CN209545592U - Short message check-in signal Doppler frequency compensation control system under high dynamic - Google Patents

Short message check-in signal Doppler frequency compensation control system under high dynamic Download PDF

Info

Publication number
CN209545592U
CN209545592U CN201821202093.6U CN201821202093U CN209545592U CN 209545592 U CN209545592 U CN 209545592U CN 201821202093 U CN201821202093 U CN 201821202093U CN 209545592 U CN209545592 U CN 209545592U
Authority
CN
China
Prior art keywords
unit
inbound
signal
generates
short message
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
CN201821202093.6U
Other languages
Chinese (zh)
Inventor
杨棣
黎明
耿超
于彦伟
周倩
张向阳
熊国庆
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
SHAANXI LINGYUN TECHNOLOGY CO LTD
Original Assignee
SHAANXI LINGYUN TECHNOLOGY CO LTD
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by SHAANXI LINGYUN TECHNOLOGY CO LTD filed Critical SHAANXI LINGYUN TECHNOLOGY CO LTD
Priority to CN201821202093.6U priority Critical patent/CN209545592U/en
Application granted granted Critical
Publication of CN209545592U publication Critical patent/CN209545592U/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Abstract

The utility model discloses short message check-in signal Doppler frequency compensation control systems under a kind of high dynamic, including frequency word converting unit, frequency word converting unit generates unit with inbound pseudo-code respectively and inbound IF carrier generates unit and connect, the output that the inbound pseudo-code generates unit generates unit with inbound text again and connect, BPSK modulation unit is successively passed through in the output that inbound text generates the output of unit and inbound IF carrier generates unit, transmitting antenna is transmitted a signal to through up-conversion transmission channel after DAC unit and bandpass filtering unit, the utility model solves the problems, such as to cause inbound to fail due to the influence of Doppler shift when equipment short message inbound existing in the prior art.

Description

Short message check-in signal Doppler frequency compensation control system under high dynamic
Technical field
The utility model belongs to Beidou satellite navigation technology field, and in particular to short message check-in signal under a kind of high dynamic Doppler frequency compensation control system.
Background technique
The Beidou satellite navigation system of China's independent development is divided into RNSS business and RDSS business, and wherein RDSS business is whole Occupy critically important status in a system.It is mainly used for the fields such as ground rescue, data communication, monitoring position, in the military and people There is long-range application prospect with direction.
Under the high-speed applications environment of missile-borne, due to the needs of carrier practical application, Beidou terminal inside it is installed Equipment devises the short message transceiver module in RDSS, can complete the satellite intercommunication of carrier and ground command system.
Inbound communication, after being forwarded by overhead satellites, quilt are wherein emitted by the short message module in the terminal device on carrier Dipper system ground station reception;Emit by the parsing and judgement of earth station, then from earth station to overhead satellites, then by defending in the air It is received after star forwarding by ground command system.This completes the carrier information processes that command system transmits to the ground.
It completes to transmit information to bearer user machine in a like fashion on the contrary, ground command system can also be adopted.
Utility model content
The purpose of the utility model is to provide short message check-in signal Doppler frequency compensation control systems under a kind of high dynamic System causes inbound failure due to the influence of Doppler shift when solving equipment short message inbound existing in the prior art Problem.
The utility model is the technical scheme adopted is that short message check-in signal Doppler frequency compensation controls under high dynamic System, including frequency word converting unit, unit is generated with inbound pseudo-code respectively for frequency word converting unit and inbound IF carrier produces Raw unit connection, the output that the inbound pseudo-code generates unit generate unit with inbound text again and connect, and inbound text generates single BPSK modulation unit, DAC unit and bandpass filtering are successively passed through in the output that the output of member and inbound IF carrier generate unit Transmitting antenna is transmitted a signal to through up-conversion transmission channel after unit.
The utility model is also characterized by
Inbound pseudo-code generates the code Doppler frequency compensation value that unit is exported according to the frequency word converting unit, in addition The corresponding code clock reference frequency word of 4.08MHz, the code clock frequency word after obtaining transmitting Doppler frequency compensation, then by code Clock frequency word is input to numerically-controlled oscillator NCO, obtains a yard clock signal, and generate pseudo-code sequence using code generator.
Inbound text generate unit by inbound pseudo-code generate unit generate code clock signal through 255 frequency dividing after be converted into Information of standing text, inbound communication text are generated after the pseudo-code sequence that unit generates carries out XOR operation with the inbound pseudo-code and are inputted To BPSK modulation unit.
Inbound IF carrier generates the carrier Doppler frequency offset that unit is exported according to the frequency word converting unit, In addition the corresponding frequency word of IF frequency, the IF signal frequency word after obtaining transmitting Doppler frequency compensation, it then will be in this Frequency signal frequency word is input to carrier wave NCO, obtains emission medium-frequency signal, which is input to BPSK modulation unit.
The analog if signal that the DAC unit exports is carried out up-conversion, filtering and power and put by up-conversion transmission channel Greatly, transmitting antenna is given.
BPSK modulation unit generates the transmitting pseudo-code sequence of unit generation in transmitting in numeric field, using inbound pseudo-code The emission medium-frequency signal that frequency carrier-generation unit generates carries out BPSK modulation.
The intermediate-freuqncy signal with BPSK modulation that DAC unit exports BPSK modulation unit carries out digital-to-analogue conversion, and carries out Bandpass filtering obtains continuous analog if signal.
The utility model has the beneficial effects that short message check-in signal Doppler frequency compensation control system under high dynamic, The transmitting signal producing method of short message transceiver is adjusted, inbound pseudo-code generates unit and converts list according to the frequency word The code Doppler frequency compensation value of member output, in addition the corresponding code clock reference frequency word of 4.08MHz, obtains transmitting Doppler's frequency The compensated code clock frequency word of rate, is then input to numerically-controlled oscillator NCO for code clock frequency word, obtains a yard clock letter Number, and pseudo-code sequence is generated using code generator, while inbound text generates unit and inbound pseudo-code is generated the code that unit generates Clock signal is converted into inbound communication text after 255 frequency dividings, and inbound communication text and the inbound pseudo-code generate unit and generate Pseudo-code sequence carry out XOR operation after be input to BPSK modulation unit, with this solve the inbound as caused by Doppler shift lose Lose problem.
Detailed description of the invention
Fig. 1 is that short message check-in signal Doppler frequency compensation Control system architecture is illustrated under the utility model high dynamic Figure;
Fig. 2 is tested using short message check-in signal Doppler frequency compensation Control system simulation under the utility model high dynamic Card scheme composition schematic diagram.
In figure, 1. frequency word converting units, 2. inbound pseudo-codes generate unit, and 3. inbound IF carriers generate unit, and 4. enter Text of standing generates unit, 5.BPSK modulation unit, 6.DAC unit, 7. bandpass filtering units, 8. up-conversion transmission channels, 9. hairs Penetrate antenna, 10. numerically-controlled oscillator NCO, 11. carrier wave NCO, 12. yards of generators.
Specific embodiment
The utility model is described in detail with reference to the accompanying drawings and detailed description.
Short message check-in signal Doppler frequency compensation control system under the utility model high dynamic, structure as shown in Figure 1, Including frequency word converting unit 1, unit 2 is generated with inbound pseudo-code respectively for frequency word converting unit 1 and inbound IF carrier generates Unit 3 connects, and the output that inbound pseudo-code generates unit 2 generates unit 4 with inbound text again and connect, and inbound text generates unit 4 Output and inbound IF carrier generate unit 3 output successively pass through BPSK modulation unit 5, DAC unit 6 and bandpass filtering Transmitting antenna 9 is transmitted a signal to through up-conversion transmission channel 8 after unit 7.
Inbound pseudo-code generates the code Doppler frequency compensation value that unit 2 is exported according to the frequency word converting unit 1, in addition The corresponding code clock reference frequency word of 4.08MHz, the code clock frequency word after obtaining transmitting Doppler frequency compensation, then by code Clock frequency word is input to numerically-controlled oscillator NCO10, obtains a yard clock signal, and generate pseudo-code sequence using code generator 12 Column.
Inbound text generates unit 4 and converts the code clock signal that inbound pseudo-code generation unit 2 generates to after 255 frequency dividings After inbound communication text, inbound communication text and the inbound pseudo-code generate the pseudo-code sequence progress XOR operation that unit 2 generates It is input to the BPSK modulation unit 5.
Inbound IF carrier generates unit 3 and is compensated according to the carrier Doppler frequency that the frequency word converting unit 1 exports Value, in addition the corresponding frequency word of IF frequency, the IF signal frequency word after obtaining transmitting Doppler frequency compensation, then should IF signal frequency word is input to carrier wave NCO11, obtains emission medium-frequency signal, which is input to the BPSK tune Unit 5 processed.
The analog if signal that up-conversion transmission channel 8 exports DAC unit 6 carries out up-conversion, filtering and power amplification, Give transmitting antenna 9.
BPSK modulation unit 5 generates the transmitting pseudo-code sequence of the generation of unit 2 to described in numeric field, using inbound pseudo-code The emission medium-frequency signal that emission medium-frequency carrier-generation unit 3 generates carries out BPSK modulation.
The intermediate-freuqncy signal with BPSK modulation that DAC unit 6 exports BPSK modulation unit 5 carries out digital-to-analogue conversion, goes forward side by side Row bandpass filtering obtains continuous analog if signal.
The utility model is by multi-party coordination and discusses, determines the high dynamic multi-beam north developed using University of Science and Technology for National Defence The two generation RDSS simulators that struggle against are verified, and can use channel simulator realization to the working performance of high dynamic short message transceiver Verifying, as shown in Figure 2:
RDSS signal imitation source: capture, tracking and the data demodulation of the main simulation for completing exit signal and check-in signal. Wherein, exit signal is dynamically simulated and (is dynamically completed by channel simulator) without carrier, and check-in signal receives processing unit Doppler range be configured according to the actual parameter of real system earth station inbound receiver, can just test in this way Whether the Doppler Compensation Method for demonstrate,proving short message transceiver is effective.
High dynamic channel simulator: it is mainly made of, has distinguished outbound channel analogue unit and inbound channel analogue unit The distance of pairs of exit signal and check-in signal, speed simulation.
The specific course of work is as follows:
Step 1 generates unit generation exit signal first with the exit signal in RDSS signal imitation source, which is to defend Star emits the signal at output port, does not consider signal dynamics effect;
Step 2, the outbound channel analogue unit that above-mentioned signal is given to high dynamic channel simulator are realized to carrier movement Simulation, including distance, speed, channel parameter etc.;
The high dynamic signal that step 3, high dynamic short message transceiver to channel simulator export is generated with how general The inbound for strangling frequency meter precompensation emits signal, and gives the inbound channel analogue unit of signal simulator;
The inbound channel analogue unit reception of step 4, channel simulator is with the inbound hair of Doppler frequency table precompensation Signal is penetrated, realizes simulation, including distance, speed, channel parameter etc. to inbound channel, and will be by entering after inbound channel The check-in signal that signal of standing gives signal imitation source receives processing unit, realizes to the capture of check-in signal, tracking and data solution It adjusts;
If the check-in signal that the inbound channel analogue unit of step 5, channel simulator receives is consistent with default scene, Then prove that the check-in signal Doppler frequency precompensation method of short message transceiver is effective.

Claims (4)

1. short message check-in signal Doppler frequency compensation control system under high dynamic, which is characterized in that converted including frequency word Unit (1), frequency word converting unit (1) generates unit (2) with inbound pseudo-code respectively and inbound IF carrier generates unit (3) even It connects, the output that the inbound pseudo-code generates unit (2) generates unit (4) with inbound text again and connect, and inbound text generates unit (4) output that output and inbound IF carrier generate unit (3) successively pass through BPSK modulation unit (5), DAC unit (6) with And bandpass filtering unit (7) transmits a signal to transmitting antenna (9) by up-conversion transmission channel (8).
2. short message check-in signal Doppler frequency compensation control system, feature under high dynamic according to claim 1 Be, the analog if signal that the up-conversion transmission channel (8) exports the DAC unit (6) carry out up-conversion, filtering and Transmitting antenna (9) are given in power amplification.
3. short message check-in signal Doppler frequency compensation control system, feature under high dynamic according to claim 1 It is, the BPSK modulation unit (5) generates the transmitting pseudo-code that unit (2) generate in numeric field, using the inbound pseudo-code Sequence generates the emission medium-frequency signal that unit (3) generate to the inbound IF carrier and carries out BPSK modulation.
4. short message check-in signal Doppler frequency compensation control system, feature under high dynamic according to claim 1 It is, the intermediate-freuqncy signal modulated with BPSK that the DAC unit (6) exports the BPSK modulation unit (5) carries out digital-to-analogue Conversion, and bandpass filtering is carried out, obtain continuous analog if signal.
CN201821202093.6U 2018-07-26 2018-07-26 Short message check-in signal Doppler frequency compensation control system under high dynamic Active CN209545592U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201821202093.6U CN209545592U (en) 2018-07-26 2018-07-26 Short message check-in signal Doppler frequency compensation control system under high dynamic

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201821202093.6U CN209545592U (en) 2018-07-26 2018-07-26 Short message check-in signal Doppler frequency compensation control system under high dynamic

Publications (1)

Publication Number Publication Date
CN209545592U true CN209545592U (en) 2019-10-25

Family

ID=68244388

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201821202093.6U Active CN209545592U (en) 2018-07-26 2018-07-26 Short message check-in signal Doppler frequency compensation control system under high dynamic

Country Status (1)

Country Link
CN (1) CN209545592U (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113422642A (en) * 2021-08-25 2021-09-21 长沙海格北斗信息技术有限公司 Beidou third-number global short message sending method under high-speed dynamic environment
CN113422640A (en) * 2021-08-24 2021-09-21 长沙海格北斗信息技术有限公司 Beidou third RDSS area long message sending method under high-speed dynamic environment
WO2022077390A1 (en) * 2020-10-15 2022-04-21 华为技术有限公司 Satellite signal processing method and satellite positioning apparatus
CN115051745A (en) * 2022-05-09 2022-09-13 中国电子科技集团公司第二十九研究所 Beidou short message inbound signal dynamic compensation method and device of high-speed spacecraft
CN116840859A (en) * 2023-07-05 2023-10-03 中国人民解放军92728部队 Satellite navigation receiver channel maintaining method based on dynamic estimation

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2022077390A1 (en) * 2020-10-15 2022-04-21 华为技术有限公司 Satellite signal processing method and satellite positioning apparatus
CN113422640A (en) * 2021-08-24 2021-09-21 长沙海格北斗信息技术有限公司 Beidou third RDSS area long message sending method under high-speed dynamic environment
CN113422642A (en) * 2021-08-25 2021-09-21 长沙海格北斗信息技术有限公司 Beidou third-number global short message sending method under high-speed dynamic environment
CN115051745A (en) * 2022-05-09 2022-09-13 中国电子科技集团公司第二十九研究所 Beidou short message inbound signal dynamic compensation method and device of high-speed spacecraft
CN115051745B (en) * 2022-05-09 2024-01-26 中国电子科技集团公司第二十九研究所 Beidou short message inbound signal dynamic compensation method and device for high-speed spacecraft
CN116840859A (en) * 2023-07-05 2023-10-03 中国人民解放军92728部队 Satellite navigation receiver channel maintaining method based on dynamic estimation
CN116840859B (en) * 2023-07-05 2024-02-09 中国人民解放军92728部队 Satellite navigation receiver channel maintaining method based on dynamic estimation

Similar Documents

Publication Publication Date Title
CN209545592U (en) Short message check-in signal Doppler frequency compensation control system under high dynamic
CN107911160A (en) Beidou satellite navigation signal large-scale parallel real-time Transmission method and system
CN107017940A (en) Unmanned plane repeat broadcast communication system route optimization method
CN102752012A (en) Air vehicle measurement and control system with upper and down links utilizing different spectrum spreading systems
CN108737088A (en) A kind of free space laser communication system based on quantum cryptography
CN114157346A (en) Cooperative backscattering covert communication system and communication method
CN102830389A (en) PXI synthetic instrument based microwave landing simulator
CN105099588A (en) Device and method for simulating interference propagation channel of aviation communication system
CN110674584B (en) Multi-aircraft joint simulation system
CN106506038A (en) A kind of telemetry communication implementation method under the unified signal model based on UQPSK
CN109217914A (en) A kind of electromagnetic wave data transmission rule and system
CN104702350B (en) A kind of radio ranging system in aviation wireless communication system
CN102778671A (en) Radar target simulation method based on correction network
CN202502248U (en) Satellite navigation system based on return communication signal system
CN102608635B (en) Method and system for implementing satellite navigation on basis of return communication signal system
Anzagira et al. Non-orthogonal multiple access (NOMA) for LED-based visible light inter-satellite communications
CN107632293A (en) Weather radar intensity scale efficacious prescriptions method
CN113891286A (en) Secret communication performance optimization device and method for unmanned aerial vehicle auxiliary communication system
CN115549784A (en) Unmanned aerial vehicle group land-air and air-air communication system and communication method
CN107395268A (en) A kind of telemetry communication method and system based on chaos system
CN108391228A (en) A kind of positioning device based on TC-OFDM technologies
CN202794546U (en) Global position system (GPS) velocimeter
Yao To Improve the Real-Time Performance of Airborne Data Link Communication System
Hengbo et al. Key technologies of high speed modulator for satellite data transmission
CN112437029B (en) High-mobility large-dynamic reliable transmission verification device

Legal Events

Date Code Title Description
GR01 Patent grant
GR01 Patent grant