CN114114329A - Airborne Beidou double-antenna command type user machine - Google Patents
Airborne Beidou double-antenna command type user machine Download PDFInfo
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- CN114114329A CN114114329A CN202111430648.9A CN202111430648A CN114114329A CN 114114329 A CN114114329 A CN 114114329A CN 202111430648 A CN202111430648 A CN 202111430648A CN 114114329 A CN114114329 A CN 114114329A
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- 238000012545 processing Methods 0.000 claims abstract description 40
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- 238000004891 communication Methods 0.000 abstract description 5
- 238000010586 diagram Methods 0.000 description 8
- 238000000034 method Methods 0.000 description 7
- 238000013461 design Methods 0.000 description 6
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- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 description 1
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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
- G01S19/14—Receivers specially adapted for specific applications
- G01S19/17—Emergency applications
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/12—Supports; Mounting means
- H01Q1/22—Supports; Mounting means by structural association with other equipment or articles
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/27—Adaptation for use in or on movable bodies
- H01Q1/28—Adaptation for use in or on aircraft, missiles, satellites, or balloons
- H01Q1/285—Aircraft wire antennas
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q21/00—Antenna arrays or systems
- H01Q21/29—Combinations of different interacting antenna units for giving a desired directional characteristic
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Abstract
The invention relates to the field of communication equipment, in particular to an airborne Beidou dual-antenna command type user machine which comprises a Beidou receiving host and a plurality of Beidou antennas, wherein the Beidou antennas are used for receiving Beidou signals and are connected with a core processing board, the core processing board is used for receiving and sending the Beidou signals, a carrier plate is connected with the core processing board, an interface is connected with the core processing board, and the carrier plate is used for selecting the Beidou antennas based on signal intensity. When the helicopter is used, the Beidou antenna system is arranged on two sides of a helicopter, Beidou signals sent by the ground are received through the Beidou antennas, the Beidou antennas with high signal strength are selected to transmit the signals after the carrier plate receives the signal strength, the signals are processed and converted through the core processing board and can be connected with external equipment through an interface to supply power and transmit data, and the power management module is used for supplying power to the whole device and improving the signal receiving efficiency.
Description
Technical Field
The invention relates to the field of communication equipment, in particular to an airborne Beidou dual-antenna command type user machine.
Background
An airborne Beidou receiver related to an emergency rescue search system based on Beidou is generally installed on an emergency rescue helicopter and mainly used for receiving position information reported by a Beidou terminal in danger and guiding the emergency rescue helicopter to directly reach the position in danger to carry out a search and rescue task.
At present, a temporary additional installation mode is adopted in China, equipment and an antenna are installed inside an engine room, the directivity of the antenna is limited due to the additional installation mode, if the equipment only has one antenna, signals cannot be received in a local direction, and normal positioning and communication cannot be achieved.
Disclosure of Invention
The invention aims to provide an airborne Beidou dual-antenna command type user machine, which adopts the design of two antennas and is arranged on glass windows at two sides of a helicopter, and the antennas can be selected according to the signal intensity in the flight process of the helicopter, so that the problems that a Beidou receiver cannot receive signals and the positioning and communication are interrupted in the flight process of the helicopter are solved.
In order to achieve the purpose, the invention provides an airborne Beidou dual-antenna command type user machine which comprises a Beidou receiving host and a plurality of Beidou antennas, wherein the Beidou receiving host comprises a support plate, a core processing plate, a power management module and a first interface, the Beidou antennas are used for Beidou signal receiving and sending processing and are connected with an aerial plug of an external antenna of the core processing plate, the core processing plate is used for Beidou signal analysis processing, the support plate is connected with the core processing plate, the first interface is connected with the core processing plate and the support plate, and the support plate is used for selecting the Beidou antennas, the power supply voltage of the core processing plate and interface conversion based on signal intensity switching.
The Beidou antenna comprises a plurality of receiving antennas, a transmitting antenna, a plurality of low noise amplifiers, a power amplifier, a combiner and a radio frequency interface, wherein the receiving antennas are connected with the low noise amplifiers, the combiner is connected with the low noise amplifiers, the power amplifier is connected with the combiner, the transmitting antennas are connected with the power amplifiers, the combiner is connected with the radio frequency interface, and the radio frequency interface is connected with the aerial plug through a radio frequency cable.
The Beidou antenna further comprises a base and a shielding cover, wherein the shielding cover is arranged above the plurality of receiving antennas and the plurality of sending antennas, and the low noise amplifier, the power amplifier, the combiner and the radio frequency interface are arranged in a separate cavity in the base; the Beidou receiver host further comprises a shielding metal shell, wherein the support plate, the core processing plate, the power management module and the first interface are installed in the shielding metal shell.
The core processing board comprises a baseband circuit module, a radio frequency circuit module, an interface circuit module and a power module, wherein the radio frequency circuit module is connected with the baseband circuit module, the interface circuit module is connected with the radio frequency circuit module, the baseband circuit module and the power module, and the power module supplies power to the baseband circuit module, the radio frequency circuit module and the interface circuit module.
The carrier plate comprises a third interface, a data conversion circuit, a power conversion circuit, a Bluetooth data processing circuit, an IC card and a reset circuit, wherein the interface conversion circuit is connected with the first interface and the core processing plate, the power conversion circuit is connected with the power conversion plate and the core processing plate, the Bluetooth and data processing circuit is connected with the third interface and the data conversion circuit, and the IC card and the reset circuit are connected with the core processing plate.
Wherein, the radio frequency circuit module includes the channel multiplexer, a plurality of wave band receiving circuit and wave band transmitting circuit, and is a plurality of the wave band receiving circuit with wave band transmitting circuit with the channel multiplexer is connected, the baseband circuit module is with a plurality of the wave band transmitting circuit with wave band transmitting circuit connects.
The power management module comprises a power conversion board and a battery, the power conversion board is connected with the battery and the support plate, when the power conversion board is used for being free of an external adapter, the circuit is switched to supply power to the battery, and when the external adapter is available, the circuit is switched to supply power to the external adapter and charge the battery.
The first interface comprises a state indicator lamp, a serial aviation plug, a power input aviation plug and a toggle switch, the serial aviation plug is connected with the carrier plate, the power input aviation plug is connected with the power conversion plate, and the toggle switch is connected with the power conversion plate. According to the airborne Beidou dual-antenna command type user machine, the continuity of Beidou signals is guaranteed as much as possible in the flying process of a helicopter. When the helicopter is used, the novel Beidou satellite remote control system is arranged on two sides of a helicopter, Beidou signals sent by satellites are received through a plurality of Beidou antennas, the carrier plate monitors the wave velocity state of the Beidou signals in real time, the Beidou antennas with high signal intensity are selected to receive and send the Beidou signals, the signals are processed and converted through the core processing board, the novel Beidou satellite remote control system can be connected with external equipment through the interface to supply power and transmit data, the power management module is used for supplying power to the whole device, and the built-in power supply can be used for outdoor field mobile use or indoor fixed long-time use for more than 4 hours.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to the drawings without creative efforts.
FIG. 1 is a block diagram of an airborne Beidou dual-antenna command type user machine of the invention;
FIG. 2 is a functional block diagram of the RF circuit module of the present invention;
FIG. 3 is a functional block diagram of the receive channel circuitry of the present invention;
FIG. 4 is a schematic diagram of an RDSS receive module;
FIG. 5 is a diagram of the composition and power supply relationships of a power management module;
FIG. 6 is an antenna composition and signal flow diagram of an airborne Beidou dual-antenna directed subscriber unit of the present invention;
FIG. 7 is a block diagram of the components of the core processing board of the present invention.
The radio frequency antenna comprises a 1-Beidou receiving host, a 2-Beidou antenna, an 11-carrier plate, a 12-core processing plate, a 13-power management module, a 14-interface, a 21-receiving antenna, a 22-sending antenna, a 23-low noise amplifier, a 24-power amplifier, a 25-combiner, a 26-shielding cover, a 121-baseband circuit module, a 122-radio frequency circuit module, a 123-interface circuit module, a 124-power module, a 131-power conversion plate, a 132-battery, a 1221-channel multiplexer, a 1222-waveband receiving circuit and a 1223-waveband transmitting circuit.
Detailed Description
Reference will now be made in detail to embodiments of the present invention, examples of which are illustrated in the accompanying drawings, wherein like or similar reference numerals refer to the same or similar elements or elements having the same or similar function throughout. The embodiments described below with reference to the drawings are illustrative and intended to be illustrative of the invention and are not to be construed as limiting the invention.
In the description of the present invention, it is to be understood that the terms "length", "width", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", and the like, indicate orientations or positional relationships based on the orientations or positional relationships illustrated in the drawings, and are used merely for convenience in describing the present invention and for simplicity in description, and do not indicate or imply that the devices or elements referred to must have a particular orientation, be constructed in a particular orientation, and be operated, and thus, are not to be construed as limiting the present invention. Further, in the description of the present invention, "a plurality" means two or more unless specifically defined otherwise.
Referring to fig. 1 to 7, the present invention provides an airborne beidou dual-antenna command type user machine:
including big dipper receiver host computer 1 and a plurality of big dipper antenna 2, big dipper receiver host computer 1 includes that support plate 11, core handle board 12, power management module 13 and first interface 14, big dipper antenna 2 is used for receiving and dispatching the big dipper signal, causes radio frequency interface 26 outward, through 5 meters radio frequency cable with the antenna aviation connector who first interface 14 locates is connected, then extends to the casing inside and handle board 12 with the core and be connected, board 12 is handled in being responsible for big dipper signal analysis and handles to the core, support plate 11 with board 12 is handled to the core power management module 13 connects, first interface 14 with support plate 11 board 12 is handled to the core power management module 13 connects, support plate 11 is used for switching selection based on signal strength big dipper antenna 2 board 12 power supply voltage and interface conversion are handled to the core.
In the embodiment, the Beidou signal continuity is ensured as much as possible in the flight process of the helicopter. When the helicopter is used, the helicopter is arranged on two sides of a helicopter, Beidou signals sent by satellites are received through the Beidou antennas 2, the carrier plate 11 selects the Beidou antennas 2 with high signal strength to transmit the signals after monitoring the state of signal beams, the signals are processed and converted through the core processing plate 12 and can be connected with external equipment through the interface 14 or the Bluetooth to supply power and transmit data, the power management module 13 is used for supplying power to the whole device, and the built-in power supply can be used for realizing mobile use in an external field for over 4 hours or indoor fixed use for a long time.
The carrier 11 is mainly responsible for antenna switching selection processing, power conversion, interface 14 conversion, reset, IC card installation, and other functions. The device mainly comprises a singlechip control circuit, a power supply conversion control circuit, a serial port conversion output circuit, a reset and second pulse output circuit, an IC card control circuit, a Bluetooth control circuit and the like.
Further, the big dipper antenna 2 includes a plurality of receiving antennas 21, a transmitting antenna 22, a plurality of low noise amplifiers 23, a power amplifier 24, a combiner 25 and a radio frequency interface 26, where the receiving antenna 21 is connected to the low noise amplifiers 23, the combiner 25 is connected to the plurality of low noise amplifiers 23, the power amplifier 24 is connected to the combiner 25, the transmitting antenna 22 is connected to the power amplifier 24, the combiner 25 is connected to the radio frequency interface 26, and the radio frequency interface 26 is connected to the first interface 14 through a radio frequency cable.
In this embodiment, the receiving antennas 21 include 1B 3 frequency band receiving antenna, 1S frequency band receiving antenna, and 1B 1/L1 receiving antenna, and the receiving antennas are amplified and filtered by the low noise amplifier 23 to obtain an effective signal, the transmitting antenna 22 is an L transmitting antenna for providing L frequency point signal transmission, and the power amplifier 24 is for providing corresponding transmission power.
Further, big dipper antenna 2 still includes base 27 and shield cover 28, shield cover 28 sets up antenna body top, base 27 sets up antenna body below. The shielding cover is arranged above the plurality of receiving antennas 21 and the plurality of transmitting antennas, and the low noise amplifier 23, the power amplifier 24, the combiner 25 and the radio frequency interface 26 are arranged in a separate cavity in the base; the Beidou receiver host further comprises a shielding metal shell, wherein the carrier plate 11, the core processing plate 12, the power management module 13 and the first interface 14 are installed in the shielding metal shell.
In this embodiment, the rf circuitry inside the host is shielded from other circuitry. The size of the panel interface 14 is consistent with that of a connector, a shielding rubber ring and a rubber pad are added to prevent electromagnetic leakage, and theoretically, the electromagnetic radiation can be effectively prevented when the size of the opening is smaller than lambda/4 (lambda is the wavelength), the frequency mainly used by the device is 2491.57MHz, 1615.68MHz and 1268MHz, and no electromagnetic leakage exists as long as the size of the opening of the panel is smaller than 12 cm. All connectors select connectors with filtering functions, and the openings of the connectors are smaller than 2 cm.
Further, the core processing board 12 includes a baseband circuit module 121, a radio frequency circuit module 122, an interface circuit module 123 and a power supply module 124, where the radio frequency circuit module 122 is connected to the baseband circuit module 121, the interface circuit module 123 is connected to the baseband circuit module 121, the radio frequency circuit module 122 and the power supply module 124, and the power supply module 124 supplies power to the baseband circuit module 121, the radio frequency circuit module 122 and the interface circuit module 123.
In this embodiment, the baseband circuit module 121 employs a shanghai double-denier microelectronic JFM7205F chip. JFM7205F is a latest big dipper RDSS/RNSS multimode baseband processing chip based on 65nm technology platform, is mainly applied to user terminal equipment such as big dipper satellite navigation, location, time service and the like, and can receive and process digitalized radio frequency satellite navigation signals of RNSS B3, B1, GPS L1 or GLONASS F1 frequency points. The device can be matched with a precise ranging code chip to complete the functions of capturing and tracking a set navigation signal, demodulating and decoding navigation messages, extracting original observed quantity and the like. JFM7205F is provided with 32-bit high-performance CPU, so that the user can select to output navigation message, original observation quantity, working state of baseband chip and other information through data bus interface 14, or select to use the built-in CPU to complete message demodulation and PVT information resolution, and directly output the message through serial port.
JFM7205F is embedded with RDSS special baseband processing circuit, supports the receiving and sending of big dipper generation RDSS satellite signal, cooperates with inside CPU to accomplish the protocol processing of coming in and going out station and communication protocol processing, supports the command function.
The radio frequency circuit module 122 adopts Beidou RDSS and RNSS radio frequency chips to adopt twice frequency conversion, and two image rejection MIXERs (MIXER1) are integrated at the RF front end. The two channels share an LNA, which is amplified and sent to the first stage MIXER 1. The intermediate frequency part is two independent channels, and an AGC, a second stage MIXER2, an LPF and an IF output buffer amplifier are respectively integrated. And a PLL, a VCO, a crystal oscillator and a frequency divider with a fixed frequency dividing ratio are integrated in the chip to provide local oscillation signals for the frequency mixer. The radio frequency chip is packaged by QFN64, and the working temperature range is-40 to +85 ℃.
The interface circuit module 123 is used for connecting with the first interface 14 antenna aviation plug, and is used for receiving and transmitting the Beidou signal at the first interface 14.
Further, the rf circuit module 122 includes a channel multiplexer 1221, a plurality of band receiving circuits 1222 and a band transmitting circuit 1223, the plurality of band receiving circuits 1222 and the band transmitting circuit 1223 are connected to the channel multiplexer 1221, and the baseband circuit module 121 is connected to the plurality of band transmitting circuits 1223 and the band transmitting circuit 1223.
In this embodiment, the plurality of band receiving circuits 1222 correspond to corresponding antennas, signals input from the beidou antenna 2 through the coaxial cable enter the channel multiplexer 1221, the channel multiplexer 1221 separates all band signals combined by the antennas and feeds the separated band signals to the receiving circuits of corresponding bands, where the B1 band and the L1 band may share the same antenna due to adjacent frequencies (B1-1561.098 MHz, L1-1575.42 MHz), and further have B3 band and S band signal inputs. The method adopts a scheme of two down-conversion, can carry out down-conversion processing on any one navigation signal of B1, B2, B3, GPS L1 and GLONASS L1 according to the level setting of pins, and provides a working clock of the whole receiver. The PLL, the VCO circuit and the AGC control circuit are integrated inside the digital control circuit, and the system noise coefficient is less than 4 dB. The chip has high integration level, and greatly simplifies the design of a receiving circuit. And the chip has high consistency and meets the requirements of standardization and miniaturization. As shown in fig. 3. The dotted line part is the integrated down-conversion chip, and the receiving channel function of secondary frequency conversion can be realized by matching with some peripheral circuits. The internal AGC circuit can realize the dynamic control range of 50 dB. The noise coefficient of the internal LNA is superior to 3dB, and the noise coefficient of the internal LNA is matched with the external LNA for use, so that the noise performance of the whole machine is good, and the application requirement is met.
The function of the RDSS receiving channel is mainly to frequency select and amplify signals. An integrated down-conversion module is selected for implementation. The module integrates an S-band two-time down-conversion receiving channel and an L-band BPSK modulation transmitting channel, adopts metal surface mount packaging, has the characteristics of high integration level, low power consumption, small size, high reliability and the like, and is very high in integration level, so that the design of a receiving circuit is greatly simplified. And the chip has high consistency and meets the requirements of standardization and miniaturization. All three channels can be realized by using the module, and the schematic block diagram is shown in figure 4
Further, the power management module 13 includes a power conversion board 131 and a battery 132, the power conversion board 131 is connected to the battery 132, the power conversion board 131 is used for converting the battery 132 to supply power to the device when there is no external adapter, and converting the external adapter to supply power and charge the battery 132 when there is an external adapter.
In this embodiment, the battery 132 is a polymer lithium battery (4 strings and 3 parallel), the standard output voltage is 16.8V, and the capacity of the battery 132 is 9450mAh or more. Using external adapters or DC 24VDCWhen external power is supplied, the input voltage is converted into 2 paths through the power conversion plate 131, and the 1 path of 18V supplies power to the equipment; the 1-path charges the battery 132, and the power conversion board 131 has a function of protecting the battery 132 from overcharging, and the power supply relationship is as shown in fig. 5. When no external power supply supplies power, the equipment adopts the built-in battery 132 to supply power, and the standard output voltage is 16.8V; the output voltage is converted and boosted to 18V by the power panel to supply power for the core processing unit.
Further, the first interface 14 includes a status indicator lamp, a serial aviation plug, a power input aviation plug and a toggle switch, the serial aviation plug is connected to the carrier plate 11, the power input aviation plug is connected to the power conversion board 131, and the toggle switch is connected to the power conversion board 131.
In the embodiment, the host connector adopts a standard aviation connector, and the cable at the tail part of the connector is connected with the inserting core in a compression joint mode, so that poor contact and falling off are prevented, and the normal work of equipment is guaranteed. The connector has the advantages of error prevention, waterproof capability, and good electromagnetic shielding effect due to the fact that the connector is provided with the shielding rubber mat.
The user machine battery 132 model of the invention is ICNPP58/54/174-6SHDJ-TX, the capacity is more than or equal to 9.45 Ah; the required voltage of an internal module of the equipment is 18/1.2A, the long-time working can be estimated to be about 8h, the requirement that the working time is more than or equal to 4 hours is met, and the long-time outfield mobile use is met. An internal carrier plate 11 of the airborne Beidou dual-antenna command type user machine comprises a Bluetooth module design, and supports wireless Bluetooth connection of an external display terminal to carry out data interaction and APP operation control; meanwhile, the equipment comprises an RS232 data interface 14 which can be connected with a special serial port line to a PC end, and is controlled by operation of PC end search and rescue software, so that the problem of limited use scenes is solved.
In order to solve the problem that signal receiving is interrupted due to different antenna orientations in the flight process of a helicopter, the implementation mode mainly considers from two aspects, namely the design of a double-antenna switching circuit and the installation position of a double-antenna. The first is that the antennas are installed in different orientations, and at a certain distance (for example, at the two side glasses of the helicopter, no matter which direction the helicopter flies, one antenna is always kept in a good signal receiving state). The design adopts a singlechip program algorithm to judge the strength of signals and then switches the antennas continuously, thereby keeping the equipment in a good signal receiving state all the time.
While the invention has been described with reference to a preferred embodiment, it will be understood by those skilled in the art that various changes in form and detail may be made therein without departing from the spirit and scope of the invention as defined by the appended claims.
Claims (8)
1. An airborne Beidou dual-antenna command type user machine is characterized in that,
including big dipper receiver host computer and a plurality of big dipper antenna, big dipper receiver host computer includes that support plate, core handle board, power management module and first interface, big dipper antenna is used for big dipper signal receiving and dispatching to handle, and with the core is handled the board and is drawn the antenna aviation plug connection outward, the board is handled to the core and is used for being responsible for big dipper signal analysis and handles, the support plate with the board is handled to the core is connected, first interface with the core handle the board the support plate is connected, the support plate is used for switching the selection based on signal strength big dipper antenna the board supply voltage is handled to the core and interface conversion.
2. The airborne Beidou dual-antenna command type subscriber machine according to claim 1,
the Beidou antenna comprises a plurality of receiving antennas, a transmitting antenna, a plurality of low noise amplifiers, a power amplifier, a combiner and a radio frequency interface, wherein the receiving antennas are connected with the low noise amplifiers, the combiner is connected with the low noise amplifiers, the power amplifier is connected with the combiner, the transmitting antenna is connected with the power amplifier, the combiner is connected with the radio frequency interface, and the radio frequency interface is connected with the aerial plug through a radio frequency cable.
3. The airborne Beidou dual-antenna directed subscriber unit of claim 2,
the Beidou antenna also comprises a base and a shielding cover, wherein the shielding cover is arranged above the plurality of receiving antennas and the plurality of sending antennas, and the low noise amplifier, the power amplifier, the combiner and the radio frequency interface are arranged in a separate cavity in the base; the Beidou receiver host comprises a shielding metal shell, wherein the support plate, the core processing plate, the power management module and the first interface are installed in the shielding metal shell.
4. The airborne Beidou dual-antenna command type subscriber machine according to claim 1,
the core processing board comprises a baseband circuit module, a radio frequency circuit module, an interface circuit module and a power module, wherein the radio frequency circuit module is connected with the baseband circuit module, the interface circuit module is connected with the radio frequency circuit module, the baseband circuit module and the power module, and the power module supplies power to the baseband circuit module, the radio frequency circuit module and the interface circuit module.
5. The airborne Beidou dual-antenna command type subscriber machine according to claim 1,
the carrier plate comprises a third interface, a data conversion circuit, a power conversion circuit, a Bluetooth data processing circuit, an IC card and a reset circuit, the interface conversion circuit is connected with the first interface and the core processing plate, the power conversion circuit is connected with the power conversion plate and the core processing plate, the Bluetooth and data processing circuit is connected with the third interface and the data conversion circuit, and the IC card and the reset circuit are connected with the core processing plate.
6. The airborne Beidou dual-antenna directed subscriber unit of claim 4,
the radio frequency circuit module comprises a channel multiplexer, a plurality of waveband receiving circuits and a waveband transmitting circuit, the waveband receiving circuits and the waveband transmitting circuit are multiple, the waveband receiving circuits and the waveband transmitting circuit are connected with the channel multiplexer, and the baseband circuit module is multiple, the waveband transmitting circuit and the waveband transmitting circuit are connected.
7. The airborne Beidou dual-antenna command type subscriber machine according to claim 1,
the power management module comprises a power conversion plate and a battery, the power conversion plate is connected with the battery and the support plate, when the power conversion plate is not provided with an external adapter, the circuit is switched to supply power to the battery, and when the external adapter is provided, the circuit is switched to supply power to the external adapter and charge the battery.
8. The airborne Beidou dual-antenna command type subscriber machine according to claim 1,
the first interface comprises a state indicator lamp, a serial aviation plug, a power input aviation plug and a toggle switch, the serial aviation plug is connected with the support plate, the power input aviation plug is connected with the power conversion plate, and the toggle switch is connected with the power conversion plate.
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| CN110568455A (en) * | 2018-06-05 | 2019-12-13 | 上海航天卫星应用有限公司 | Beidou beacon system |
| CN216646824U (en) * | 2021-11-29 | 2022-05-31 | 中国人民解放军第六九O五工厂 | Airborne Beidou double-antenna command type user machine |
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2021
- 2021-11-29 CN CN202111430648.9A patent/CN114114329A/en active Pending
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| CN104459721A (en) * | 2014-11-14 | 2015-03-25 | 北京九天利建信息技术有限公司 | Beidou short message all-directional receiving and sending user receiver terminal |
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| CN208384102U (en) * | 2018-06-05 | 2019-01-15 | 上海航天卫星应用有限公司 | A kind of ″Beidou″ beacon equipment applied to black box |
| CN110568455A (en) * | 2018-06-05 | 2019-12-13 | 上海航天卫星应用有限公司 | Beidou beacon system |
| CN216646824U (en) * | 2021-11-29 | 2022-05-31 | 中国人民解放军第六九O五工厂 | Airborne Beidou double-antenna command type user machine |
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