CN202929409U - Movable type satellite communication earth station antenna servo system operating means - Google Patents
Movable type satellite communication earth station antenna servo system operating means Download PDFInfo
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- CN202929409U CN202929409U CN 201220655745 CN201220655745U CN202929409U CN 202929409 U CN202929409 U CN 202929409U CN 201220655745 CN201220655745 CN 201220655745 CN 201220655745 U CN201220655745 U CN 201220655745U CN 202929409 U CN202929409 U CN 202929409U
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- satellite communication
- earth station
- communication earth
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- sky
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Abstract
Disclosed is a movable type satellite communication earth station antenna servo system operating means, comprising a button operating circuit, an operating information access circuit connected to the button operating circuit, and a data storage circuit used for storing the satellite parameters corresponding to the movable type satellite communication earth station, wherein the button operating circuit, the operating information access circuit, and the data storage circuit are all connected with an antenna control unit in the movable type satellite communication earth station antenna servo system. The movable type satellite communication earth station antenna servo system operating means of the utility model features simple structure, reasonable design, easy realization, convenient operation, high operating reliability and stability, and lower cost. The movable type satellite communication earth station antenna servo system operating means does not break the original operation of the prior art, and is applicable to the operation of the portable and vehicle-loaded satellite communication earth station antenna servo system with high practicality and good usage effect, thereby being easy to promote.
Description
Technical field
The utility model relates to technical field of satellite communication, especially relates to a kind of mobile satellite communication earth station sky and watches system's operating means.
Background technology
The mobile satellite communication earth station is widely used in accident emergency disposal process, opens the emergency satellite communication link, for organizing and directing of emergency disposal provides communication support.The mobile satellite communication earth station generally all moves under the environment of condition very severe.Mobile satellite communication earth station sky is watched system's running control and is all adopted software interface in the market, and keyboard or soft switch click mode operate, although automaticity is high, and the operation more complicated, master by non-professional persons is got up more difficult; It is start-up routine that general process is controlled in the operation of mobile satellite communication earth station, and antenna launches, and seeks the setting of star parameter, automatic star-seeking, and the antenna collection, and all rely on interface menu selection and menu redirect to realize, process is comparatively complicated.
The utility model content
Technical problem to be solved in the utility model is for above-mentioned deficiency of the prior art, provide a kind of mobile satellite communication earth station sky to watch system's operating means, it is simple in structure, and is reasonable in design, and it is convenient to realize, easy and simple to handle, operational reliability and stability are high, save cost, and is practical, result of use is good, is convenient to promote the use of.
For solving the problems of the technologies described above, the technical solution adopted in the utility model is: system's operating means is watched in a kind of mobile satellite communication earth station sky, it is characterized in that: comprise button operation circuit and the operation information place in circuit that joins with the button operation circuit, and be used for storing mobile formula satellite communication earth station to the data storage circuitry of satellite parametric reduction, described button operation circuit, operation information place in circuit and data storage circuitry all join with the antenna control unit that mobile satellite communication earth station sky is watched in system.
System's operating means is watched in above-mentioned mobile satellite communication earth station sky, and it is characterized in that: described button operation circuit is made of three buttons, and three described buttons are respectively antenna and launch button, automatic star-seeking button and antenna collection button.
System's operating means is watched in above-mentioned mobile satellite communication earth station sky, it is characterized in that: described operation information place in circuit is by the level control circuit that joins with described antenna control unit and connect circuit with the time-delay that described level control circuit joins and consist of, and described button operation circuit joins with described time-delay connection circuit.
System's operating means is watched in above-mentioned mobile satellite communication earth station sky, and it is characterized in that: described data storage circuitry is programmable storage AT24C02A.
system's operating means is watched in above-mentioned mobile satellite communication earth station sky, it is characterized in that: described antenna control unit comprises with mobile satellite communication earth station sky watches the main controller module that system's Satellite beacon receiver joins, the input end of described main controller module is connected to for mobile satellite communication earth station sky being watched the orientation of system's Satellite communication antenna and inclinator that degree of tilt detects and being used for the polarization angular transducer that the polarization angle of system's Satellite communication antenna detects is watched in mobile satellite communication earth station sky, and be used for GPS module and the electronic compass that the geographic position of system's Satellite communication antenna is detected watched in mobile satellite communication earth station sky, the output terminal of described main controller module is connected to the motor driver that drives for to the motor that drives the satellite communication antena running.
System's operating means is watched in above-mentioned mobile satellite communication earth station sky, and it is characterized in that: described main controller module mainly is made of single-chip microcomputer MSP430F149.
The utility model compared with prior art has the following advantages:
1, the utility model circuit structure is simple, and is reasonable in design, and it is convenient to realize.
When 2, the utility model uses, being connected to mobile satellite communication earth station sky watches on antenna control unit in system, easy-to-connect, during operation, launch button, automatic star-seeking button and three button operations of antenna collection button by antenna and can realize that mobile satellite communication earth station sky watches the operation of system and control, compare with mode of operation of the prior art, simplified system's operation, need not professional operating personnel can operate.
3, the utility model operation information place in circuit is made of level control circuit and time-delay connection circuit, has guaranteed the reliability and stability of button operation.
4, the utility model is saved cost, do not destroy original operation in prior art yet, be used for portable, vehicle-mounted quiet communication satellite communication earth station sky and watch the operation that system's running is controlled, can make mobile satellite communication earth station sky watch system controls system and more oversimplifies, practical, result of use is good, is convenient to promote the use of.
In sum, the utility model is simple in structure, and is reasonable in design, and it is convenient, easy and simple to handle to realize, operational reliability and stability are high, save cost, and practical, result of use is good, is convenient to promote the use of.
Below by drawings and Examples, the technical solution of the utility model is described in further detail.
Description of drawings
Fig. 1 is schematic block circuit diagram of the present utility model.
Description of reference numerals:
1-button operation circuit; 1-1-antenna launches button; 1-2-automatic star-seeking button;
1-3-antenna collection button; 2-operation information place in circuit; 2-1-level control circuit;
Circuit is connected in 2-2-time-delay; 3-data storage circuitry; 4-antenna control unit;
4-1-main controller module; 4-2-inclinator; 4-3-polarization angular transducer;
4-4-GPS module; 4-5-electronic compass; 4-6-motor driver;
5-satellite beacon receiver; 6-motor.
Embodiment
As shown in Figure 1, the utility model comprises button operation circuit 1 and the operation information place in circuit 2 that joins with button operation circuit 1, and be used for storing mobile formula satellite communication earth station to the data storage circuitry 3 of satellite parametric reduction, described button operation circuit 1, operation information place in circuit 2 and data storage circuitry 3 all join with the antenna control unit 4 that mobile satellite communication earth station sky is watched in system.
As shown in Figure 1, in the present embodiment, described button operation circuit 1 is made of three buttons, and three described buttons are respectively, and antenna launches button 1-1, automatic star-seeking button 1-2 and antenna is collected button 1-3.Described operation information place in circuit 2 is by the level control circuit 2-1 that joins with described antenna control unit 4 and connect circuit 2-2 with the time-delay that described level control circuit 2-1 joins and consist of, and described button operation circuit 1 is connected circuit 2-2 with described time-delay and joined.Described data storage circuitry 3 is programmable storage AT24C02A.
as shown in Figure 1, in the present embodiment, described antenna control unit 4 comprises with mobile satellite communication earth station sky watches the main controller module 4-1 that system's Satellite beacon receiver 5 joins, the input end of described main controller module 4-1 is connected to for mobile satellite communication earth station sky being watched the orientation of system's Satellite communication antenna and inclinator 4-2 that degree of tilt detects and being used for the polarization angular transducer 4-3 that the polarization angle of system's Satellite communication antenna detects is watched in mobile satellite communication earth station sky, and be used for GPS module 4-4 and the electronic compass 4-5 that the geographic position of system's Satellite communication antenna is detected watched in mobile satellite communication earth station sky, the output terminal of described main controller module 4-1 is connected to the motor driver 4-6 that drives for to the motor 6 that drives the satellite communication antena running.Concrete, described main controller module 4-1 mainly is made of single-chip microcomputer MSP430F149.
during concrete enforcement, antenna launches button 1-1, automatic star-seeking button 1-2 and antenna collection button 1-3 accesses respectively fracture in the I/O of main controller module 4-1 in antenna control unit 4, antenna launches button 1-1, automatic star-seeking button 1-2 and antenna collection button 1-3 are by connect once next time, be off-state after unclamping, the time span of on-state is controlled by level control circuit 2-1, antenna launches button 1-1, automatic star-seeking button 1-2 and antenna collection button 1-3 are respectively used to transmit the mobile satellite communication earth station antenna to main controller module 4-1 and launch, automatic star-seeking and antenna collection operation information.In the button off-state, it is high level that level control circuit 2-1 keeps the I/O mouth of main controller module 4-1, the I/O mouth ground connection that certain button is connected once corresponding main controller module 4-1 once, level control circuit 2-1 keeps the ground signalling 0.5s time, is convenient to main controller module 4-1 and carries out the operational motion judgement.
Described operation information place in circuit 2 is used for the control of operation information.During concrete enforcement, described level control circuit 2-1 adopts the LM324N integrated operational amplifier to consist of voltage follower, takes out reference voltage U from main controller module 4-1
e, by the driving coupling of routine, be controlled at antenna and launch button 1-1, automatic star-seeking button 1-2 and antenna collection button 1-3 off-state, make the I/O mouth of main controller module 4-1 keep high level (greater than 3.3V).Described time-delay is connected circuit 2-2 and is adopted integrating circuit and realize with the Q trigger that integrating circuit joins, control antenna launches button 1-1, automatic star-seeking button 1-2 and antenna collection button 1-3 on-state, keep low level (OV) time-delay to 0.5S, solve the contradiction that the keyswitch time is short, main controller module 4-1 is difficult to judge, guarantee the reliability of operation.
Described data storage circuitry 3 be mainly used in the storing mobile satellite communication earth station to the parameter of satellite, comprise the beacon frequency of satellite, polarization of the e mode, satellite positioning longitude etc.A general cover mobile satellite communication earth station is only for a telstar job, so this data storage circuitry 3 can for a long time with the station use, if star work need to be changed in this station, can be restored to the parameter modification in data memory circuit 3.
During use, principle of work of the present utility model and the course of work are: after the mobile satellite communication earth station transports the scene to, open the complete machine power supply, main controller module 4-1 has judged whether the button connection signal, if have, judgement is the operation that antenna launches button 1-1, automatic star-seeking button 1-2 and which button of antenna collection button 1-3 again, then carries out respectively corresponding operation.The utility model has realized that by button operation mobile satellite communication earth station sky watches the operation of system and control, and has simplified system's operation.
The above; it is only preferred embodiment of the present utility model; be not that the utility model is imposed any restrictions; every any simple modification, change and equivalent structure of above embodiment being done according to the utility model technical spirit changes, and all still belongs in the protection domain of technical solutions of the utility model.
Claims (6)
1. system's operating means is watched in a mobile satellite communication earth station sky, it is characterized in that: comprise button operation circuit (1) and the operation information place in circuit (2) that joins with button operation circuit (1), and be used for storing mobile formula satellite communication earth station to the data storage circuitry (3) of satellite parametric reduction, described button operation circuit (1), operation information place in circuit (2) and data storage circuitry (3) all join with the antenna control unit (4) that mobile satellite communication earth station sky is watched in system.
2. watch system's operating means according to mobile satellite communication earth station claimed in claim 1 sky, it is characterized in that: described button operation circuit (1) is made of three buttons, and three described buttons are respectively antenna expansion button (1-1), automatic star-seeking button (1-2) and antenna collection button (1-3).
3. watch system's operating means according to mobile satellite communication earth station claimed in claim 1 sky, it is characterized in that: described operation information place in circuit (2) is by the level control circuit (2-1) that joins with described antenna control unit (4) and connect circuit (2-2) with the time-delay that described level control circuit (2-1) joins and consist of, and described button operation circuit (1) is connected circuit (2-2) with described time-delay and joined.
4. watch system's operating means according to mobile satellite communication earth station claimed in claim 1 sky, it is characterized in that: described data storage circuitry (3) is programmable storage AT24C02A.
5. watch system's operating means according to mobile satellite communication earth station claimed in claim 1 sky, it is characterized in that: described antenna control unit (4) comprises with mobile satellite communication earth station sky watches the main controller module (4-1) that system's Satellite beacon receiver (5) joins, the input end of described main controller module (4-1) is connected to for mobile satellite communication earth station sky being watched the orientation of system's Satellite communication antenna and inclinator (4-2) that degree of tilt detects and being used for the polarization angular transducer (4-3) that the polarization angle of system's Satellite communication antenna detects is watched in mobile satellite communication earth station sky, and be used for GPS module (4-4) and the electronic compass (4-5) that the geographic position of system's Satellite communication antenna is detected watched in mobile satellite communication earth station sky, the output terminal of described main controller module (4-1) is connected to the motor driver (4-6) that drives for to the motor (6) that drives the satellite communication antena running.
6. watch system's operating means according to mobile satellite communication earth station claimed in claim 5 sky, it is characterized in that: described main controller module (4-1) mainly is made of single-chip microcomputer MSP430F149.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220655745 CN202929409U (en) | 2012-11-30 | 2012-11-30 | Movable type satellite communication earth station antenna servo system operating means |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220655745 CN202929409U (en) | 2012-11-30 | 2012-11-30 | Movable type satellite communication earth station antenna servo system operating means |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202929409U true CN202929409U (en) | 2013-05-08 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201220655745 Expired - Fee Related CN202929409U (en) | 2012-11-30 | 2012-11-30 | Movable type satellite communication earth station antenna servo system operating means |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202929409U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103715505A (en) * | 2013-12-19 | 2014-04-09 | 北京航天科工世纪卫星科技有限公司 | Semi-automatic portable satellite communication antenna |
| CN104932532A (en) * | 2015-05-05 | 2015-09-23 | 南京中网卫星通信股份有限公司 | Backpack type satellite communication portable station control device and application method thereof |
-
2012
- 2012-11-30 CN CN 201220655745 patent/CN202929409U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103715505A (en) * | 2013-12-19 | 2014-04-09 | 北京航天科工世纪卫星科技有限公司 | Semi-automatic portable satellite communication antenna |
| CN104932532A (en) * | 2015-05-05 | 2015-09-23 | 南京中网卫星通信股份有限公司 | Backpack type satellite communication portable station control device and application method thereof |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C56 | Change in the name or address of the patentee |
Owner name: SHAANXI OSAI COMMUNICATION SCIENCE + TECHNOLOGY CO Free format text: FORMER NAME: XI'AN OSAI COMMUNICATION SCIENCE + TECHNOLOGY CO., LTD. |
|
| CP01 | Change in the name or title of a patent holder |
Address after: 710065 Shaanxi city of Xi'an province high tech Zone Road No. 89 Fenglin Oasis Park Building No. 9 room 10904 Genting Patentee after: SHAANXI XIOUSAI COMMUNICATION SCIENCE TECHNOLOGY CO., LTD. Address before: 710065 Shaanxi city of Xi'an province high tech Zone Road No. 89 Fenglin Oasis Park Building No. 9 room 10904 Genting Patentee before: Xi'an Osai Communication Science & Technology Co., Ltd. |
|
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20130508 Termination date: 20181130 |