CN103227722B - For the HVDC Modulation power supply ofdm communication system of unmanned plane - Google Patents

For the HVDC Modulation power supply ofdm communication system of unmanned plane Download PDF

Info

Publication number
CN103227722B
CN103227722B CN201310088238.XA CN201310088238A CN103227722B CN 103227722 B CN103227722 B CN 103227722B CN 201310088238 A CN201310088238 A CN 201310088238A CN 103227722 B CN103227722 B CN 103227722B
Authority
CN
China
Prior art keywords
signal
power supply
conversion
ofdm
hvdc modulation
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.)
Expired - Fee Related
Application number
CN201310088238.XA
Other languages
Chinese (zh)
Other versions
CN103227722A (en
Inventor
樊邦奎
王守杰
闫敦豹
赵炳爱
聂志彪
朱剑佑
马静谨
张瑞雨
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.)
BEIJING INSTITUTE OF INFORMATION TECHNOLOGY
Original Assignee
BEIJING INSTITUTE OF INFORMATION TECHNOLOGY
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 BEIJING INSTITUTE OF INFORMATION TECHNOLOGY filed Critical BEIJING INSTITUTE OF INFORMATION TECHNOLOGY
Priority to CN201310088238.XA priority Critical patent/CN103227722B/en
Publication of CN103227722A publication Critical patent/CN103227722A/en
Application granted granted Critical
Publication of CN103227722B publication Critical patent/CN103227722B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Transmitters (AREA)
  • Amplifiers (AREA)

Abstract

The present invention relates to a kind of HVDC Modulation power supply ofdm communication system for unmanned plane, belong to radio communication technology field.Described system comprises transmitter and receiver, described transmitter comprises: the prediction of exciter, amplitude decision device, encoder, HVDC Modulation power supply, final power amplifier, output filter and transmitting antenna, wherein, the instantaneous amplitude of the signal that exciter will send by amplitude prediction decision device and set point compare, and send comparative result to encoder; Encoder compared result is carried out coding and is formed binary code, and HVDC Modulation power supply provides electric energy according to binary code to final power amplifier, and final power amplifier is used for carrying out power amplification to the signal that exciter will send; Output filter is used for mating with the input impedance of transmitting antenna the output impedance of final power amplifier; Transmitting antenna is used for the signal of telecommunication being become magnetic signal and being transmitted into space.Described HVDC Modulation power supply ofdm communication system can improve the power-efficient of unmanned plane.

Description

For the HVDC Modulation power supply ofdm communication system of unmanned plane
Technical field
The present invention relates to a kind of HVDC Modulation power supply ofdm communication system for unmanned plane, particularly relate to the HVDC Modulation power supply ofdm communication system for unmanned plane that a kind of power-efficient is high, belong to radio communication technology field.
Background technology
Unmanned plane is a kind of based on the not manned aircraft of wireless remotecontrol or self program control.The features such as compared with manned aircraft, it has, and volume is little, cost is low, easy to use, low to do station environmental requirement, battlefield survival is stronger.In modern war, unmanned plane can go deep into forward position, position and one or two hundred kilometers, enemy's rear area and carry out reconnaissance and surveillance to enemy's situation, can as deceiving enemy's bait, interference is implemented to enemy, enemy is attacked, can also communication repeating be carried out, but, unmanned plane needs electric energy when completing its task, if electric energy is once use up, its serving as of task just cannot complete.
Fig. 1 provides the oscillogram of electric energy when being the final power amplifier amplifying signal provided in prior art.As shown in Figure 1, in order to make the u that transmits fdistortionlessly transmitted by wireless channel, need the supply voltage value E provided to be greater than transmitted maximum amplitude at final power amplifying stage, so, most of energy has been consumed by the form with heat energy.And to OFDM (OrthogonalFrequencyDivisionMultiplexing OFDM) system, the peak-to-average ratio of signal is very high, the amplitude com parison of major part signal is low, and only have the Amplitude Ratio of minimum a part of signal larger, and adopt method of supplying power to of the prior art, be fixed the power supply of voltage or electric current to final stage power amplifier, the utilance of power supply is extremely low.
Summary of the invention
For overcoming the shortcoming existed in prior art, goal of the invention of the present invention is to provide a kind of HVDC Modulation power supply ofdm communication system for unmanned plane, and its power utilization rate is high, can reach more than 80%.
For realizing described goal of the invention, the invention provides a kind of HVDC Modulation power supply ofdm communication system for unmanned plane, it comprises transmitter and receiver, described transmitter comprises: exciter, amplitude prediction decision device, encoder, HVDC Modulation power supply, signal for sending exciter carries out the final power amplifier of power amplification, for the output filter that mates with the input impedance of transmitting antenna the output impedance of final power amplifier with for the signal of telecommunication amplified through final power being become magnetic signal and being transmitted into the transmitting antenna in space, described receiver comprises: for space magnetic signal being become the reception antenna of the signal of telecommunication, the signal of telecommunication for being received by reception antenna carries out the small signal amplifier amplified, local oscillation signal for small signal amplifier institute's amplifying signal and the first oscillator at the corresponding levels being produced carries out the first frequency mixer that down-conversion forms intermediate-freuqncy signal, the A-D converter of data-signal is formed for intermediate-freuqncy signal being carried out analog to digital conversion, for removing the time interval in data-signal, then carry out serial to parallel conversion successively, FFT conversion and the ofdm demodulator of parallel serial conversion and the signal for being exported by ofdm demodulator carry out the symbol inverse mapper of symbol inverse mapping, it is characterized in that, the instantaneous amplitude of the signal that exciter will send by amplitude prediction decision device and set point compare, and send comparative result to encoder, encoder compared result is carried out coding and is formed binary code, and HVDC Modulation power supply provides electric energy according to binary code to final power amplifier, described HVDC Modulation power supply comprises n level DC voltage unit, each DC voltage unit is by the cascade of afterflow coil, each DC voltage unit comprises a battery pack, fly-wheel diode, an electronic switch and a driving stage, and the positive pole of battery pack is connected to the negative pole of fly-wheel diode, the positive pole of fly-wheel diode is connected to the first end of electronic switch, second end of electronic switch is connected to the negative pole of battery pack, the control end of electronic switch is connected to driving stage, the binary code that driving stage provides according to encoder controls the break-make of electronic switch, described n be greater than or equal to 2 integer.
Preferably, exciter comprises symbol mapper, OFDM modulation device, D/A translation circuit, second frequency mixer, second oscillator at the corresponding levels and prime amplifier, wherein, symbol mapper is used for inputted serial binary code stream being carried out grouping and forms data symbol and data symbol is mapped to complex data data sequence, OFDM modulation device is for being modulated to N number of subcarrier by institute's complex data data sequence serial to parallel conversion, then carry out IFFT conversion and form parallel time domain data, namely parallel OFDM symbol, described parallel time domain data is carried out the OFDM symbol that parallel serial conversion forms serial, between the OFDM symbol of each serial, then insert the OFDM symbol data flow inserting guard time interval of guard time gap-forming serial, data flow is carried out digital-to-analogue conversion and is formed analog signal u by D/A translation circuit i, second frequency mixer is used for analog signal u ithe local oscillation signal u produced with the second oscillator at the corresponding levels 0carry out up-conversion and form signal u to be sent h, prime amplifier is to sent signal u hcarry out amplifying and give final power amplifier and carry out power amplification.
Compared with prior art, the HVDC Modulation power supply ofdm communication system for unmanned plane provided by the invention, can bring up to 60% by power utilization rate.
Accompanying drawing explanation
Fig. 1 provides the oscillogram of electric energy when being the final power amplifier amplifying signal provided in prior art;
Fig. 2 is the composition frame chart of the HVDC Modulation power supply ofdm communication system for unmanned plane provided by the invention;
Fig. 3 is the composition frame chart of HVDC Modulation power supply provided by the invention.
Fig. 4 provides the oscillogram of electric energy when being final power amplifier amplifying signal provided by the invention.
Embodiment
Below in conjunction with accompanying drawing, describe the present invention in detail.
Fig. 2 is the composition frame chart of the HVDC Modulation power supply ofdm communication system for unmanned plane provided by the invention.As shown in Figure 2, the invention provides a kind of HVDC Modulation power supply ofdm communication system for unmanned plane, it comprises transmitter and receiver, described transmitter comprises: exciter, amplitude prediction decision device, encoder, HVDC Modulation power supply, signal for sending exciter carries out the final power amplifier of power amplification, for the output filter that mates with the input impedance of transmitting antenna the output impedance of final power amplifier with for the signal of telecommunication amplified through final power being become magnetic signal and being transmitted into the transmitting antenna in space, described receiver comprises: for space magnetic signal being become the reception antenna of the signal of telecommunication, the signal of telecommunication for being received by reception antenna carries out the small signal amplifier amplified, local oscillation signal for small signal amplifier institute's amplifying signal and the first oscillator at the corresponding levels being produced carries out the first frequency mixer that down-conversion forms intermediate-freuqncy signal, the A-D converter of data-signal is formed for intermediate-freuqncy signal being carried out analog to digital conversion, for removing the time interval in data-signal, then carry out serial to parallel conversion successively, FFT conversion and the ofdm demodulator of parallel serial conversion and the signal for being exported by ofdm demodulator carry out the symbol inverse mapper of symbol inverse mapping.Exciter comprises symbol mapper, OFDM modulation device, D/A translation circuit, frequency mixer, oscillator at the corresponding levels and prime amplifier, wherein, symbol mapper is used for inputted serial binary code stream being carried out grouping and forms data symbol and data symbol is mapped to complex data sequence, OFDM modulation device is for carrying out serial to parallel conversion by complex data sequence and being modulated to K subcarrier, and the data on K subcarrier are designated as X 0, X 0..., X k-1; Then carry out IFFT conversion and form parallel time domain data x 0, x 1..., x k-1, i.e. x 0, x 1..., x k-1be an OFDM symbol, described parallel time domain data carried out the OFDM symbol that parallel serial conversion forms serial, then between each OFDM symbol, insert guard time gap-forming OFDM symbol; Data flow is carried out digital-to-analogue conversion and is formed analog signal u by D/A translation circuit i; Second frequency mixer is used for analog signal u ithe local oscillation signal u produced with the second oscillator at the corresponding levels 0carry out up-conversion and form signal u to be sent h, prime amplifier is to sent signal u hcarry out amplifying and give final power amplifier and carry out power amplification.Amplitude prediction decision device is to x 0, x 0..., x k-1amplitude successively with n set point A t1, set point A t1..., set point A tn(wherein, A t1< A t1< ..., < A tn) compare, and sending comparative result to encoder, encoder carries out coding according to comparative result and forms binary code, and HVDC Modulation power supply provides electric energy according to binary code to final stage power amplifier.Undistorted for ensureing signal, usually, set point A tnbe greater than the maximum of data in all OFDM symbol.
Still as shown in Figure 2, carry out grouping form data symbol at the binary code stream of transmitting terminal input, data symbol maps through symbol mapper and forms complex data sequence, forms the low rate data streams X that K bar is parallel after complex data sequence serial to parallel conversion 0, X 0..., X k-1; The sample value that IFFT conversion obtains time domain is carried out to it:
x k = &Sigma; m = 0 K = 1 X m e i 2 &pi;nk / K
Wherein, m is the discrete point of frequency domain, and k is the discrete point of time domain.
At receiving terminal, the signal removing guard time interval is y through the time domain data that serial to parallel conversion is formed 0, y 1..., y k-1, the value that FFT conversion obtains frequency domain is carried out to it:
Y m = &Sigma; k = 0 K = 1 y k e - i 2 &pi;nk / K .
Fig. 3 is that direct current provided by the invention can the composition frame chart of modulation power source.As shown in Figure 3, described HVDC Modulation power supply comprises n optical transmitting set OT 0, OT 1, OT 2and OT n, N=n-1, n optical receiver OR 0, OR 1, OR 2and OR nwith n level direct current component, each DC voltage unit by the cascade of afterflow coil, described n be greater than or equal to 2 integer.Described optical transmitting set the binary control signal that encoder exports is converted to light signal with by Optical Fiber Transmission to corresponding optical receiver.Described optical receiver receives corresponding optical transmitting set and launches the light signal of coming, and the light signal of reception is converted to the signal of telecommunication that controls driving stage realizes being in DC voltage unit at different levels on suspended voltage and low level control part high-voltage isolating with this.
First DC voltage unit M 0comprise a battery pack U 0, a sustained diode 0, electronic switch and a driving stage P 0, electronic switch is CMOS tube CMOS 0, described battery pack U 0positive pole be connected to sustained diode 0negative pole; Sustained diode 0positive pole be connected to CMOS tube CMOS 0drain electrode, CMOS tube CMOS 0source electrode be connected to described battery pack U 0negative pole, CMOS tube CMOS 0grid be connected to driving stage P 0, driving stage P 0according to optical receiver OR 0the binary system control command that the encoder received sends controls CMOS tube CMOS 0break-make.CMOS tube CMOS 0work on off state, as CMOS tube CMOS 0grid when inputting a high potential, CMOS tube CMOS 0conducting, battery pack U 0negative pole be equivalent to receive sustained diode 0positive pole.Sustained diode 0the voltage at two ends is U 0, upper end is just, lower end is negative.As CMOS tube CMOS 0grid when inputting an electronegative potential, CMOS tube CMOS 0cut-off.Sustained diode 0the voltage at two ends is diode junction voltage.
In like manner, second DC voltage unit M 1comprise a battery pack U 1, a rectifier R 1, a sustained diode 1, electronic switch and a driving stage P 1, electronic switch is CMOS tube CMOS 1, described battery pack U 1positive pole be connected to and be connected to sustained diode 1negative pole; Sustained diode 1positive pole be connected to CMOS tube CMOS 1drain electrode, CMOS tube CMOS 1source electrode battery pack U 1negative pole, CMOS tube CMOS 1grid be connected to driving stage P 1, by driving stage P 1according to optical receiver OR 1the binary system control command that the encoder received sends controls CMOS tube CMOS 1break-make.CMOS tube CMOS 1work on off state, as CMOS tube CMOS 1grid when inputting a high potential, CMOS tube CMOS 1conducting, battery pack U 1negative pole be equivalent to receive sustained diode 1positive pole.Sustained diode 1the voltage at two ends is U 1, upper end is just, lower end is negative.As CMOS tube CMOS 1grid when inputting an electronegative potential, CMOS tube CMOS 1cut-off.Sustained diode 1the voltage at two ends is diode junction voltage.
3rd DC voltage unit M 2comprise a battery pack U 2, a rectifier R 2, a sustained diode 2, electronic switch and a driving stage P 2, electronic switch is CMOS tube CMOS 2, described battery pack U 2, positive pole be connected to the negative pole of fly-wheel diode; Sustained diode 2positive pole be connected to CMOS tube CMOS 2drain electrode, CMOS tube CMOS 2source electrode be connected to battery pack U 2negative pole, CMOS tube CMOS 2grid be connected to driving stage P 2, by driving stage P 2according to optical receiver OR 2the binary system control command that the encoder received sends controls CMOS tube CMOS 2break-make.CMOS tube CMOS 2work on off state, as CMOS tube CMOS 2grid when inputting a high potential, CMOS tube CMOS 2conducting, battery pack U 2negative pole be equivalent to receive sustained diode 2positive pole.Sustained diode 2the voltage at two ends is U 2, upper end is just, lower end is negative.As CMOS tube CMOS 2grid when inputting an electronegative potential, CMOS tube CMOS 2cut-off.Sustained diode 2the voltage at two ends is diode junction voltage.
The like, the n-th DC voltage unit M ncomprise a battery pack U n, a rectifier R n, a sustained diode n, electronic switch and a driving stage P n, electronic switch is CMOS tube CMOS n, described battery pack U npositive pole be connected to the negative pole of fly-wheel diode; Sustained diode npositive pole be connected to CMOS tube CMOS ndrain electrode, CMOS tube CMOS nsource electrode be connected to battery pack U nnegative pole, CMOS tube CMOS ngrid be connected to driving stage P n, by driving stage P naccording to optical receiver OR nthe binary system control command that the encoder received sends controls CMOS tube CMOS nbreak-make.Metal-oxide-semiconductor CMOS nwork on off state, as CMOS tube CMOS ngrid when inputting a high potential, CMOS tube CMOS nconducting, battery pack U nnegative pole when in receiving sustained diode npositive pole.Sustained diode nthe voltage at two ends is U n, upper end is just, lower end is negative.As CMOS tube CMOS ngrid when inputting an electronegative potential, CMOS tube CMOS ncut-off, sustained diode nthe voltage at two ends is diode junction voltage.
1st DC voltage unit M 0with the 2nd DC voltage unit M 1between with afterflow coil L 01be connected, i.e. afterflow coil L 01be connected to sustained diode 0negative pole and sustained diode 1positive pole between; 2nd DC voltage unit M 1with the 3rd DC voltage unit M 2between with afterflow coil L 12be connected, i.e. afterflow coil L 12be connected to sustained diode 1negative pole and sustained diode 2positive pole between; The like, the 3rd DC voltage unit M 2with the 4th DC voltage unit M 3between with afterflow coil L 23be connected.So, if each DC voltage unit M 0, M 1, M 2... and M nelectronic switch conducting all simultaneously when, the total output total voltage of HVDC Modulation power supply is U always=U 0+ U 1+ U 2+ ... + U n.The magnitude of voltage that in the present invention, each DC voltage unit exports is identical, then total output voltage U always=nU 0
In the present invention, amplitude prediction decision device is successively by x kamplitude and each A t1, A t2... and A tncompare, if x kamplitude be less than A t1, encoder exports a corresponding binary code, the electronic switch conducting of a DC voltage unit, and the electronic switch cut-off of other DC voltage unit, HVDC Modulation power supply is U to the power supply that final stage power amplifier provides always=U 0; If x kamplitude be greater than or equal to A t1and be less than A t2, encoder exports a corresponding binary code, the electronic switch conducting of two DC voltage units, the cut-off of the electronic switch of other DC voltage unit, and the total output total voltage of HVDC Modulation power supply is U always=2U 0; If x kamplitude be greater than or equal to A tn-1and be less than A tn, encoder exports a corresponding binary code, all DC voltage unit M 0, M 1, M 2... and M nthe equal conducting of electronic switch, HVDC Modulation power supply is U to the total voltage that final stage power amplifier provides always=nU 0.
Fig. 4 provides the oscillogram of electric energy when being final power amplifier amplifying signal provided by the invention.As shown in Figure 4, as the signal u that will launch famplitude large time, the electronic switch that can make each DC voltage unit conducting all simultaneously, the power supply U provided alwaysfor each power supply sum.As the signal u that will launch famplitude hour, partial power conducting can be made, the power supply U provided alwaysfor each DC voltage unit sum of conducting, that is, the voltage provided is little, so, just improves the utilance of power supply.
Although below done to elaborate to the present invention by reference to the accompanying drawings, it should be recognized by those skilled in the art that under the prerequisite not departing from the present invention's design, any improvement of making based on the present invention and convert the content still belonged in scope.

Claims (3)

1. the HVDC Modulation power supply ofdm communication system for unmanned plane, it comprises transmitter and receiver, described transmitter comprises: exciter, amplitude prediction decision device, encoder, HVDC Modulation power supply, signal for sending exciter carries out the final power amplifier of power amplification, for the output filter that mates with the input impedance of transmitting antenna the output impedance of final power amplifier with for the signal of telecommunication amplified through final power being become magnetic signal and being transmitted into the transmitting antenna in space, described receiver comprises: for space magnetic signal being become the reception antenna of the signal of telecommunication, the signal of telecommunication for being received by reception antenna carries out the small signal amplifier amplified, local oscillation signal for small signal amplifier institute's amplifying signal and the first oscillator at the corresponding levels being produced carries out the first frequency mixer that down-conversion forms intermediate-freuqncy signal, the A-D converter of data-signal is formed for intermediate-freuqncy signal being carried out analog to digital conversion, for removing the guard time interval in data-signal, then carry out serial to parallel conversion successively, FFT conversion and the ofdm demodulator of parallel serial conversion and the signal for being exported by ofdm demodulator carry out the symbol inverse mapper of symbol inverse mapping, it is characterized in that, the instantaneous amplitude of the signal that exciter will send by amplitude prediction decision device and set point compare, and send comparative result to encoder, encoder compared result is carried out coding and is formed binary code, and HVDC Modulation power supply provides electric energy according to binary code to final power amplifier, described HVDC Modulation power supply comprises n level DC voltage unit, each DC voltage unit is by the cascade of afterflow coil, each DC voltage unit comprises a battery pack, fly-wheel diode, an electronic switch and a driving stage, and the positive pole of battery pack is connected to the negative pole of fly-wheel diode, the positive pole of fly-wheel diode is connected to the first end of electronic switch, second end of electronic switch is connected to the negative pole of battery pack, the control end of electronic switch is connected to driving stage, the binary code that driving stage provides according to encoder controls the break-make of electronic switch, described n be greater than or equal to 2 integer.
2. the HVDC Modulation power supply ofdm communication system for unmanned plane according to claim 1, it is characterized in that, exciter comprises symbol mapper, OFDM modulation device, D/A translation circuit, second frequency mixer, second oscillator at the corresponding levels and prime amplifier, wherein, symbol mapper is used for the serial binary code stream of input being carried out grouping and forms data symbol and data symbol is mapped to complex data sequence, OFDM modulation device is for being modulated to N number of subcarrier by complex data sequence serial to parallel conversion, then carry out IFFT conversion and form parallel time domain data, namely parallel OFDM symbol, described parallel time domain data is carried out the OFDM symbol that parallel serial conversion forms serial, between the OFDM symbol of each serial, then insert the OFDM symbol data flow inserting guard time interval of guard time gap-forming serial, data flow is carried out digital-to-analogue conversion and is formed analog signal u by D/A translation circuit i, second frequency mixer is used for analog signal u ithe local oscillation signal u produced with the second oscillator at the corresponding levels 0carry out up-conversion and form signal u to be sent h, prime amplifier is to sent signal u hcarry out amplifying and give final power amplifier and carry out power amplification.
3. the HVDC Modulation power supply ofdm communication system for unmanned plane according to any one of claim 1 to 2, it is characterized in that, described battery pack is solar battery group.
CN201310088238.XA 2013-03-20 2013-03-20 For the HVDC Modulation power supply ofdm communication system of unmanned plane Expired - Fee Related CN103227722B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201310088238.XA CN103227722B (en) 2013-03-20 2013-03-20 For the HVDC Modulation power supply ofdm communication system of unmanned plane

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201310088238.XA CN103227722B (en) 2013-03-20 2013-03-20 For the HVDC Modulation power supply ofdm communication system of unmanned plane

Publications (2)

Publication Number Publication Date
CN103227722A CN103227722A (en) 2013-07-31
CN103227722B true CN103227722B (en) 2016-04-06

Family

ID=48837992

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201310088238.XA Expired - Fee Related CN103227722B (en) 2013-03-20 2013-03-20 For the HVDC Modulation power supply ofdm communication system of unmanned plane

Country Status (1)

Country Link
CN (1) CN103227722B (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105048546B (en) * 2015-07-13 2018-02-27 国鹰航空科技有限公司 Photovoltaic modulation power source communication system for unmanned plane
CN105664503A (en) * 2016-03-16 2016-06-15 中山大学 Unmanned aerial vehicle device based on multiplayer remote control and implementing method
CN109361423B (en) * 2018-09-03 2020-03-03 中国科学院声学研究所 Underwater communication method under long-delay multipath condition
CN109959831A (en) * 2019-04-17 2019-07-02 成都航空职业技术学院 A kind of laboratory simulation unmanned plane power-supply system
CN111683031B (en) * 2020-05-13 2021-08-20 上海交通大学 Method and system for controlling backscattering circuit based on multi-subcarrier modulation

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101035104A (en) * 2006-03-06 2007-09-12 华为技术有限公司 Spread spectrum orthogonal frequency division multiplexing mixing system
CN102323568A (en) * 2011-06-17 2012-01-18 武汉中原电子集团有限公司 Radar responding device

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6334219B1 (en) * 1994-09-26 2001-12-25 Adc Telecommunications Inc. Channel selection for a hybrid fiber coax network

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101035104A (en) * 2006-03-06 2007-09-12 华为技术有限公司 Spread spectrum orthogonal frequency division multiplexing mixing system
CN102323568A (en) * 2011-06-17 2012-01-18 武汉中原电子集团有限公司 Radar responding device

Also Published As

Publication number Publication date
CN103227722A (en) 2013-07-31

Similar Documents

Publication Publication Date Title
CN103227722B (en) For the HVDC Modulation power supply ofdm communication system of unmanned plane
CN102474303B (en) Power line communications apparatus
CN102143110A (en) Digital modulator and digital-to-analog conversion techniques associated therewith
CN101359933B (en) Dc line carrier communication device
CN103227649B (en) OFDM (orthogonal frequency division multiplexing) transmitter provided with direct current modulation power supply of unmanned aerial vehicle
CN104753604A (en) Optical Communication System, Method For Controlling Optical Communication, And Optical Transmitter
CN102045091A (en) Short range data transmission device and method based on electromagnetic induction
CN108629959B (en) Remote control underwater acoustic communication system and unmanned underwater vehicle
CN206962545U (en) Radio energy transmission system
CN103219874B (en) Direct-current modulation power supply drain electrode modulation device of unmanned machine
CN105162540B (en) Wireless digital broadcasting station
CN103107970A (en) Communication system based on compressed sensing
Cantos et al. Performance of a waveform design for wireless power transfer with imperfect channel state information
CN102752000A (en) Chip and method for processing transmission signal
CN114244389A (en) Terminal chip, base station device, and bidirectional wireless communication system
CN204835587U (en) A photovoltaic modulation power source communication system for unmanned aerial vehicle
ur Rehman et al. LabVIEW based modeling of SWIPT system using BPSK modulation
CN202093172U (en) Beidou user terminal device
CN113395230B (en) Ultra-low power consumption OFDMA wireless downlink system and method based on nonlinear frequency mixing
CN206341218U (en) Satellite communication transceiver
CN114726395B (en) Wireless information and energy simultaneous transmission system based on adjustable frequency source and working method thereof
CN105048546A (en) Photovoltaic modulation power supply communication system applied to unmanned plane
CN103426278B (en) Unmanned hardstand remote-control data transmitting device
CN211429309U (en) Unattended system with Bluetooth intelligent module
CN103326438A (en) Wireless charging system in reflection-type communication mode

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20160406

Termination date: 20170320

CF01 Termination of patent right due to non-payment of annual fee