CN106338929A - Multi-type test parameter unified index modeling method - Google Patents
Multi-type test parameter unified index modeling method Download PDFInfo
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- CN106338929A CN106338929A CN201610643450.1A CN201610643450A CN106338929A CN 106338929 A CN106338929 A CN 106338929A CN 201610643450 A CN201610643450 A CN 201610643450A CN 106338929 A CN106338929 A CN 106338929A
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- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B17/00—Systems involving the use of models or simulators of said systems
- G05B17/02—Systems involving the use of models or simulators of said systems electric
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Abstract
The invention provides a multi-type test parameter unified index modeling method. The multi-type test parameter unified index modeling method is successfully applied to the parameter integrated display of the test command and display system of a liquid rocket power system. It is proved that the feasibility and reliability of the method are excellent. With the method adopted, flexible, universal and services easy to operate can be provided for a user, requirements of the user, such as requirements for real-time display, query and comparison of test parameters can be satisfied quickly and conveniently. The method includes the following steps that: first step, a test parameter index management framework is constructed according to the test characteristics of the liquid rocket power system, for example, an acquisition server, system management information and test information classification are defined; second step, the test information is further subdivided into experimental acquisition parameters, processing chart parameters and video information parameters; third step, the test parameters are grouped according to systems, and the acquisition server and channels are configured; and fourth step, display attribute configuration is carried out for parameters required to be displayed, for example, special alarm, special display, curve comparison and the like can be configured.
Description
Technical field
Present invention is mainly used for the observing and controlling of liquid rocket power (electromotor) system test and commander field.
Background technology
With the development of China's Aerospace Technology, in Space radiation test, measurement and control system become increasingly complex,
The thing followed is all types of acquisition parameter increasing number, required precision raising, and the parameter being supplied to pilot command personnel is shown
Show that system is also just put forward higher requirement.Especially the development of China's new generation's carrier rocket cz-6, cz-7 and cz-5 and after
The features such as supervention exhibition assumes cycle is short, technical requirements are high, Information Meter is highly integrated, therefore it is required that pilot command display system will possess
Modularity, standardized feature, can rapidly adapt to the demand of different model test, do urgent problems among these and be intended to set up work
The multisystems such as skill, measurement and control, the standard of multiclass shape parameter unitize, that is, set up test parameterss index physical model.
Content of the invention
The purpose of the present invention is to propose to a kind of method of polymorphic type test parameterss unified metric modeling, and it is successfully applied to liquid
The parameter integrative display of body Rocket propulsion system pilot command display system is it was demonstrated that it has good feasibility and reliability, energy
Enough provide the user with flexible, general, easy-operating service, especially quickly, easily can meet user to test parameterss
Real-time query, show and compare peer-on-demand.
A kind of method of polymorphic type test parameterss unified metric modeling, comprises the following steps:
The first step, according to liquid rocket dynamical system test features, sets up parameter system framework, such as definition collection service
Device, system management messages and Test Information classification；
Second step, segments further to Test Information, is divided into test acquisition parameter, technique graph parameter and video information ginseng
Number；
Test parameterss are carried out packet configuration parameter acquisition server and passage by system by the 3rd step；
4th step, carries out display properties configuration to the parameter needing display, such as special alert, Special display, curve comparison
Deng.
Beneficial effects of the present invention:
The present invention is using a kind of general, flexible parameter index modeling method, numerous and diverse during Rocket propulsion system is tested
Parameter shows and adjusts work becomes easy, user can be made comprehensively, quickly to understand trystate and control test process, reduce and use
Family work difficulty, mitigation workload, efficiently reduce test and prepare and debug time.
Brief description
Fig. 1 is the method flow schematic diagram of the polymorphic type test parameterss unified metric modeling of the present invention.
Specific embodiment
The realization of polymorphic type test parameterss unified metric modeling method, is real-time in liquid rocket dynamical system test parameterss
It is applied in transfer display system and verifies it now is possible to be promoted as a kind of universal method.It includes following reality
Apply step:
The first step, parameter index management modeling, according to experimental technique documentation requirements, Test Information is classified and is joined
Put, such as definition adopt data set server, defined parameters packet, configuration parameter display properties and with technique graph parameter mapping relations
Etc. content, form achievement data physical model；
Second step, system detectio monitors, using during test matching test, by the detection monitoring tools of system, profit
Check reasonability, the effectiveness of the configuration of each data acquisition sender and this system with the physical model of INDEX MANAGEMENT configuration；
3rd step, direct broadcast service detects, before the test during phase matching test and heat run, using INDEX MANAGEMENT configuration
Physical model first determine whether parameter whether from effective acquisition server, whether by effective form sending, then
The data parameters in effectively source are transmitted to storage service and client；
4th step, storage service, live data is parsed according to physical model, stores test parameterss data base；
5th step, parameter display terminal, using INDEX MANAGEMENT configuration physical model control displaying control represent effect,
Show content, parsing live data or extraction parsing order program data, then shown.
The non-detailed description of the present invention is known to the skilled person technology.
Claims (1)
1. a kind of method of polymorphic type test parameterss unified metric modeling, comprises the following steps:
The first step, according to liquid rocket dynamical system test features, sets up parameter system framework, such as defines acquisition server, is
System management information and Test Information classification；
Second step, segments further to Test Information, is divided into test acquisition parameter, technique graph parameter and video information parameter；
Test parameterss are carried out packet configuration parameter acquisition server and passage by system by the 3rd step；
4th step, carries out display properties configuration to the parameter needing display, such as special alert, Special display, curve ratio equity.
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| Application Number | Priority Date | Filing Date | Title |
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| CN201610643450.1A CN106338929A (en) | 2016-08-09 | 2016-08-09 | Multi-type test parameter unified index modeling method |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201610643450.1A CN106338929A (en) | 2016-08-09 | 2016-08-09 | Multi-type test parameter unified index modeling method |
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| CN106338929A true CN106338929A (en) | 2017-01-18 |
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Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101576440A (en) * | 2009-06-22 | 2009-11-11 | 北京航空航天大学 | Virtual testing platform of liquid rock engine and testing method thereof |
| US20090312882A1 (en) * | 2008-06-16 | 2009-12-17 | Hammerbeck Warren John | Systems and methods for automated simulation of a propulsion system and testing of propulsion control systems |
| CN101865182A (en) * | 2010-07-19 | 2010-10-20 | 中国航空工业集团公司西安飞机设计研究所 | Airplane hydraulic test distributed test system and method thereof |
| CN102033998A (en) * | 2010-12-10 | 2011-04-27 | 北京航空航天大学 | Method for automatically generating reliability model |
| CN105653754A (en) * | 2014-12-05 | 2016-06-08 | 内蒙航天动力机械测试所 | Solid rocket engine virtual test base system and testing method |
-
2016
- 2016-08-09 CN CN201610643450.1A patent/CN106338929A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20090312882A1 (en) * | 2008-06-16 | 2009-12-17 | Hammerbeck Warren John | Systems and methods for automated simulation of a propulsion system and testing of propulsion control systems |
| CN101576440A (en) * | 2009-06-22 | 2009-11-11 | 北京航空航天大学 | Virtual testing platform of liquid rock engine and testing method thereof |
| CN101865182A (en) * | 2010-07-19 | 2010-10-20 | 中国航空工业集团公司西安飞机设计研究所 | Airplane hydraulic test distributed test system and method thereof |
| CN102033998A (en) * | 2010-12-10 | 2011-04-27 | 北京航空航天大学 | Method for automatically generating reliability model |
| CN105653754A (en) * | 2014-12-05 | 2016-06-08 | 内蒙航天动力机械测试所 | Solid rocket engine virtual test base system and testing method |
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Application publication date: 20170118 |