CN113433848A - Remote measurement and control method and system for airplane secondary energy test - Google Patents
Remote measurement and control method and system for airplane secondary energy test Download PDFInfo
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- CN113433848A CN113433848A CN202110608247.1A CN202110608247A CN113433848A CN 113433848 A CN113433848 A CN 113433848A CN 202110608247 A CN202110608247 A CN 202110608247A CN 113433848 A CN113433848 A CN 113433848A
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- 238000005259 measurement Methods 0.000 title claims abstract description 140
- 238000012360 testing method Methods 0.000 title claims abstract description 137
- 238000000034 method Methods 0.000 title claims abstract description 24
- 238000012545 processing Methods 0.000 claims abstract description 19
- 239000000446 fuel Substances 0.000 claims abstract description 17
- 238000012544 monitoring process Methods 0.000 claims abstract description 6
- 230000007613 environmental effect Effects 0.000 claims description 6
- 230000005540 biological transmission Effects 0.000 claims description 4
- ORILYTVJVMAKLC-UHFFFAOYSA-N Adamantane Natural products C1C(C2)CC3CC1CC2C3 ORILYTVJVMAKLC-UHFFFAOYSA-N 0.000 claims description 3
- 238000012800 visualization Methods 0.000 claims description 3
- 239000000835 fiber Substances 0.000 claims 1
- 238000010276 construction Methods 0.000 abstract description 3
- 238000010586 diagram Methods 0.000 description 2
- 239000013307 optical fiber Substances 0.000 description 2
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 230000017525 heat dissipation Effects 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 238000004088 simulation Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
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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
- G05B19/00—Programme-control systems
- G05B19/02—Programme-control systems electric
- G05B19/04—Programme control other than numerical control, i.e. in sequence controllers or logic controllers
- G05B19/042—Programme control other than numerical control, i.e. in sequence controllers or logic controllers using digital processors
- G05B19/0423—Input/output
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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
- G05B2219/00—Program-control systems
- G05B2219/20—Pc systems
- G05B2219/23—Pc programming
- G05B2219/23051—Remote control, enter program remote, detachable programmer
Abstract
The application belongs to the technical field of airplane comprehensive tests and relates to a remote measurement and control method and system for airplane secondary energy tests. The remote measurement and control method comprises the following steps: s1, acquiring measurement and control data sent by the fuel test environment measurement and control system, the hydraulic test environment measurement and control system, the power supply test environment measurement and control system, the environment control test environment measurement and control system and the comprehensive test system; step S2, processing the measurement and control data according to the preset test process management steps; and step S3, sending the processed data to corresponding measurement and control systems through the high-speed network interface according to the requirements of the measurement and control systems. The application makes full use of the existing test environment resources, reduces the system hardware construction, and forms a set of comprehensive measurement and control system capable of monitoring a plurality of airborne energy systems in real time by scheduling the existing measurement and control system environment resources.
Description
Technical Field
The application belongs to the technical field of airplane comprehensive tests, and particularly relates to a remote measurement and control method and system for an airplane secondary energy test.
Background
The secondary energy system of the airplane relates to each link of energy generation, distribution, transmission, conversion, use and the like, provides energy sources such as machine, electricity, liquid, gas and the like for a mission system, a weapon system, a flight control system and the like on the airplane, and simultaneously finishes the heat dissipation of the airplane.
Disclosure of Invention
In order to solve the above problems, the present application provides an onboard real-time thermal equivalent simulation method and system, which can effectively implement unified management and scheduling of measurement and control systems in test environments of multiple locations, and can comprehensively acquire, store, analyze and process data of the measurement and control systems in each test environment.
The application provides in a first aspect a remote measurement and control method for aircraft secondary energy tests, mainly including:
s1, acquiring measurement and control data sent by the fuel test environment measurement and control system, the hydraulic test environment measurement and control system, the power supply test environment measurement and control system, the environment control test environment measurement and control system and the comprehensive test system;
step S2, processing the measurement and control data according to the preset test process management steps;
and step S3, sending the processed data to corresponding measurement and control systems through the high-speed network interface according to the requirements of the measurement and control systems.
Preferably, in step S2, the processing of the measurement and control data includes recording and storing, real-time monitoring, and visualization processing of the measurement and control data.
Preferably, in step S2, the processing the measurement and control data includes:
the global knowledge management is used for calling global knowledge;
the test environment management is used for building a test environment;
the test process management is used for respectively controlling the operation of the fuel test environment measurement and control system, the hydraulic test environment measurement and control system, the power supply test environment measurement and control system, the environment control test environment measurement and control system and the comprehensive test system according to preset test steps and reading measurement and control data;
and the test reconstruction tracing is used for reconstructing the test and tracing the data.
The second aspect of the application provides a long-range system of observing and controling for aircraft secondary energy is experimental, mainly includes:
the data acquisition module is used for acquiring measurement and control data sent by the fuel test environment measurement and control system, the hydraulic test environment measurement and control system, the power supply test environment measurement and control system, the environment control test environment measurement and control system and the comprehensive test system;
the data processing module is used for processing the measurement and control data according to preset test process management steps;
the data transmission module is used for transmitting the processed data to the corresponding measurement and control system through the high-speed network interface according to the requirement of each measurement and control system;
the remote measurement and control system is connected with the fuel test environment measurement and control system, the hydraulic test environment measurement and control system, the power supply test environment measurement and control system, the environment measurement and control system and the comprehensive test system through the high-speed network interface system.
Preferably, the remote measurement and control system is built by adopting a porphyry industrial personal computer 610L series.
Preferably, the high-speed network interface system is erected by using Huacheng gigabit network switches and optical fiber cables.
Preferably, the fuel test environment measurement and control system is constructed by adopting PXIe-4302 of the NI company in America.
Preferably, the hydraulic test environment measurement and control system is constructed by adopting PXI-1308 or PXI-1338 of the NI company in America.
Preferably, the power supply test environment measurement and control system is constructed by adopting TB-4300 of the NI company in America.
Preferably, the environmental measurement and control system of the environmental control test is constructed by adopting TB-4302C, PXIe-4302, PXI-8433 and Tuhua ADAM modules of the NI company in America.
Preferably, the comprehensive test system (7) is constructed by adopting PXI-8433 and PXIe-4302.
The application makes full use of the existing test environment resources, reduces the system hardware construction, and forms a set of comprehensive measurement and control system capable of monitoring a plurality of airborne energy systems in real time by scheduling the existing measurement and control system environment resources.
Drawings
FIG. 1 is a system architecture diagram of a preferred embodiment of the remote measurement and control system for aircraft secondary energy testing according to the present application.
FIG. 2 is a schematic diagram of the system connections of the embodiment of FIG. 1 of the present application.
Detailed Description
In order to make the implementation objects, technical solutions and advantages of the present application clearer, the technical solutions in the embodiments of the present application will be described in more detail below with reference to the accompanying drawings in the embodiments of the present application. In the drawings, the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. The described embodiments are some, but not all embodiments of the present application. The embodiments described below with reference to the drawings are exemplary and intended to be used for explaining the present application, and should not be construed as limiting the present application. All other embodiments obtained by a person of ordinary skill in the art without any inventive work based on the embodiments in the present application are within the scope of protection of the present application. Embodiments of the present application will be described in detail below with reference to the drawings.
The application provides in a first aspect a remote measurement and control method for aircraft secondary energy tests, mainly including:
s1, acquiring measurement and control data sent by the fuel test environment measurement and control system, the hydraulic test environment measurement and control system, the power supply test environment measurement and control system, the environment control test environment measurement and control system and the comprehensive test system;
step S2, processing the measurement and control data according to the preset test process management steps;
and step S3, sending the processed data to corresponding measurement and control systems through the high-speed network interface according to the requirements of the measurement and control systems.
In some optional embodiments, as shown in fig. 2, in step S2, the processing of the measurement and control data includes recording and storing, real-time monitoring, and visualization processing of the measurement and control data.
In some optional embodiments, as shown in fig. 2, in step S2, the processing the measurement and control data includes:
the global knowledge management is used for calling global knowledge;
the test environment management is used for building a test environment;
the test process management is used for respectively controlling the operation of the fuel test environment measurement and control system, the hydraulic test environment measurement and control system, the power supply test environment measurement and control system, the environment control test environment measurement and control system and the comprehensive test system according to preset test steps and reading measurement and control data;
and the test reconstruction tracing is used for reconstructing the test and tracing the data.
The second aspect of the present application provides a remote measurement and control system for an aircraft secondary energy test corresponding to the above method, as shown in fig. 1, mainly including:
the data acquisition module is used for acquiring measurement and control data sent by the fuel test environment measurement and control system, the hydraulic test environment measurement and control system, the power supply test environment measurement and control system, the environment control test environment measurement and control system and the comprehensive test system;
the data processing module is used for processing the measurement and control data according to preset test process management steps;
the data transmission module is used for transmitting the processed data to the corresponding measurement and control system through the high-speed network interface according to the requirement of each measurement and control system;
the remote measurement and control system is connected with the fuel test environment measurement and control system, the hydraulic test environment measurement and control system, the power supply test environment measurement and control system, the environment measurement and control system and the comprehensive test system through the high-speed network interface system.
In some optional embodiments, the remote measurement and control system is built using the porphyry industrial personal computer 610L series. The high-speed network interface system is erected by adopting Huacheng kilomega network switch and optical fiber cables. The fuel test environment measurement and control system is constructed by adopting PXIe-4302 of the American NI company. The hydraulic test environment measurement and control system is constructed by adopting PXI-1308 or PXI-1338 of the NI company in America. The power supply test environment measurement and control system is constructed by adopting TB-4300 of the American NI company. The environmental measurement and control system for the environmental control test is constructed by adopting TB-4302C, PXIe-4302, PXI-8433 and Tuhua ADAM modules of the American NI company.
As shown in fig. 2, a plurality of system test environments of the aircraft are distributed in each plant, and because the system is huge, the system cannot be intensively built at present, in order to better realize comprehensive measurement and control of the energy of the secondary energy system, a set of measurement and control system capable of realizing remote test and comprehensive management and control is constructed, and the hardware resources of the existing test environment are effectively combined to realize comprehensive test and control of the energy of each system of the aircraft. Through the unified allocation and comprehensive configuration of the test environment management and test process management system, the control scheduling of the original measurement and control system of the fuel test environment, the hydraulic test environment, the environment control test environment and the power supply test environment is realized, the unified storage and management of a plurality of system test data are realized through the comprehensive measurement and control system, through the high-speed network system, each environment test data can be effectively subjected to data interaction and comprehensive display, and effective data resources are provided for the test and research of a secondary energy system.
Due to the adoption of the scheme, the existing test environment resources are fully utilized, the system hardware construction is reduced, and a set of comprehensive measurement and control system capable of monitoring a plurality of airborne energy systems in real time is formed by scheduling the existing measurement and control system environment resources.
The above description is only for the specific embodiments of the present application, but the scope of the present application is not limited thereto, and any changes or substitutions that can be easily conceived by those skilled in the art within the technical scope of the present application should be covered within the scope of the present application. Therefore, the protection scope of the present application shall be subject to the protection scope of the claims.
Claims (10)
1. A remote measurement and control method for an aircraft secondary energy test is characterized by comprising the following steps:
s1, acquiring measurement and control data sent by the fuel test environment measurement and control system, the hydraulic test environment measurement and control system, the power supply test environment measurement and control system, the environment control test environment measurement and control system and the comprehensive test system;
step S2, processing the measurement and control data according to the preset test process management steps;
and step S3, sending the processed data to corresponding measurement and control systems through the high-speed network interface according to the requirements of the measurement and control systems.
2. The remote measurement and control method for the aircraft secondary energy test as claimed in claim 1, wherein in step S2, the processing of the measurement and control data includes recording and storing, real-time monitoring and visualization processing of the measurement and control data.
3. The remote measurement and control method for the aircraft secondary energy test as claimed in claim 2, wherein in step S2, the processing of the measurement and control data comprises:
the global knowledge management is used for calling global knowledge;
the test environment management is used for building a test environment;
the test process management is used for respectively controlling the operation of the fuel test environment measurement and control system, the hydraulic test environment measurement and control system, the power supply test environment measurement and control system, the environment control test environment measurement and control system and the comprehensive test system according to preset test steps and reading measurement and control data;
and the test reconstruction tracing is used for reconstructing the test and tracing the data.
4. The utility model provides a long-range system of observing and controling for aircraft secondary energy is experimental which characterized in that includes:
the data acquisition module is used for acquiring measurement and control data sent by the fuel test environment measurement and control system, the hydraulic test environment measurement and control system, the power supply test environment measurement and control system, the environment control test environment measurement and control system and the comprehensive test system;
the data processing module is used for processing the measurement and control data according to preset test process management steps;
the data transmission module is used for transmitting the processed data to the corresponding measurement and control system through the high-speed network interface according to the requirement of each measurement and control system;
the remote measurement and control system is connected with the fuel test environment measurement and control system, the hydraulic test environment measurement and control system, the power supply test environment measurement and control system, the environment measurement and control system and the comprehensive test system through the high-speed network interface system.
5. The remote measurement and control system for the secondary energy test of the airplane as claimed in claim 4, wherein the remote measurement and control system is built by adopting 610L series of the Jones industrial personal computer.
6. The remote measurement and control system for aircraft secondary energy tests as claimed in claim 4, wherein the high-speed network interface system is deployed using Huacheng gigabit network switches and fiber optic cables.
7. The remote measurement and control system for the aircraft secondary energy test as claimed in claim 4, wherein the fuel test environment measurement and control system is constructed by adopting PXIe-4302 of the American NI company.
8. The remote measurement and control system for the secondary energy tests of the airplanes according to claim 4, wherein the hydraulic test environment measurement and control system is constructed by PXI-1308 or PXI-1338 of the NI corporation in America.
9. The remote measurement and control system for the secondary energy test of the aircraft as claimed in claim 4, wherein the power supply test environment measurement and control system is constructed by TB-4300 of American NI.
10. The remote measurement and control system for the secondary energy tests of airplanes according to claim 4, wherein the environmental measurement and control system for the environmental control tests is constructed by using TB-4302C, PXIe-4302, PXI-8433, and Mowa ADAM modules of the American NI company.
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