CN212258961U - Super-fusion satellite communication command system - Google Patents
Super-fusion satellite communication command system Download PDFInfo
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- CN212258961U CN212258961U CN202021058930.XU CN202021058930U CN212258961U CN 212258961 U CN212258961 U CN 212258961U CN 202021058930 U CN202021058930 U CN 202021058930U CN 212258961 U CN212258961 U CN 212258961U
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- 238000004891 communication Methods 0.000 title claims abstract description 62
- 238000010295 mobile communication Methods 0.000 claims abstract description 12
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Abstract
The utility model relates to a super-fusion satellite communication command system, a rear emergency consultation terminal equipped with an emergency consultation server and two or more fusion front finger devices, wherein satellite communication is established between the rear emergency consultation terminal and the fusion front finger devices through a Ka satellite portable station; the system comprises a mobile communication box connected with the fusion front finger equipment and an emergency field system consisting of a trunking interphone, a high-definition emergency deployment and control ball machine and a mobile video terminal, wherein the emergency field system and the mobile communication box are communicated through an MESH portable terminal, the integration of various communication modes is realized based on satellite communication, and meanwhile, the system architecture is improved, and the phenomenon of communication interruption is avoided.
Description
Technical Field
The utility model relates to a command system, concretely relates to super integration satellite communication command system.
Background
The emergency command system refers to a necessary coping mechanism system established by governments and other public institutions in the processes of pre-accident prevention, incident coping, in-process handling and after-treatment management of emergencies. A series of necessary measures are taken to ensure the safety of the lives and properties of the public; the emergency command system can comprehensively provide specific information such as site images, sound, positions and the like.
In terms of the present, a conventional command system generally comprises a background command center and at least one front-end command unit, and the background command center completes the unified scheduling of the front-end command unit. The structure has the defects that in some occasions with serious natural disasters, such as earthquakes, debris flows and the like, large-area power grid faults and basic network abnormalities are caused, and various communication networks cannot work normally. In the process of disaster relief, in order to ensure the smooth development and organization of work, a field command part needs to be built quickly, sometimes a plurality of field command parts need to be built according to the requirements of a disaster area and a disaster terrain, and the voice and the video of communication units, control balls, unmanned aerial vehicles and other equipment in the disaster relief field are accessed to the respective corresponding field command parts, so that the dispatching and the commanding of emergency maintenance work are realized, and the smooth development of the disaster relief work is ensured in the simplest and most efficient mode. Once the background command center loses communication with the front-end command department, paralysis of the command system can be caused.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to overcome prior art's not enough, provide a super integration satellite communication command system, realize the integration of multiple communication mode based on satellite communication, improve system architecture simultaneously, avoid appearing the phenomenon of communication interrupt.
The purpose of the utility model is realized through the following technical scheme:
a super-converged satellite communication command system, comprising:
the system comprises a rear emergency consultation terminal and two or more than two fused front-finger devices, wherein the rear emergency consultation terminal is provided with an emergency consultation server, and satellite communication is established between the rear emergency consultation terminal and the fused front-finger devices through a Ka satellite portable station;
the system comprises a mobile communication box connected with the fusion front finger equipment and an emergency field system consisting of a trunking interphone, a high-definition emergency control ball machine and a mobile video terminal, wherein the emergency field system and the mobile communication box are communicated through an MESH portable terminal.
Furthermore, the rear emergency consultation terminal and the integrated front finger device both adopt portable mobile single-machine structures.
Furthermore, the mobile communication box is internally provided with a communication basic module, a route switching module, a double 4G module, a double-frequency MESH ad hoc network module, a cluster gateway module and a communication configuration management module, and a plurality of external interfaces are reserved for accessing various communication systems or communication gateways.
Furthermore, the Ka satellite portable station adopts a 0.75-meter Ka frequency band backpack automatic satellite communication antenna.
Further, the system also comprises a communication gateway arranged between the Ka satellite portable station and the MESH portable terminal, and is used for establishing a communication link between the MESH portable terminal and a rear emergency consultation terminal, wherein the communication link is in a disconnected state in an initial state. That is to say, under the general condition, the MESH ad hoc network is used for realizing the communication between the converged front finger equipment and the field emergency system, so as to indirectly receive the instruction of the rear emergency consultation terminal, and after the communication between the converged front finger equipment and the field emergency system is disconnected, a communication link between the rear emergency consultation terminal and the field emergency system can be established, so as to continue to command the field.
Compare with traditional emergency command system the beneficial effects of the utility model are that:
(1) the scheme adopts a mode of integrating satellite communication and various network communications to realize the transmission of the instruction, improves a command architecture, sets a plurality of integrated front-pointing devices, and can transmit the instruction through another group of communication channels even if one group of communication is disconnected, thereby improving the stability of the system;
(2) the device is organically integrated with monitoring, scheduling, consultation, display control, communication, power supply and the like, has small volume, light weight and easy carrying, is portable and integrated with front fingers, mobile communication and front-end devices (individual soldiers, cloth control balls, unmanned aerial vehicles and the like) to reach the position nearby the site, and can be used after the power supply is turned on by one key;
(3) the wireless Mesh ad hoc network is also called as a wireless multi-hop network, has the characteristics of flexibility, easy use, easy expansion and the like, can self-organize, self-optimize and self-cure, and has high throughput rate and large capacity. The system can support various topological structures (star, network, chain and the like), and provides the capability of quickly and flexibly constructing a wireless network for a client;
(4) the front commanding department monitors and dispatches on-site rescue workers in real time, and the rear commanding post can communicate with the front commanding post in real time to know the rescue situation in time and can directly carry out dispatching and commanding on-site workers according to the rescue needs;
(5) the front command departments can orderly command the on-site emergency personnel in the local area, and also can realize multi-party real-time audio consultation among the front fingers and the rear command departments, and real-time multi-angle communication scheduling is realized;
(6) each front command post can initiate a multi-party collaborative consultation, wherein one command part is damaged or fails, and other front fingers can take over seamlessly. When the emergency rescue leader reaches the rescue site, one front command part can be used as the leader front command part, the rescue leader can check the audio and video information of a plurality of front command parts in real time, and the plurality of rescue sites are organized through video consultation to carry out cooperative scheduling for ordered rescue, so that the smooth development of rescue work is guaranteed in a fastest and efficient manner.
Drawings
Fig. 1 is a schematic diagram of the system of the present invention.
Detailed Description
The technical solution of the present invention is described in further detail below with reference to the accompanying drawings, but the scope of the present invention is not limited to the following description.
As shown in fig. 1, a super-convergence satellite communication command system includes a rear emergency consultation terminal configured with an emergency consultation server and two or more convergence front finger devices, and satellite communication is established between the rear emergency consultation terminal and the convergence front finger devices through a Ka satellite portable station; the system comprises a mobile communication box connected with the fusion front finger equipment and an emergency field system consisting of a trunking interphone, a high-definition emergency control ball machine and a mobile video terminal, wherein the emergency field system and the mobile communication box are communicated through an MESH portable terminal in an ad hoc network.
The rear emergency consultation terminal and the integrated front finger device both adopt portable mobile single-machine structures.
The integrated front finger equipment is mainly used for leaders and managers in front and for emergency multi-party command in places other than emergency command places. The system is a mobile, portable and integrated front emergency command and dispatching system. The system is used for rapidly developing various information acquisition and emergency command in front lines and emergency sites, and synchronously performing multi-party visual consultation and command scheduling with other sites and rear command centers.
The main technical parameters are as follows:
furthermore, the mobile communication box is internally provided with a communication basic module, a route exchange module, a double 4G module, a double-frequency MESH ad hoc network module, a cluster gateway module and a communication configuration management module, and a plurality of external interfaces are reserved for accessing various communication systems or communication gateways.
The technical parameters are as follows:
the Ka satellite portable station adopts a 0.75 m Ka frequency band backpack automatic satellite communication antenna, and is a backpack satellite antenna supporting the China satellite 16 number high-flux satellite communication service. The operation is simple, the collection is easy, the carrying is convenient, and the method is suitable for high-flux application, single emergency and other scenes.
The product is characterized in that: antenna weight (including BUC, side lobe, MODEM, battery, adapter, backpack): not more than 16 Kg; the offset feed structure has the advantages that the feed source part does not need to be disassembled and assembled when being collected and unfolded, the modem does not need to be disassembled and assembled when being internally provided with a built-in collection and unfolding, the power can be supplied by a common camera battery, the azimuth can be rotated in 360 degrees without limit, and the requirements of the national military standard on high temperature, low air pressure and vibration can be met.
The technical parameters are as follows:
receiving the frequency of 18.70-20.20 GHz;
the transmitting frequency is 29.46-30.00 GHz;
the receiving gain is more than or equal to 41.6dBi @20.20 GHz;
the emission gain is more than or equal to 44.5dBi @30.00 GHz;
side lobe characteristics 29-25log10 θ dBi (100 λ/D < θ <7 °);
the G/T value is 15dB/K @ 10-degree elevation angle;
polarization mode circular polarization (left-handed, right-handed);
the tracking precision is less than or equal to 0.2 degree RMS;
the satellite aligning time is less than or equal to 3 min;
control mode wired/wireless (WiFi) control;
a control terminal PC or a handheld intelligent terminal;
power supply 90-264 VAC,48VDC (optional);
the power consumption (without BUC) is less than or equal to 90W;
the net weight is less than or equal to 15.5 Kg;
the azimuth working range is 360 degrees;
the pitching working range is 10-90 degrees;
the working temperature is-40 ℃ to +55 ℃;
the storage temperature is-55 ℃ to +70 ℃;
wind-resistant working wind speed: less than or equal to 14 m/s;
wind speed preservation: less than or equal to 20m/s (weight);
the rain is less than or equal to 100 mm/h;
high temperature: meeting part 3 of the GJB150.3A-2009 military equipment laboratory environmental test method;
low temperature: meeting part 4 of the GJB150.4A-2009 military equipment laboratory environmental test method;
vibration: meeting part 16 of the GJB150.16A-2009 military equipment laboratory environmental test method;
low air pressure: meeting part 2 of the GJB150.2A-2009 military equipment laboratory environmental test method;
further, the system also comprises a communication gateway arranged between the Ka satellite portable station and the MESH portable terminal, and is used for establishing a communication link between the MESH portable terminal and a rear emergency consultation terminal, wherein the communication link is in a disconnected state in an initial state. That is to say, under the general condition, the MESH ad hoc network is used for realizing the communication between the converged front finger equipment and the field emergency system, so as to indirectly receive the instruction of the rear emergency consultation terminal, and after the communication between the converged front finger equipment and the field emergency system is disconnected, a communication link between the rear emergency consultation terminal and the field emergency system can be established, so as to continue to command the field.
The foregoing is illustrative of the preferred embodiments of the present invention, and it is to be understood that the invention is not limited to the precise forms disclosed herein, and that various other combinations, modifications, and environments may be resorted to, falling within the scope of the invention as defined by the appended claims. But that modifications and variations may be effected by those skilled in the art without departing from the spirit and scope of the invention, which is to be limited only by the claims appended hereto.
Claims (5)
1. A super-converged satellite communication command system, comprising:
the system comprises a rear emergency consultation terminal and two or more than two fused front-finger devices, wherein the rear emergency consultation terminal is provided with an emergency consultation server, and satellite communication is established between the rear emergency consultation terminal and the fused front-finger devices through a Ka satellite portable station;
the system comprises a mobile communication box connected with the fusion front finger equipment and an emergency field system consisting of a trunking interphone, a high-definition emergency control ball machine and a mobile video terminal, wherein the emergency field system and the mobile communication box are communicated through an MESH portable terminal.
2. The super-convergence satellite communication command system according to claim 1, wherein the rear emergency consultation terminal and the convergence front finger device both adopt a portable mobile single-machine structure.
3. The super-fusion satellite communication command system according to claim 2, wherein the mobile communication box is internally provided with a communication base module, a route switching module, a dual 4G module, a dual-frequency MESH ad-hoc network module, a trunking gateway module, and a communication configuration management module, and a plurality of external interfaces are reserved for accessing various communication systems or communication gateways.
4. The super fusion satellite communication command system of claim 3, wherein the Ka satellite portable station employs a 0.75 meter Ka band piggyback autonomous satellite communication antenna.
5. The super-convergence satellite communication command system according to claim 4, further comprising a communication gateway disposed between the Ka satellite portable station and the MESH portable terminal, for establishing a communication link between the MESH portable terminal and a rear emergency consultation terminal, wherein the communication link is in a disconnected state in an initial state.
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CN202021058930.XU CN212258961U (en) | 2020-06-10 | 2020-06-10 | Super-fusion satellite communication command system |
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CN202021058930.XU CN212258961U (en) | 2020-06-10 | 2020-06-10 | Super-fusion satellite communication command system |
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Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
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CN114158026A (en) * | 2021-11-26 | 2022-03-08 | 中国卫通集团股份有限公司 | Emergency communication command system based on satellite broadband platform |
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Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN114158026A (en) * | 2021-11-26 | 2022-03-08 | 中国卫通集团股份有限公司 | Emergency communication command system based on satellite broadband platform |
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