CN203084490U - Carrier rocket pre-launching monitoring system - Google Patents
Carrier rocket pre-launching monitoring system Download PDFInfo
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- CN203084490U CN203084490U CN 201320029926 CN201320029926U CN203084490U CN 203084490 U CN203084490 U CN 203084490U CN 201320029926 CN201320029926 CN 201320029926 CN 201320029926 U CN201320029926 U CN 201320029926U CN 203084490 U CN203084490 U CN 203084490U
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- server
- data processing
- network switch
- carrier rocket
- monitoring
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Abstract
The utility model discloses a carrier rocket pre-launching monitoring system. The carrier rocket monitoring system comprises a data processing server, a data publishing server, a display browse terminal and a network switch, wherein the data processing server and the data publishing server are connected with the display browse terminal through the network switch. The carrier rocket monitoring system employs browser / server mode (B/S mode) monitoring information processing and displaying technology. When the monitoring parameter increases and decreases or the monitoring parameter criterion changes, only the data processing server and the data publishing server related software have to be changed. WEB technology is employed to publish parameters, and IE standard browser is employed to browse client information. Use and maintenance are more convenient. A threshold analysis method with multiple-parameter combined determination is employed to determine related parameters in combined manner according to the requirements of related subsystems of carrier rocket pre-launching, thereby satisfying the complex judgment with coupling relationship in the subsystem parameters.
Description
Technical field
The present invention relates to a kind of carrier rocket and penetrate preceding monitoring system, relate in particular to a kind of carrier rocket of browser/server pattern that adopts and penetrate preceding monitoring system, be mainly used in the preceding information monitoring of carrier rocket emission, belong to the observation and control technology field.
Background technology
Monitoring is before rocket is about to blast off each system of rocket to be carried out last analysis-by-synthesis before penetrating, and is the main means of aid decision making emission and the important step of guaranteeing the launch mission success.Monitoring technology is meant in order in time, accurately to find fault before carrier rocket faces emission, a technology of during " 30min " to " igniting " crucial telemetry parameter being monitored in real time before penetrating before the carrier rocket emission.
Monitoring information is handled and is shown and adopts Client (C/S model) before the carrier rocket emission at present, client need install special use penetrate before the monitoring software for display, when monitoring parameter increase and decrease or the variation of monitoring parameter criterion, need to revise and monitor software for display and Installation and Debugging again, inconvenient operation and maintenance before special use is penetrated.On the other hand, the monitoring parameter method of discrimination adopts limit value to judge that method is according to the parameter bound data to be judged before penetrating at present, and the method is applicable to the judgement of simple parameter data, can not be used for having between parameter the complexity judgement of coupled relation.
The utility model content
The technical matters that the utility model solves is: overcome the deficiencies in the prior art, provide a kind of carrier rocket to penetrate preceding monitoring system, adopt browser/server pattern (B/S pattern), the WEB technology is adopted in the parameter issue, client-side information is browsed and is used the IE standard browser, and operation and maintenance is convenient.
The technical solution of the utility model is: a kind of carrier rocket is penetrated preceding monitoring system, comprises data processing server, data distribution server, display navigation terminal and the network switch; All be connected between data processing server, the data distribution server and between the display navigation terminal by the network switch, data processing server receives the telemetry A that the telemetry server produces by the network switch, by the network switch Telemetering Data Processing information B that produces is sent to data distribution server; Data distribution server receives the Telemetering Data Processing information B that data processing server sends by the network switch, according to the browser/server pattern the crucial telemetry parameter C among the Telemetering Data Processing information B is carried out real-time release, the display navigation terminal is carried out browse displays to the crucial telemetry parameter C that receives by the network switch.
The utility model compared with prior art has following beneficial effect: the utility model adopts browser/server pattern (B/S pattern) monitoring information to handle and display technique, when monitoring parameter increase and decrease or the variation of monitoring parameter criterion, only need to revise data processing server and data distribution server related software, the WEB technology is adopted in the parameter issue, client-side information is browsed and is used the IE standard browser, and operation and maintenance is convenient; The utility model adopts multiparameter to unite the range analysis method of judgement, and the relevant subsystem requirement of monitoring before penetrating according to carrier rocket to the method for correlation parameter employing associating judgement, has been satisfied the complexity that has coupled relation in the subsystem parameter and judged.
Description of drawings
Fig. 1 is a composition structural drawing of the present utility model.
Embodiment
The utility model is described in more detail below in conjunction with the drawings and specific embodiments:
As shown in Figure 1, the utility model comprises data processing server, data distribution server, display navigation terminal and the network switch, all be connected between data processing server, the data distribution server and between the display navigation terminal by the network switch, data processing server receives the telemetry A that the telemetry server produces by the network switch, by the network switch Telemetering Data Processing information B that produces is sent to data distribution server; Data distribution server receives the Telemetering Data Processing information B that data processing server sends by the network switch, according to the browser/server pattern the crucial telemetry parameter C among the Telemetering Data Processing information B is carried out real-time release, the display navigation terminal is carried out browse displays to the crucial telemetry parameter C that receives by the network switch.
Telemetry server: be used for outwards sending each subsystem data A of rocket that telemetry system measures; Data processing server:, each the subsystem telemetry A of rocket that receives is handled in real time and analyzes, and the Telemetering Data Processing information B after will handling offers data distribution server according to correlation discriminating method or criterion; Data distribution server: handle in real time and analysis result according to data processing server,, crucial telemetry parameter C among the Telemetering Data Processing information B is carried out real-time release according to browser/server pattern (B/S pattern); Display navigation terminal: be used for crucial telemetry parameter C is carried out browse displays.
The specifying information flow specification is as follows:
(1) in test and the emission process, the telemetry server sends each subsystem data A of rocket that telemetry system measures;
(2) after data processing server receives telemetry server transmission information A, according to correlation discriminating method or criterion, the telemetry that receives is handled and analysis obtains Telemetering Data Processing information B in real time, the Telemetering Data Processing information B that produces is sent to data distribution server by the network switch;
(3) after data distribution server receives Telemetering Data Processing information B, according to browser/server pattern (B/S pattern), crucial telemetry parameter C among the Telemetering Data Processing information B is carried out real-time release, and the WEB technology is adopted in the parameter issue, and client-side information is browsed and used the IE standard browser;
(4) the display navigation terminal is finished and is penetrated preceding Monitoring Data display navigation by the crucial telemetry parameter C among the network switch reception Telemetering Data Processing information B.
To adopt multiparameter to unite the range analysis method of judgement as shown in table 1 in monitoring before penetrating.
The monitoring multiparameter was united the range analysis method of judgement before table 1 was penetrated
The utility model not detailed description is a technology as well known to those skilled in the art.
Claims (1)
1. a carrier rocket is penetrated preceding monitoring system, it is characterized in that: comprise data processing server, data distribution server, display navigation terminal and the network switch; All be connected between data processing server, the data distribution server and between the display navigation terminal by the network switch, data processing server receives the telemetry A that the telemetry server produces by the network switch, by the network switch Telemetering Data Processing information B that produces is sent to data distribution server; Data distribution server receives the Telemetering Data Processing information B that data processing server sends by the network switch, according to the browser/server pattern the crucial telemetry parameter C among the Telemetering Data Processing information B is carried out real-time release, the display navigation terminal is carried out browse displays to the crucial telemetry parameter C that receives by the network switch.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201320029926 CN203084490U (en) | 2013-01-21 | 2013-01-21 | Carrier rocket pre-launching monitoring system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201320029926 CN203084490U (en) | 2013-01-21 | 2013-01-21 | Carrier rocket pre-launching monitoring system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203084490U true CN203084490U (en) | 2013-07-24 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201320029926 Expired - Lifetime CN203084490U (en) | 2013-01-21 | 2013-01-21 | Carrier rocket pre-launching monitoring system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203084490U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103487271A (en) * | 2013-09-24 | 2014-01-01 | 北京宇航系统工程研究所 | Fault diagnosis system of carrier rocket |
| CN104601611A (en) * | 2013-10-30 | 2015-05-06 | 北京临近空间飞行器系统工程研究所 | Browse issue system and method based on data real-time filtering |
| CN112556514A (en) * | 2020-12-08 | 2021-03-26 | 北京航天发射技术研究所 | Remote state monitoring system for heavy carrier rocket launching support equipment |
-
2013
- 2013-01-21 CN CN 201320029926 patent/CN203084490U/en not_active Expired - Lifetime
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103487271A (en) * | 2013-09-24 | 2014-01-01 | 北京宇航系统工程研究所 | Fault diagnosis system of carrier rocket |
| CN104601611A (en) * | 2013-10-30 | 2015-05-06 | 北京临近空间飞行器系统工程研究所 | Browse issue system and method based on data real-time filtering |
| CN104601611B (en) * | 2013-10-30 | 2017-11-28 | 北京临近空间飞行器系统工程研究所 | It is a kind of that dissemination method is browsed based on data real time filtering |
| CN112556514A (en) * | 2020-12-08 | 2021-03-26 | 北京航天发射技术研究所 | Remote state monitoring system for heavy carrier rocket launching support equipment |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CX01 | Expiry of patent term |
Granted publication date: 20130724 |
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| CX01 | Expiry of patent term |