CN1968058A - Airborne communication navigation testing station - Google Patents
Airborne communication navigation testing station Download PDFInfo
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- CN1968058A CN1968058A CNA2006101246184A CN200610124618A CN1968058A CN 1968058 A CN1968058 A CN 1968058A CN A2006101246184 A CNA2006101246184 A CN A2006101246184A CN 200610124618 A CN200610124618 A CN 200610124618A CN 1968058 A CN1968058 A CN 1968058A
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Abstract
The invention relates to a carrier communication navigate testing station, which comprises testing system controller, program-control tester, program-control aviation signal source, and program-control Taconic simulator, wherein the testing system controller is connected to program-control tester, program-control aviation signal source, and program-control Taconic simulator; the program-control tester is connected to tested communicator; the program-control aeration signal source is connected to tested navigate product. The invention has the advantages that: (1), it can be used in plane research, to apply third-generation level; (2), it can operate in several operation systems, with better compatibility; (3), it can apply the tests of several products.
Description
Technical field
The present invention relates to a kind of airborne communication navigation testing station.
Background technology
4 stages have roughly been experienced in the development of tester technology, be in for the 4th stage at present, be so-called virtual instrument (Virtual Instrument), it is the new type that computer technology is applied to technical device, it is with the all-purpose computer of having expanded the distinct interface integrated circuit board hardware platform as tester, by calling different TT﹠C softwares, thereby realize different observing and controlling functions.Software become guarantee test macro quick and precisely, the core of characteristic such as reliable and stable, complete function, friendly interface, upgrading be flexible.The software development environment of virtual instrument adopts the visual programming language more and more, and typical technology has: the AgilentVEE of the Labview of American National instrument company, U.S. Agilent Technologies.Labview has integrated the repertoire of hardware communications such as satisfying GPIB, VXI, PXI, RS-232, RS-485 and data collecting card, the also built-in built-in function of being convenient to use software standards such as TCP/IP, ActiveX, not only can under several operation systems, move, and can under different operating system, keep compatible.In aviation electronics product test field, product category to be measured is many, parameter is numerous and diverse, with respect to combining multiple instrumental function, having disposed for the desk-top radio frequency/audio equipment of gpib interface, cassette such as VXI, PXI technical device also can't satisfy whole requirements, is applicable to that the general TT﹠C software that the multiple product test needs does not also go out.
Summary of the invention
The purpose of this invention is to provide a kind of airborne communication navigation testing station, it is with the desk-top radio frequency/audio equipment of GPIB card control, finishes the isoparametric observing and controlling of bus signals, switching signal, analog signal to product to be measured by adapter and grammed switch.
The present invention is achieved like this, it comprises testing system controller, program-control tester, program-control aviation signal source, program-control Taconic simulator, testing system controller connects program-control tester, program-control aviation signal source, program-control Taconic simulator respectively, program-control tester connects communication products to be measured, program-control aviation signal source connects navigation product to be measured, it is characterized in that operating procedure is as follows:
(1) selects test function, enter the corresponding operating interface;
(2) carry out every functional test, comprise control box transducer electric performance test, integrated navigation control box electric performance test, Tacan transceiver electric performance test, course downslide receiver electric performance test, beacon receiver electric performance test, radio-compass receiver electric performance test, interphone electric performance test, ultrashort wave radio set electric performance test;
(3) confirm whether continue test, be then to turn back to initial state, otherwise the model and the piece number of input product;
(4) test data is outputed to word document and form test report;
(5) preservation and printing test report on request.
Advantage of the present invention is: (1) serves the development of new aircraft, and the third generation technical merit (synthesization, digitlization, intellectuality) that is had with new aircraft adapts; (2) not only can under several operation systems, move, and can under different operating system, keep compatible; (3) be applicable to the test of multiple product.
Description of drawings
Fig. 1 is working envelope figure of the present invention;
Fig. 2 is an operating procedure flow chart of the present invention;
Embodiment
As Fig. 1, shown in, the present invention includes testing system controller 5, program-control tester 9, program-control aviation signal source 2, program-control Taconic simulator 6, testing system controller 5 connects program-control tester 9, program-control aviation signal source 2, program-control Taconic simulator 6 and printer 4 respectively, program-control tester 9 connects communication products 11 to be measured, program-control aviation signal source 2 connects navigation product 1 to be measured and navigation product adapter 3, D.C. regulated power supply 7 connects navigation product adapter 3 and communication products adapter 10, and single-phase intermediate frequency power supply 8 connects navigation product adapter 3.
As shown in Figure 1, operating procedure of the present invention is as follows:
(1) selects test function, enter the corresponding operating interface;
(2) carry out every functional test, comprise control box transducer electric performance test, integrated navigation control box electric performance test, Tacan transceiver electric performance test, course downslide receiver electric performance test, beacon receiver electric performance test, radio-compass receiver electric performance test, interphone electric performance test, ultrashort wave radio set electric performance test;
(3) confirm whether continue test, if then turn back to initial state, if otherwise the model and the piece number of input product;
(4) test data is outputed to word document and form test report;
(5) preservation and printing test report on request.
Claims (1)
1, a kind of airborne communication navigation testing station, it comprises testing system controller, program-control tester, program-control aviation signal source, program-control Taconic simulator, testing system controller connects program-control tester, program-control aviation signal source, program-control Taconic simulator respectively, program-control tester connects communication products to be measured, program-control aviation signal source connects navigation product to be measured, it is characterized in that operating procedure is as follows:
(1) selects test function, enter the corresponding operating interface;
(2) carry out every functional test, comprise control box transducer electric performance test, integrated navigation control box electric performance test, Tacan transceiver electric performance test, course downslide receiver electric performance test, beacon receiver electric performance test, radio-compass receiver electric performance test, interphone electric performance test, ultrashort wave radio set electric performance test;
(3) confirm whether continue test, be then to turn back to initial state, otherwise the model and the piece number of input product;
(4) test data is outputed to word document and form test report;
(5) preservation and printing test report on request.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNA2006101246184A CN1968058A (en) | 2006-09-23 | 2006-09-23 | Airborne communication navigation testing station |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNA2006101246184A CN1968058A (en) | 2006-09-23 | 2006-09-23 | Airborne communication navigation testing station |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN1968058A true CN1968058A (en) | 2007-05-23 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNA2006101246184A Pending CN1968058A (en) | 2006-09-23 | 2006-09-23 | Airborne communication navigation testing station |
Country Status (1)
| Country | Link |
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| CN (1) | CN1968058A (en) |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102035612A (en) * | 2009-10-01 | 2011-04-27 | 罗伯特·博世有限公司 | Mobile computer device using a modulated aural signal and method for transmitting information in aid of the modulated aural signal |
| CN103900616A (en) * | 2014-04-16 | 2014-07-02 | 中国人民解放军空军航空仪器设备计量总站 | Tacan simulator metering method and Tacan simulator metering device |
| CN104515515A (en) * | 2013-09-30 | 2015-04-15 | 哈尔滨飞机工业集团有限责任公司 | Radio compass tester |
| CN105024766A (en) * | 2014-04-21 | 2015-11-04 | 哈尔滨飞机工业集团有限责任公司 | Communication control management equipment tester |
| CN105824249A (en) * | 2016-05-13 | 2016-08-03 | 中国航空工业集团公司西安飞机设计研究所 | Testing method and testing system for aircraft parameter display results |
| CN107592307A (en) * | 2017-09-11 | 2018-01-16 | 中国航空工业集团公司西安飞机设计研究所 | A kind of airborne audio management system voice transfer verification method |
| CN108387237A (en) * | 2018-03-20 | 2018-08-10 | 陈昌志 | General Aviation radar number passes ip radio station networking navigation system |
| CN112557799A (en) * | 2020-12-12 | 2021-03-26 | 江西洪都航空工业集团有限责任公司 | Comprehensive CNI system testing device |
-
2006
- 2006-09-23 CN CNA2006101246184A patent/CN1968058A/en active Pending
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102035612A (en) * | 2009-10-01 | 2011-04-27 | 罗伯特·博世有限公司 | Mobile computer device using a modulated aural signal and method for transmitting information in aid of the modulated aural signal |
| CN104515515A (en) * | 2013-09-30 | 2015-04-15 | 哈尔滨飞机工业集团有限责任公司 | Radio compass tester |
| CN103900616A (en) * | 2014-04-16 | 2014-07-02 | 中国人民解放军空军航空仪器设备计量总站 | Tacan simulator metering method and Tacan simulator metering device |
| CN103900616B (en) * | 2014-04-16 | 2017-12-29 | 中国人民解放军空军航空仪器设备计量总站 | A kind of Tacan simulator metering method and device |
| CN105024766A (en) * | 2014-04-21 | 2015-11-04 | 哈尔滨飞机工业集团有限责任公司 | Communication control management equipment tester |
| CN105024766B (en) * | 2014-04-21 | 2018-11-16 | 哈尔滨飞机工业集团有限责任公司 | Communication control management equipment test device |
| CN105824249A (en) * | 2016-05-13 | 2016-08-03 | 中国航空工业集团公司西安飞机设计研究所 | Testing method and testing system for aircraft parameter display results |
| CN107592307A (en) * | 2017-09-11 | 2018-01-16 | 中国航空工业集团公司西安飞机设计研究所 | A kind of airborne audio management system voice transfer verification method |
| CN108387237A (en) * | 2018-03-20 | 2018-08-10 | 陈昌志 | General Aviation radar number passes ip radio station networking navigation system |
| CN112557799A (en) * | 2020-12-12 | 2021-03-26 | 江西洪都航空工业集团有限责任公司 | Comprehensive CNI system testing device |
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| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Open date: 20070523 |