; the numerical control attenuation module 23 completes the output power control of the radio frequency signal; the isolator 24 is used to reduce the effect of back-end reflected signals on the front-end signal due to impedance mismatches. In the navigation satellite signal generation simulator, the number of the paths of the DA conversion module 21 is 4, the DA conversion value of each path is 16bit, and the rate of the DA conversion module is 500 MHz. The adjustable range of the numerical control attenuation module 23 is 8dB, and the stepping amplitude is 1 dB.
In the navigation satellite signal generation simulator provided by the invention, the digital signal generation unit 10 generates a digital intermediate frequency signal according to a time-frequency signal, the downlink signal radio frequency unit 20 converts the digital intermediate frequency signal into an analog intermediate frequency signal, and completes the up-conversion of the analog intermediate frequency signal and outputs a radio frequency navigation signal with corresponding power, so that the software of a digital baseband signal processing function is realized, the flexible and variable upgrading of a signal system, a signal format, a text arrangement, a modulation mode and the like is facilitated, the designability, the expansibility and the maintainability of a system are greatly enhanced, and the test verification of the system and key technology on the ground is facilitated.
Further, the GPU in the digital signal generating unit 10 generates digital baseband signals of the B1 frequency point navigation signal, the B2 frequency point navigation signal, and the B3 frequency point navigation signal simultaneously through streaming, so that the high-speed computing capability of the GPU can ensure the real-time performance of signal processing, and ensure the consistency of information reception with a real satellite and signal generation delay.
In addition, a corresponding code stream is generated by a precise ranging code and C code generator under the control of a 1PPS signal of an external component 30 and a time frequency signal of a corresponding frequency point, the code stream is modulated to a navigation message of a corresponding channel and then converted into a non-return-to-zero code by an amplitude mapper, a baseband forming filter filters a high-frequency component and then modulates the high-frequency component to a digital intermediate-frequency signal, fault troubleshooting and debugging are facilitated, a software-based digital baseband signal processing mode can output all processed intermediate state information, and an internal information interface can be completely opened for external output; the hardware function degradation is realized, so that the hardware state does not restrict the system upgrading, and the reconfigurable capability of information processing is improved.
Furthermore, the DA conversion module 21 converts the B1 frequency point navigation signal, the B2 frequency point navigation signal and the B3 frequency point navigation signal into analog intermediate frequency signals, the modulation module 22 completes frequency point analog orthogonal modulation of the B1 frequency point navigation signal, the B2 frequency point navigation signal and the B3 frequency point navigation signal, and the numerical control attenuation module 23 completes output power control of radio frequency signals, so that the capabilities of storing sampled data in real time and replaying the sampled data to the radio frequency signals offline are realized, and problem backtracking and troubleshooting are facilitated.
Finally, the chip sample-and-hold characteristic of the DA conversion module 21 causes the DA conversion module to have a Sinc filtering effect on the signal and suppress high-frequency components, thereby affecting the signal quality, so that the anti-Sinc filtering is performed before the digital baseband signal is output to the DA conversion module 21 to compensate the Sinc effect of the DA chip.
In summary, the above embodiments have described the different configurations of the navigation satellite signal generation simulator in detail, and it is needless to say that the present invention includes, but is not limited to, the configurations listed in the above embodiments, and any modifications based on the configurations provided in the above embodiments are within the scope of the present invention. One skilled in the art can take the contents of the above embodiments to take a counter-measure.
The above description is only for the purpose of describing the preferred embodiments of the present invention, and is not intended to limit the scope of the present invention, and any variations and modifications made by those skilled in the art based on the above disclosure are within the scope of the appended claims.
Claims (7)
1. A navigation satellite signal generation simulator, comprising a digital signal generation unit and a downlink signal radio frequency unit, wherein:
the digital signal generating unit is used for generating a digital intermediate frequency signal according to the time frequency signal; the downlink signal radio frequency unit is used for converting the digital intermediate frequency signal into an analog intermediate frequency signal, finishing up-conversion of the analog intermediate frequency signal and outputting a radio frequency navigation signal with corresponding power so as to simulate generation of a navigation satellite signal;
the digital intermediate frequency signals comprise B1 frequency point navigation signals, B2 frequency point navigation signals and B3 frequency point navigation signals;
the GPU in the digital signal generating unit simultaneously generates digital baseband signals of the B1 frequency point navigation signal, the B2 frequency point navigation signal and the B3 frequency point navigation signal;
the digital signal generating unit comprises a digital carrier generating module, a digital signal processing module and an interface communication module, wherein:
the digital carrier generation module drives the phase accumulation of the digital carrier through a 1PPS signal of an external component, and then takes the phase accumulation value as an address of a digital carrier lookup table to output the carrier through the digital carrier lookup table;
the digital signal processing module is used for generating a spread spectrum code and a channel code of a digital baseband signal layer, generating a B1 frequency point navigation signal, a B2 frequency point navigation signal and a B3 frequency point navigation signal, receiving a navigation message generated by a navigation task processor, and modulating the navigation message to a B1 frequency point navigation signal, a B2 frequency point navigation signal and a B3 frequency point navigation signal;
the interface communication module is used for providing an interface for the digital signal processing module to communicate with the outside.
2. The navigation satellite signal generation simulator of claim 1, wherein a high speed fiber optic connection is employed between said digital signal generating unit and said downlink signal radio frequency unit.
3. The navigation satellite signal generation simulator of claim 1, wherein the digital baseband signal is split into 13 channels.
4. The navigation satellite signal generation simulator of claim 1, wherein the digital signal processing module comprises a precision ranging code, a C-code generator, an amplitude mapper, a baseband shaping filter, and an anti-Sinc filter, wherein:
the precision ranging code and the C code generator generate corresponding code streams under the control of the 1PPS signals of the external components and the time frequency signals of corresponding frequency points, the code streams are modulated to navigation messages of corresponding channels and then converted into non-return-to-zero codes through the amplitude mapper, the baseband shaping filter filters high-frequency components, then the digital intermediate-frequency signals are modulated to the digital intermediate-frequency signals, and the digital intermediate-frequency signals are filtered through the anti-Sinc filter and then output to the downlink signal radio-frequency unit through the interface communication module.
5. The navigation satellite signal generation simulator of claim 4, wherein the downlink signal radio frequency unit comprises a DA conversion module, a modulation module, a digitally controlled attenuation module, and an isolator, wherein:
the DA conversion module converts the B1 frequency point navigation signal, the B2 frequency point navigation signal and the B3 frequency point navigation signal into the analog intermediate frequency signal;
the modulation module is used for completing frequency point analog orthogonal modulation of the B1 frequency point navigation signal, the B2 frequency point navigation signal and the B3 frequency point navigation signal and switching between a spread spectrum mode and a single carrier mode;
the numerical control attenuation module completes the output power control of the radio frequency signal;
the isolator is used for reducing the influence of the back-end reflected signal on the front-end signal caused by impedance mismatching.
6. The navigation satellite signal generation simulator of claim 5, wherein said DA conversion module has 4 paths, each path has a DA conversion value of 16bit, and the rate of the DA conversion module is 500 MHz.
7. The navigation satellite signal generation simulator of claim 5, wherein the digitally controlled attenuation module is adjustable in range of 8dB with a step size of 1 dB.
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| CN202010863991.1A CN112013875B (en) | 2019-11-27 | 2019-11-27 | Real-time navigation signal generation device based on GPU |
| CN201911179348.0A CN110824509B (en) | 2019-11-27 | 2019-11-27 | Navigation satellite signal generation simulator |
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| JP2004309307A (en) * | 2003-04-07 | 2004-11-04 | Hitachi Ltd | Satellite simulation system |
| US8406277B2 (en) * | 2005-12-16 | 2013-03-26 | Qualcomm Incorporated | Signal processor and signal processing method |
| CN101033974B (en) * | 2007-01-19 | 2010-05-19 | 北京东方联星科技有限公司 | Navigation satellite signal generating system based on software |
| US8378889B2 (en) * | 2008-08-08 | 2013-02-19 | 02Micro Inc | Calculating navigation system time in a satellite navigation system |
| CN101706580A (en) * | 2009-11-24 | 2010-05-12 | 北京航空航天大学 | PXIe bus based GNSS signal simulator and implementation method thereof |
| CN102096074B (en) * | 2010-11-22 | 2012-09-26 | 航天恒星科技有限公司 | Galileo search signal simulator |
| CN201936013U (en) * | 2010-12-31 | 2011-08-17 | 桂林电子科技大学 | Global position system (GPS) and global navigation satellite system (GLONASS) combined simulator |
| CN102375146A (en) * | 2011-09-23 | 2012-03-14 | 上海交通大学 | Method and system for simulating GPS (Global Positioning System) digital medium-frequency signal |
| CN104597462A (en) * | 2015-02-27 | 2015-05-06 | 南通航大电子科技有限公司 | GNSS (global navigation satellite system) signal simulator and implementing method thereof on basis of GPU (graphic processing unit) |
| CN106526624B (en) * | 2017-01-18 | 2023-08-15 | 桂林电子科技大学 | Satellite navigation signal simulator and simulation method thereof |
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