CN212366211U - High-precision satellite communication positioning antenna - Google Patents
High-precision satellite communication positioning antenna Download PDFInfo
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- CN212366211U CN212366211U CN202021062966.5U CN202021062966U CN212366211U CN 212366211 U CN212366211 U CN 212366211U CN 202021062966 U CN202021062966 U CN 202021062966U CN 212366211 U CN212366211 U CN 212366211U
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- antenna
- gain antenna
- satellite communication
- support
- communication positioning
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Abstract
The utility model particularly relates to a high-precision satellite communication positioning antenna, which belongs to the technical field of satellite communication positioning and comprises a signal transceiver, a main body connecting component and an energy conversion component, wherein a low-gain antenna is welded on the upper end of a supporting rod, a high-gain antenna edge is welded on the lower end of the supporting rod, a transition support and a satellite support are welded on a transition connecting component, a solar battery wing and the satellite support are bolted by a bolt, the utility model has the advantages that the low-gain antenna and the high-gain antenna are mutually matched, an arc-shaped magnetic block surrounded by a matrix forms a magnetic ring, has anti-interference capability, ensures more stable signal transmission and prevents electromagnetic radiation, therefore, signals are received and transmitted with high precision, stable energy is supplied and converted, the solid engine operates stably and efficiently, accurate and stable conversion and processing of the signals and stable operation of the signal transceiver are guaranteed, and high-precision communication and positioning effects are achieved.
Description
Technical Field
The utility model particularly relates to a high accuracy satellite communication positioning antenna belongs to satellite communication positioning technical field.
Background
At present, a satellite communication positioning antenna running around the earth continuously transmits a code modulated continuous wave radio signal to the earth surface, wherein the code carries an accurate transmitting signal of a satellite signal and accurate positions of satellites in space at different times. The satellite navigation receivers on board the vehicle, after receiving the radio signals from the satellites, if they have clocks exactly synchronized with the satellite clocks, can measure the arrival times of the signals, and thus can calculate the propagation time of the signals in space, so as to realize the positioning function.
The existing high-precision satellite communication positioning antenna has some defects in the use process, when a satellite communication system receives a continuous wave radio signal which is transmitted on the earth surface and modulated by codes, the interference of uncertain factors can be caused, the transmitted signal causes deviation, so that the positioning is not accurate enough, the time can be not accurate gradually, and the measured time can also have certain deviation.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a high accuracy satellite communication location antenna just for solving above-mentioned problem.
The utility model discloses a following technical scheme realizes above-mentioned purpose, a high accuracy satellite communication positioning antenna, including signal transceiver, main part coupling assembling, energy conversion subassembly, its characterized in that: the signal transceiver comprises a low-gain antenna, a high-gain antenna, a support rod, a connecting column, a triangular fixed ring, an arc-shaped magnetic block, a servo turntable and a solid engine, the upper end of the support rod is connected with the low-gain antenna in a welding manner, the lower end of the connecting column is welded and connected with the edge of the high-gain antenna, the middle of the connecting column is riveted and connected with the triangular fixed ring, the upper end of the connecting column is welded and connected with the high-gain antenna, the lower end of the connecting column is welded and connected with the solid engine, the main body connecting assembly comprises a main body shell, a transition support and a transition connecting part, the main body shell wraps the solid engine, the lower end of the energy conversion component is welded with the transition bracket, the energy conversion component comprises a satellite bracket, a solar cell wing and a bolt, the transition connecting part is welded with the transition bracket and the satellite bracket, and the bolt is used for connecting the solar battery wing and the satellite bracket through bolts.
Preferably, in order to enhance the collection intensity of the signal transceiver, the high-gain antenna is a parabolic antenna, and the signal can be reflected and focused at a focus, so that the signal can be collected accurately.
Preferably, to enhance the collection efficiency of the signal transceiver, the signal transceiver has the low-gain antenna and the high-gain antenna, which together collect signals.
Preferably, in order to enhance the collection accuracy of the signal transceiver, the arc-shaped magnetic block array surrounds the connecting column for a circle to improve the signal receiving capability of the antenna.
Preferably, to enhance the stability of the body, the solid engine is enclosed and protected by the body casing.
Preferably, to enhance the stability of the signal transceiver, the high gain antenna and the low gain antenna are connected by welding four support rods.
Preferably, for enhancing the whole energy, enough and stable are provided, and the solar cell wings are four in number and arc-shaped, so that the solar energy can be conveniently collected.
The utility model has the advantages that: the utility model discloses a low-gain antenna and high-gain antenna mutually support, the arc magnetic path that the array shape centers on forms the magnetic ring, has the interference killing feature, make signal transmission more stable, prevent electromagnetic radiation, thereby high accuracy is received and propagated signal, stable energy provides and the conversion, make solid engine stabilize high-efficient operation, the steady operation of also having guaranteed the accurate stable conversion of signal and processing and signal transceiver, reach the effect of high accuracy communication and location.
Drawings
Fig. 1 is a schematic view of the overall structure of the present invention;
fig. 2 is a schematic structural diagram of the energy conversion assembly of the present invention;
fig. 3 is a schematic structural diagram of the signal transceiver of the present invention;
FIG. 4 is an overall front view of the present invention;
fig. 5 is an overall left side view of the present invention;
FIG. 6 is a schematic view of the whole half-section of the present invention;
in the figure: 1. the device comprises a signal transceiver, 3, an energy conversion component, 11, a low-gain antenna, 12, a high-gain antenna, 13, a supporting rod, 14, a connecting column, 15, a triangular fixing ring, 16, an arc-shaped magnetic block, 17, a servo turntable, 18, a solid engine, 21, a main body shell, 22, a transition support, 23, a transition connecting component, 31, a satellite support, 32, a solar cell wing, 33 and a bolt.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Referring to fig. 1-6, a high-precision satellite communication positioning antenna includes a signal transceiver, a main body connection component, and an energy conversion component, and is characterized in that: the signal transceiver comprises a low-gain antenna, a high-gain antenna, a support rod, a connecting column, a triangular fixed ring, an arc-shaped magnetic block, a servo turntable and a solid engine, wherein the upper end of the support rod is welded with the low-gain antenna, the lower end of the support rod is welded with the edge of the high-gain antenna, so that the relative position of the low-gain antenna and the high-gain antenna is stable, the triangular fixed ring is riveted and connected in the middle of the connecting column, the framework of the support rod is stable, the upper end of the support rod is welded with the high-gain antenna, the lower end of the support rod is welded with the solid engine, so that the antenna stably runs along with the solid engine, the main body connecting assembly comprises a main body shell, a transition support and a transition connecting part, the main body shell wraps the solid engine to play a protection role, the lower end of, the bolt is with solar cell wing and satellite support bolted connection, the utility model discloses a low-gain antenna and high-gain antenna mutually support, the arc magnetic path that the formation centers on forms the magnetic ring, the interference killing feature has, make signal transmission more stable, prevent electromagnetic radiation, thereby high accuracy is received and propagated signal, stable energy provides and the conversion, make solid engine stabilize high-efficient operation, the stable operation of also having guaranteed the accurate stable conversion of signal and processing and signal transceiver, reach the effect of high accuracy communication and location.
As a technical optimization scheme of the utility model, the high gain antenna is parabolic antenna, can be a focus to the signal reflection gathering, the accurate signal of collecting of being convenient for.
As a technical optimization scheme of the utility model, signal transceiver has low-gain antenna and high-gain antenna, collects the signal jointly.
As a technical optimization scheme of the utility model, arc magnetic path array shape is around improving antenna signal reception ability in spliced pole a week.
As a technical optimization scheme of the utility model, the solid engine is protected by main body cover parcel.
As a technical optimization scheme of the utility model, high gain antenna is connected with four spinal branch vaulting pole weldings with low gain antenna.
As a technical optimization scheme of the utility model, the solar cell wing is total four and be the arc, is convenient for collect solar energy.
The working principle is as follows: the utility model discloses when using, at first the signal is collected through low gain antenna 11 and high gain antenna 12 and is caught the signal, servo revolving stage 17 and the operation of solid engine 18, through processing system according to the longitude and the initial angle of latitude and relative horizontal plane of position, then according to its gesture and geographical position, satellite longitude automatic determination uses the horizontal plane as the antenna elevation of benchmark, the position of rotating under the prerequisite that keeps the elevation to the horizontal plane unchangeable to with the signal maximum mode automatic alignment satellite. In the carrier motion process, the change of the carrier attitude is measured, the change is converted into an error angle of an antenna through the operation of a mathematical platform, the azimuth angle, the pitch angle and the polarization angle of the antenna are adjusted through a servo mechanism, the fact that the antenna is within a specified range during the change process of the carrier is guaranteed, the two kinds of tracking can be automatically switched according to the field situation, data such as antenna polarization, azimuth and pitching and the like are continuously output, meanwhile, signals are transmitted through an advanced mobile satellite communication system and are transmitted out through a signal transceiver 1, the high-precision communication positioning effect is achieved, and the solar cell wings 32 continuously provide energy for equipment to use.
It is obvious to a person skilled in the art that the invention is not restricted to details of the above-described exemplary embodiments, but that it can be implemented in other specific forms without departing from the spirit or essential characteristics of the invention. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.
Furthermore, it should be understood that although the present description refers to embodiments, not every embodiment may contain only a single embodiment, and such description is for clarity only, and those skilled in the art should integrate the description, and the embodiments may be combined as appropriate to form other embodiments understood by those skilled in the art.
Claims (7)
1. The utility model provides a high accuracy satellite communication location antenna, includes signal transceiver (1), main part coupling assembling, energy conversion subassembly (3), its characterized in that: the signal transceiver (1) comprises a low-gain antenna (11), a high-gain antenna (12), a support rod (13), a connecting column (14), a triangular fixed ring (15), an arc-shaped magnetic block (16), a servo rotary table (17) and a solid engine (18), wherein the upper end of the support rod (13) is connected with the low-gain antenna (11) in a welding mode, the lower end of the support rod (13) is connected with the edge of the high-gain antenna (12) in a welding mode, the triangular fixed ring (15) is connected in the middle of the connecting column (14) in a riveting mode, the upper end of the support rod is connected with the high-gain antenna (12) in a welding mode, the lower end of the support rod is connected with the solid engine (18) in a welding mode, the main body connecting assembly comprises a main body shell (21), a transition support (22) and a transition connecting, the energy conversion assembly (3) comprises a satellite support (31), solar cell wings (32) and bolts (33), the transition connection parts (23) are connected with the transition support (22) and the satellite support (31) in a welding mode, and the bolts (33) connect the solar cell wings (32) with the satellite support (31) through bolts.
2. A high accuracy satellite communication positioning antenna as recited in claim 1, wherein: the high-gain antenna (12) is a parabolic antenna, and can reflect and focus signals at a focus so as to facilitate accurate signal collection.
3. A high accuracy satellite communication positioning antenna as recited in claim 1, wherein: the signal transceiver (1) is provided with the low-gain antenna (11) and the high-gain antenna (12) which are used for collecting signals together.
4. A high accuracy satellite communication positioning antenna as recited in claim 1, wherein: the arc-shaped magnetic block (16) is arranged around the connecting column (14) in a matrix shape, so that the signal receiving capability of the antenna is improved.
5. A high accuracy satellite communication positioning antenna as recited in claim 1, wherein: the solid engine (18) is enclosed and protected by the main body housing (21).
6. A high accuracy satellite communication positioning antenna as recited in claim 1, wherein: the high gain antenna (12) and the low gain antenna (11) are welded together by four support rods (13).
7. A high accuracy satellite communication positioning antenna as recited in claim 1, wherein: the solar cell wings (32) are four in number and arc-shaped, and solar energy can be collected conveniently.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021062966.5U CN212366211U (en) | 2020-06-10 | 2020-06-10 | High-precision satellite communication positioning antenna |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021062966.5U CN212366211U (en) | 2020-06-10 | 2020-06-10 | High-precision satellite communication positioning antenna |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN212366211U true CN212366211U (en) | 2021-01-15 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202021062966.5U Expired - Fee Related CN212366211U (en) | 2020-06-10 | 2020-06-10 | High-precision satellite communication positioning antenna |
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| Country | Link |
|---|---|
| CN (1) | CN212366211U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114430507A (en) * | 2021-12-27 | 2022-05-03 | 亚太卫星宽带通信（深圳）有限公司 | Inter-satellite link baseband transceiver |
-
2020
- 2020-06-10 CN CN202021062966.5U patent/CN212366211U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114430507A (en) * | 2021-12-27 | 2022-05-03 | 亚太卫星宽带通信（深圳）有限公司 | Inter-satellite link baseband transceiver |
| CN114430507B (en) * | 2021-12-27 | 2024-02-23 | 亚太卫星宽带通信（深圳）有限公司 | Inter-satellite link baseband transceiver |
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| Date | Code | Title | Description |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20210115 Termination date: 20210610 |
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| CF01 | Termination of patent right due to non-payment of annual fee |