CN111071481A - Universal test platform integration method and system - Google Patents
Universal test platform integration method and system Download PDFInfo
- Publication number
- CN111071481A CN111071481A CN202010003195.0A CN202010003195A CN111071481A CN 111071481 A CN111071481 A CN 111071481A CN 202010003195 A CN202010003195 A CN 202010003195A CN 111071481 A CN111071481 A CN 111071481A
- Authority
- CN
- China
- Prior art keywords
- test
- resources
- target
- specific
- requirements
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/60—Testing or inspecting aircraft components or systems
Abstract
The application relates to a universal test platform integration method and a universal test platform integration system, wherein the method comprises the following steps: acquiring a target test requirement; selecting target universal test resources from the universal test resource set according to target test requirements; selecting target specific test resources from the specific test resource set according to target test requirements; and assembling the target general test resources and the target specific test resources through the interconnection and intercommunication connecting mechanism and the interconnection and intercommunication interface specification to obtain a target test platform, so that the target test platform realizes target test. According to the technical scheme, different test platforms are built in a combined mode to meet different test requirements, and the test resources are assembled through the interconnection and intercommunication connecting mechanism and the interface specification, so that the integrated system is highly compatible, flexibly connected, interconnected and intercommunicated and modularized.
Description
Technical Field
The application relates to the technical field of aviation equipment testing, in particular to a general test platform integration method and system.
Background
In the field of comprehensive testing and diagnosis of aviation equipment, along with the improvement of the function advancement and complexity of an aviation equipment system, the combat efficiency of an aviation aircraft is improved, and meanwhile, a large number of testing and guaranteeing problems are brought. An Automatic Test System (ATS) is important guarantee equipment for improving the combat readiness integrity of aviation equipment and reducing the downtime, and is an important means for ensuring the combat effectiveness of an aviation aircraft. However, the automatic test system of the current aviation equipment in China has the following problems: firstly, the unified planning is lacked, the method is generally developed according to the machine type, and the standardization, serialization and universalization degrees are low; secondly, the device has the advantages of large quantity, large volume, lack of standardization and integration, poor maneuverability and deployment, and incapability of meeting the requirements of maneuvering operation of modern wars.
Disclosure of Invention
In order to solve the above technical problem, embodiments of the present application provide a method and a system for integrating a universal test platform.
In a first aspect, an embodiment of the present application provides a method for integrating a universal test platform, where the method includes:
acquiring a target test requirement;
selecting target universal test resources from the universal test resource set according to target test requirements;
selecting target specific test resources from the specific test resource set according to target test requirements;
and assembling the target general test resources and the target specific test resources through the interconnection and intercommunication connecting mechanism and the interconnection and intercommunication interface specification to obtain a target test platform, so that the target test platform realizes target test.
Optionally, before obtaining the target test requirement, the method further includes:
acquiring a general test demand set and a specific test demand set according to test demands of different airborne equipment;
acquiring a universal test resource set according to the universal test demand set;
acquiring a specific test resource set according to a specific test requirement set;
and determining the interconnection and interworking connection mechanism and the interconnection and interworking interface specification according to the general test resource set and the specific test resource set.
Optionally, obtaining a general test requirement set and a specific test requirement set according to test requirements of different onboard devices includes:
the method comprises the steps of carrying out statistical analysis on test signal requirements of different airborne equipment, obtaining a plurality of general test requirements by taking the same test signal requirements of different airborne equipment as general test requirements, and obtaining a plurality of specific test requirements by taking different test signal requirements of different airborne equipment as specific test requirements.
Optionally, obtaining the universal test resource set according to the universal test requirement set includes:
determining a first hardware resource and/or a first software resource required by each corresponding universal test signal requirement according to the universal test requirement set, and forming the first hardware resource and/or the first software resource required by each universal test signal into a corresponding universal test resource;
obtaining a set of specific test resources according to a set of specific test requirements, comprising:
and determining second hardware resources and/or second software resources required by each corresponding specific test signal requirement according to the specific test requirement set, and combining the second hardware resources and/or the second software resources required by each specific test signal into corresponding specific test resources.
Optionally, determining the interconnection and interworking connection mechanism and the interconnection and interworking interface specification according to the general test resource set and the specific test resource set includes:
and determining the interconnection connecting mechanism and the interconnection interface specification, so that the universal test resources and the specific test resources, the universal test resources and the specific test resources are combined through the same interconnection connecting mechanism and the same interconnection interface specification.
Optionally, the universal test resource set includes a plurality of different universal test resources, the specific test resource set includes a plurality of different specific test resources, each universal test resource can independently implement a universal test, and each specific test resource is combined with at least one universal test resource to implement a specific test.
Optionally, the interconnection and interconnection connection mechanism is configured to implement mechanical connection and electrical communication connection between the test resources, where the test resources include general test resources and specific test resources.
Optionally, the method further comprises:
acquiring an extended test requirement set according to test requirements of different airborne equipment;
and acquiring an extended test resource set according to the extended test requirement set.
Optionally, each test resource is of a combined chassis structure, and the test resources are assembled in a structure stacking manner through an interconnection connection structure and an interconnection interface specification.
In a second aspect, the present application provides a universal test platform integration system, which composes different test platforms according to any one of the methods described above to implement tests with different requirements.
Compared with the prior art, the technical scheme provided by the embodiment of the application has the following advantages:
the technical scheme provided by the embodiment of the application can meet the detection requirements of various different airborne devices, the test platform of each combination is appropriate in size, easy to splice, combine and deploy, quick to reconstruct, simple and easy to operate, and extensible and cuttable. The universalization, serialization and unification of the test resources are realized through the interconnection connecting mechanism and the interconnection interface specification, the maneuvering capability, the accompanying guarantee capability and the test efficiency of the automatic test system are improved, the cost of the test system is reduced, and the rapid and efficient detection and maintenance of the weapon equipment are realized. In addition, a certain redundant channel and an expandable space are reserved, so that the flexible and expandable test resources are realized, and the platform resource expansion requirement brought by future airborne equipment detection is met.
Because the traditional automatic test system is mostly professional equipment developed aiming at certain type equipment or specific test tasks, the function is single, the universality and the sustainability are lacked, and the maneuvering transition efficiency of the equipment is seriously influenced by the complicated cable disassembly and assembly among the system chassis. According to the technical scheme, the hierarchical characteristics of the structure and the function of the automatic test platform can be utilized, the universal hardware platform design of the airborne electronic equipment is carried out from two aspects of test resource allocation generalization and system architecture generalization through the analytical research on the detection requirements of the airborne equipment of different types and multiple specialties, a set of 'basic + professional' standard architecture tailorable extensible universal automatic test platform is established, and test systems with different professional configurations meet test tasks of airborne equipment of different specialties. The platform adopts the interconnection combination machine case, realizes the flexible interconnection of electrical signals among the platform machine cases through the interconnection connection mechanism, has no external connection cable, and synchronously completes the electrical connection when the structures are stacked, so that the system reconstruction is quick, simple and easy to operate, the maneuverability and the following guarantee capability of the test system are greatly improved, and meanwhile, the modular design is carried out on the interconnection interface, so that the platform can realize quick expansion or reduction in a modular mode. The invention has important research significance for the fields of development of test maintenance guarantee and the like of electronic equipment such as radars, airplanes and the like, and has better economic benefit and military benefit.
Drawings
The accompanying drawings, which are incorporated in and constitute a part of this specification, illustrate embodiments consistent with the invention and together with the description, serve to explain the principles of the invention.
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, and it is obvious for those skilled in the art that other drawings can be obtained according to the drawings without inventive exercise.
FIG. 1 is a flowchart illustrating a general test platform integration method according to an embodiment;
FIG. 2 is a flowchart illustrating a general test platform integration method according to another embodiment;
FIG. 3 is a diagram illustrating a combination of generic test resources and specific test resources, according to an embodiment;
FIG. 4 is a block diagram of a test resource interconnect, according to an embodiment.
Detailed Description
In order to make the objects, technical solutions and advantages of the embodiments of the present application clearer, the technical solutions in the embodiments of the present application will be clearly and completely described below with reference to the drawings in the embodiments of the present application, and it is obvious that the described embodiments are some embodiments of the present application, but not all embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present application.
Fig. 1 is a flowchart illustrating a general test platform integration method according to an embodiment. Referring to fig. 1, the universal test platform integration method includes the following steps:
s100: and acquiring target test requirements.
Particularly, in the field of comprehensive test and diagnosis of aviation equipment, test maintenance guarantee of airborne equipment such as radars and airplanes has important research significance. The existing airborne equipment has multiple types, cross-machine types and multiple specialties, so that before a test platform aiming at test requirements corresponding to different airborne equipment is developed, corresponding target test requirements need to be obtained according to analysis and statistics.
S200: and selecting the target universal test resource from the universal test resource set according to the target test requirement.
Specifically, the universal test resource set includes at least one universal test resource, and the universal test resource may include a main control unit, an ac/dc power supply unit, a basic test unit, and the like. The universal test resources can be used as a universal module to be combined with other specific test resources to achieve a specific test purpose, and can also be used as an independent test module (namely a test platform) to achieve the same test purpose of different airborne equipment. According to the target test requirement, the required test resources can be known, so that the target universal test resources can be selected from the existing universal test resource set.
S300: and selecting target specific test resources from the specific test resource set according to the target test requirements.
In particular, the specific test resource is a test resource required to be used by the specific test requirement of one or more onboard devices.
S400: and assembling the target general test resources and the target specific test resources through the interconnection and intercommunication connecting mechanism and the interconnection and intercommunication interface specification to obtain a target test platform, so that the target test platform realizes target test.
Specifically, the target general test resource and the target specific test resource need to be assembled through the interconnection connection mechanism and the interconnection interface specification to form a complete target test platform, and the target test platform completes the target test through mutual cooperation of the general test resource and the specific test resource.
Fig. 2 is a schematic flowchart of a general test platform integration method according to another embodiment. Referring to fig. 2, before step S100, the method further includes the steps of:
s010: and acquiring a general test requirement set and a specific test requirement set according to the test requirements of different airborne equipment.
Specifically, in order to meet the detection requirements of the cross-model and multi-professional airborne equipment, a large amount of statistical analysis needs to be carried out on the test signal requirements of each model and each professional airborne equipment, and from the range of the model, the professional span of the tested airborne equipment and the test depth of each airborne equipment, the sufficient sample number can more comprehensively cover the design of various different test requirements of the airborne equipment.
Different onboard equipment, some of which have the same test requirements, namely as universal test requirements; some on-board devices have their own independent test requirements, i.e., as specific test requirements. Of course, the specific test requirement may also be a specific test requirement common to multiple onboard devices.
S020: and acquiring a universal test resource set according to the universal test demand set.
S030: and acquiring a specific test resource set according to the specific test requirement set.
Specifically, implementation of a general test requirement requires certain general test resources, and implementation of a specific test requirement also requires certain specific test resources. The test resources may include hardware resources and may also include software code resources. Support of hardware resources and/or software code resources is required regardless of whether generic or specific test requirements are implemented.
S040: and determining the interconnection and interworking connection mechanism and the interconnection and interworking interface specification according to the general test resource set and the specific test resource set.
In particular, the generalization of test resources and the modularization of a test system are realized. Based on a general test platform with a basic and professional architecture, a general interface bus can adopt an LAN bus as a resource control bus, and signals such as control, power supply and the like are defined on an interconnection interface according to a bus form. And the interconnection and intercommunication connecting mechanism can realize flexible interconnection and intercommunication among the test resources, thereby realizing good compatibility.
In one embodiment, step S010 specifically includes: the method comprises the steps of carrying out statistical analysis on test signal requirements of different airborne equipment, obtaining a plurality of general test requirements by taking the same test signal requirements of different airborne equipment as general test requirements, and obtaining a plurality of specific test requirements by taking different test signal requirements of different airborne equipment as specific test requirements.
In one embodiment, step S020 specifically includes: and determining the first hardware resource and/or the first software resource required by each corresponding universal test signal requirement according to the universal test requirement set, and combining the first hardware resource and/or the first software resource required by each universal test signal into the corresponding universal test resource.
In one embodiment, step S030 specifically includes: and determining second hardware resources and/or second software resources required by each corresponding specific test signal requirement according to the specific test requirement set, and combining the second hardware resources and/or the second software resources required by each specific test signal into corresponding specific test resources.
Specifically, to complete the acquisition or detection of a certain test signal, a corresponding hardware resource and/or software resource needs to be configured, and then the corresponding hardware resource and/or software resource performs the acquisition or detection of the corresponding test signal.
In one embodiment, step S040 specifically includes: and determining the interconnection connecting mechanism and the interconnection interface specification, so that the universal test resources and the specific test resources, the universal test resources and the specific test resources are combined through the same interconnection connecting mechanism and the same interconnection interface specification.
Specifically, after the connection mechanism and the interface specification are unified, all the test resources can be interconnected and intercommunicated, and the universalization is really realized.
In one embodiment, the set of generic test resources includes a plurality of different generic test resources, the set of specific test resources includes a plurality of different specific test resources, each generic test resource is independently operable to perform a generic test, and each specific test resource is operable in combination with at least one generic test resource to perform a specific test.
In particular, the generic test resources may be used independently, and a particular test resource needs to be combined with at least one generic test resource to achieve a target test.
In one embodiment, the interconnection and interconnection mechanism is used for realizing mechanical connection and electrical communication connection between test resources, wherein the test resources comprise general test resources and specific test resources.
Specifically, the test platform adopts a flexible interconnection connection mechanism and a uniform interconnection interface specification to realize the modular design of interconnection. The flexible interconnection of electrical signals among the test resources is realized through the flexible interconnection and intercommunication connecting mechanism, the electrical connection is synchronously completed, the interconnection and intercommunication interface is subjected to modular design, signals such as control, power supply and the like are defined on the interconnection and intercommunication interface according to a bus form, and the test resources can be expanded or reduced in a modular mode.
In one embodiment, the method further comprises:
acquiring an extended test requirement set according to test requirements of different airborne equipment;
and acquiring an extended test resource set according to the extended test requirement set.
Specifically, the test requirements of airborne equipment of various types are comprehensively considered, the test resources of the comprehensive automatic test system are configured, and certain redundant channels, expandable space and expandable capacity are reserved to realize the generalization and the expandability of the test resources.
In one embodiment, each test resource is a combined chassis structure, and the test resources are assembled in a structure stacking mode through an interconnection connection structure and an interconnection interface specification.
Specifically, hardware resources and software resources of each test resource are integrated in a combined chassis, and when combination is needed among the test resources, mechanical connection, electrical interconnection and intercommunication and communication among signals are facilitated. Preferably, the interconnection connection structure does not largely use long cable connection, and is convenient to combine.
FIG. 3 is a diagram illustrating a combination of generic test resources and specific test resources, according to an embodiment. Referring to fig. 3, a target generic test resource 10 and a target specific test resource 20 are combined to obtain a target test platform. The target generic test resource 10 is composed of 4 combined chassis, and the target specific test resource 20 is composed of 1 combined chassis.
The test platform adopts an open architecture, hardware can be cut and reconstructed, and integration according to professional division is supported. The maximum configuration of the platform is comprehensive, the platform can cover all professional tested object testing functions, the minimum configuration is basic, and universal testing resources, a switching system and a testing adaptive interface required by the tested object testing requirements are provided. The test platform can be flexibly expanded on the basis of basic models according to the specialties of avionics, aviation special equipment, aviation ordnance and the like. Certain physical space, logic space, bus drive, power supply load and other expansion capabilities are reserved for specific test resources. The basic test platform consists of 4 combined cases which are stacked in a scale of 2 (rows) multiplied by 2 (columns); the specific test platform consists of 4 basic combined boxes and 1 combined box of the specific test resource, and 5 combined boxes are stacked on the scale of 2 (rows) × 2 (columns) + 1.
FIG. 4 is a block diagram of a test resource interconnect, according to an embodiment. Referring to fig. 4, the target generic test resource 10 and the target specific test resource 20 of fig. 3 are combined into a target test platform in a stacked form through an interworking connection mechanism and an interworking interface specification.
Of course, the target generic test resource 10 may also be combined with other specific test resources into a new test platform; the target specific test resources 20 may also be combined with other general purpose test resources into a new test platform.
Signals such as control and power supply are defined on the interconnection interface, so that the chassis can be expanded or reduced in a modular mode.
In one embodiment, the general test resources generally adopt a networking topology architecture to exchange data, and adopt an instrumentation bus which takes a new generation high-speed test bus PXIe as a core and is compatible with a PXI bus to realize a hardware architecture of a basic system; the hardware architecture of the expansion system is realized by adopting a PXIe/PXI/LXI bus expansion mode. The universal test resources may include basic signal sources, basic measurement instruments, power supplies, electronic loads, digital communication resources, switching systems, and the like. The extended professional resources comprise radio frequency testing instruments, microwave testing instruments, atmospheric testing resources and the like. Under a standard bus system and a networked switching architecture, the hardware of the universal automatic test platform can be conveniently cut, expanded and upgraded.
In one embodiment, the test platform employs a quick-disconnect composite interconnect. The structure types of the combined structure interconnection device are divided into a cross shape and a T shape, and the cross shape and the T shape are respectively used for connecting four combined machine cases and connecting two combined machine cases. The combined structure interconnector is a structure fastening device used for interconnecting the combined chassis and the combined base into a whole. The combined structure interconnection device can effectively prevent displacement between combined system combined cases and between the combined cases and the combined base, and ensure the reliability of electrical interconnection and the mechanical stability of hardware resource combination.
In one embodiment, the flexible electrical connection between the interconnected combined chassis is divided into two butt joints: the operation of directly pushing and pulling by hands in one butting stroke does not need special tools; the secondary butt joint stroke is realized by a rotating handle mechanism of the interconnection and intercommunication connecting mechanism. Due to the adoption of the flexible structure design, the connection of cables can be synchronously completed in the process of disassembling and reconstructing the case, the complex cable disassembly and assembly of the traditional test platform are avoided, the butt joint process is quick, smooth and reliable, and the speed and the precision of combined butt joint are improved.
On the basis of the design of a universal test platform based on a basic and professional framework, the platform adopts an interconnection modular design, and flexible interconnection of electric signals is completed among all combined chassis units of the platform through a flexible interconnection connecting mechanism, so that the rapid combination and reconfiguration of the system are realized. A general automatic test platform network control configuration is established by a tree network topological structure, the design of a control cable in an interconnection case is fully considered, the control of test resources of all combined cases of the subsystems can be met, the control problem of the test resources after the system is reconstructed can be solved, and the maneuvering capacity, the accompanying guarantee capacity and the test efficiency of the automatic test system are improved.
The universal automatic testing platform based on electrical flexible interconnection is constructed based on 'foundation + specialty' aiming at the problems of low standardization, serialization and universalization degrees, large quantity, large volume, lack of integration, poor maneuverability, poor deployment and the like of the existing automatic testing system, so that the maneuverability, the accompanying guarantee capability and the testing efficiency of the automatic testing system are improved, the cost of the testing system is reduced, and the rapid and efficient detection and maintenance of weaponry are realized.
According to the method, according to the detection requirements of cross-machine type and multi-professional airborne equipment, test resource allocation universalization and system architecture universalization are used as design targets, a set of tailorable extensible universal automatic test platform with a basic + professional standard architecture is constructed through equipment test requirement statistical analysis, universalization hardware platform design and modularized design of interconnection and intercommunication, and the test requirements of different professional airborne equipment can be met; the method is based on electrical flexible interconnection and intercommunication, adopts the interconnection combined case, realizes the electrical signal flexible interconnection between the platform cases through the combined structure interconnector and the flexible interconnection and intercommunication connecting device, synchronously completes electrical connection while stacking the structure, ensures that the system is convenient and rapid to reconstruct, greatly reduces the requirement on case assembly precision, enhances operability, and improves the reliability of electrical flexible interconnection and intercommunication due to the application of the connector self-locking function. The universal automatic test platform integration method based on electric flexible interconnection and intercommunication enables the disassembly and assembly efficiency of the system to be improved, and can meet the requirements of quick and flexible tasks.
It is noted that, in this document, relational terms such as "first" and "second," and the like, may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus. Without further limitation, an element defined by the phrase "comprising an … …" does not exclude the presence of other identical elements in a process, method, article, or apparatus that comprises the element.
The foregoing are merely exemplary embodiments of the present invention, which enable those skilled in the art to understand or practice the present invention. Various modifications to these embodiments will be readily apparent to those skilled in the art, and the generic principles defined herein may be applied to other embodiments without departing from the spirit or scope of the invention. Thus, the present invention is not intended to be limited to the embodiments shown herein but is to be accorded the widest scope consistent with the principles and novel features disclosed herein.
Claims (10)
1. A method for integrating a universal test platform, the method comprising:
acquiring a target test requirement;
selecting target universal test resources from a universal test resource set according to the target test requirements;
selecting a target specific test resource from a specific test resource set according to the target test requirement;
and assembling the target general test resource and the target specific test resource through an interconnection connecting mechanism and an interconnection interface specification to obtain a target test platform, so that the target test platform realizes target test.
2. The method of claim 1, wherein prior to said obtaining a target test requirement, the method further comprises:
acquiring a general test demand set and a specific test demand set according to test demands of different airborne equipment;
acquiring a universal test resource set according to the universal test demand set;
acquiring a specific test resource set according to the specific test requirement set;
and determining the specification of the interconnection and interworking connection mechanism and the interconnection and interworking interface according to the general test resource set and the specific test resource set.
3. The method of claim 2, wherein the obtaining a set of generic test requirements and a set of specific test requirements based on test requirements of different onboard devices comprises:
the method comprises the steps of carrying out statistical analysis on test signal requirements of different airborne equipment, obtaining a plurality of general test requirements by taking the same test signal requirements of different airborne equipment as general test requirements, and obtaining a plurality of specific test requirements by taking different test signal requirements of different airborne equipment as specific test requirements.
4. The method of claim 3, wherein obtaining a set of generic test resources from the set of generic test requirements comprises:
determining a first hardware resource and/or a first software resource required by each corresponding universal test signal requirement according to the universal test requirement set, and forming the first hardware resource and/or the first software resource required by each universal test signal into a corresponding universal test resource;
the obtaining a specific test resource set according to the specific test requirement set includes:
and determining second hardware resources and/or second software resources required by each corresponding specific test signal requirement according to the specific test requirement set, and combining the second hardware resources and/or the second software resources required by each specific test signal into corresponding specific test resources.
5. The method of claim 4, wherein determining the interworking connection mechanism and the interworking interface specification from the generic set of test resources and the specific set of test resources comprises:
and determining the interconnection connecting mechanism and the interconnection interface specification, so that the universal test resources and the specific test resources, the universal test resources and the specific test resources are combined through the same interconnection connecting mechanism and the same interconnection interface specification.
6. The method of claim 5, wherein the set of generic test resources comprises a plurality of different generic test resources, wherein the set of specific test resources comprises a plurality of different specific test resources, wherein each of the generic test resources is capable of independently performing a generic test, and wherein each of the specific test resources is combined with at least one of the generic test resources to perform a specific test.
7. The method of claim 6, wherein the interconnection and interconnection mechanism is configured to implement a mechanical connection and an electrical communication connection between test resources, wherein the test resources comprise general test resources and specific test resources.
8. The method of claim 2, further comprising:
acquiring an extended test requirement set according to test requirements of different airborne equipment;
and acquiring an extended test resource set according to the extended test requirement set.
9. The method of claim 7, wherein each of the test resources is a combined chassis structure, and the test resources are assembled in a structure stacking manner through the interworking connection structure and the interworking interface specification.
10. A universal test platform integration system, characterized in that the system composes different test platforms according to the method of any of claims 1-9 to achieve tests of different requirements.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010003195.0A CN111071481B (en) | 2020-01-02 | 2020-01-02 | Universal test platform integration method and system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010003195.0A CN111071481B (en) | 2020-01-02 | 2020-01-02 | Universal test platform integration method and system |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN111071481A true CN111071481A (en) | 2020-04-28 |
| CN111071481B CN111071481B (en) | 2021-06-01 |
Family
ID=70321749
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202010003195.0A Active CN111071481B (en) | 2020-01-02 | 2020-01-02 | Universal test platform integration method and system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN111071481B (en) |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103558043A (en) * | 2013-11-04 | 2014-02-05 | 北京航天测控技术有限公司 | Test diagnosis method and device |
| CN103693211A (en) * | 2013-12-25 | 2014-04-02 | 北京航天测控技术有限公司 | Test method for helicopter rotating part signal and wireless collecting device therefor |
| CN104181908A (en) * | 2013-05-22 | 2014-12-03 | 中国国际航空股份有限公司 | DFDAU test platform and test method |
| CN104184525A (en) * | 2013-05-22 | 2014-12-03 | 中国国际航空股份有限公司 | Digital-flight-data-acquisition-unit-based test platform and test method of signal transmission device |
| CN105956981A (en) * | 2016-05-06 | 2016-09-21 | 西安工业大学 | Disaster information cloud computing system and disaster information cloud computing method |
| CN106628250A (en) * | 2017-02-14 | 2017-05-10 | 上海子锦电子科技有限公司 | Function-modularization comprehensive automatic detecting system for JL9 airplane |
| US20180067501A1 (en) * | 2016-09-07 | 2018-03-08 | The Boeing Company | Programmable multi-gravity test platform and method for using same |
| CN109542794A (en) * | 2018-12-04 | 2019-03-29 | 中国航空工业集团公司西安航空计算技术研究所 | A kind of Software Automatic Testing Method applied to embedded system |
| CN110606223A (en) * | 2019-10-08 | 2019-12-24 | 北京交通大学 | Coaxial dual-rotor unmanned aerial vehicle ground flight test platform and test method |
-
2020
- 2020-01-02 CN CN202010003195.0A patent/CN111071481B/en active Active
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104181908A (en) * | 2013-05-22 | 2014-12-03 | 中国国际航空股份有限公司 | DFDAU test platform and test method |
| CN104184525A (en) * | 2013-05-22 | 2014-12-03 | 中国国际航空股份有限公司 | Digital-flight-data-acquisition-unit-based test platform and test method of signal transmission device |
| CN103558043A (en) * | 2013-11-04 | 2014-02-05 | 北京航天测控技术有限公司 | Test diagnosis method and device |
| CN103693211A (en) * | 2013-12-25 | 2014-04-02 | 北京航天测控技术有限公司 | Test method for helicopter rotating part signal and wireless collecting device therefor |
| CN105956981A (en) * | 2016-05-06 | 2016-09-21 | 西安工业大学 | Disaster information cloud computing system and disaster information cloud computing method |
| US20180067501A1 (en) * | 2016-09-07 | 2018-03-08 | The Boeing Company | Programmable multi-gravity test platform and method for using same |
| CN106628250A (en) * | 2017-02-14 | 2017-05-10 | 上海子锦电子科技有限公司 | Function-modularization comprehensive automatic detecting system for JL9 airplane |
| CN109542794A (en) * | 2018-12-04 | 2019-03-29 | 中国航空工业集团公司西安航空计算技术研究所 | A kind of Software Automatic Testing Method applied to embedded system |
| CN110606223A (en) * | 2019-10-08 | 2019-12-24 | 北京交通大学 | Coaxial dual-rotor unmanned aerial vehicle ground flight test platform and test method |
Non-Patent Citations (1)
| Title |
|---|
| 文永明，余锋祥: "航空设备通用自动测试平台研究", 《计算机测量与控制》 * |
Also Published As
| Publication number | Publication date |
|---|---|
| CN111071481B (en) | 2021-06-01 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN105786620A (en) | Integrated reconfigurable summarized information processing loading system | |
| CN109270366A (en) | A kind of test method of short cycle batch productionization satellite | |
| CN103677815B (en) | A kind of spacecraft low-frequency cable electrical property autotest program generates method | |
| CN102692572A (en) | Airplane radiofrequency device electromagnetic compatibility analysis method based on time availability | |
| CN111071481B (en) | Universal test platform integration method and system | |
| CN104316814A (en) | Aircraft cable plugging connection state automatic detection system | |
| CN104484257B (en) | A kind of general 1553B bus communication emulation test system and method | |
| CN113495842A (en) | Automatic test system and test method for mass production of satellites | |
| CN215769426U (en) | Multi-bus intelligent test and launch control device | |
| CN114374451A (en) | Large-scale MIMO channel simulation method and device based on optical matrix switching | |
| CN109992457B (en) | Testing system of hierarchical configurable microsatellite | |
| CN114422455A (en) | Multi-dimensional resource management architecture and method based on air-space-ground integrated network | |
| RU2669330C1 (en) | Integrated automated system of cosmodrome | |
| CN108199759B (en) | Satellite onboard electronic system with multiple cabin sections | |
| CN112988629A (en) | Data recording device and method, storage medium | |
| CN112304653A (en) | Universal comprehensive test method and system for satellite test | |
| CN114671049B (en) | Dynamic reconfigurable aircraft cabin entertainment system integration test method and device | |
| CN112193436B (en) | Integrated verification test environment system for civil passenger plane cabin system | |
| CN217034539U (en) | Survey launch and control system suitable for polytypic carrier rocket | |
| Gao et al. | Intelligent electronic information equipment maintenance and testing system based on general test instruments | |
| CN214201727U (en) | Aviation complete machine cable detection system | |
| CN214409249U (en) | General type cable tester | |
| Wen et al. | Research on the design of Reconfigurable Universal Automatic Test System | |
| US20230208718A1 (en) | Network topology planning and validation | |
| CN114048545A (en) | Military aircraft-oriented lightweight test process modeling method |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |