CN105372530A - Single test debugging system with real-time simulation test capability - Google Patents

Single test debugging system with real-time simulation test capability Download PDF

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Publication number
CN105372530A
CN105372530A CN201510828733.9A CN201510828733A CN105372530A CN 105372530 A CN105372530 A CN 105372530A CN 201510828733 A CN201510828733 A CN 201510828733A CN 105372530 A CN105372530 A CN 105372530A
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China
Prior art keywords
switch
testing device
real
test
signal
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CN201510828733.9A
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Chinese (zh)
Inventor
孙海力
邹德儒
孙翔宇
常双利
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Shenyang Aircraft Design and Research Institute Aviation Industry of China AVIC
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Shenyang Aircraft Design and Research Institute Aviation Industry of China AVIC
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Priority to CN201510828733.9A priority Critical patent/CN105372530A/en
Publication of CN105372530A publication Critical patent/CN105372530A/en
Pending legal-status Critical Current

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Abstract

The invention discloses a single test debugging system with real-time simulation test capability. The single test debugging system with real-time simulation test capability comprises a test control computer; a switch which is connected with the test control computer; a discrete quantity simulation test device which is connected with the switch; an analog quantity simulation test device which is connected with the switch; a bus simulation test device which is connected with the switch; clock synchronization equipment which is connected with the switch; and a transfer conditioning case which is respectively connected with the discrete quantity simulation test device, the analog quantity simulation test device, the bus simulation test device and an avionic device to be tested. The single test debugging system with real-time simulation test capability can realize the following advantages that the single test debugging system has comprehensive real-time simulation test capability of discrete quantity, analog quantity and bus and multiple types of signals; and connection of tested equipment of different interfaces can be conveniently realized by the transfer conditioning case.

Description

A kind of list inspection debug system with real-time simulation power of test
Technical field
The present invention relates to aircraft technology field, be specifically related to a kind of list inspection debug system with real-time simulation power of test.
Background technology
The list inspection debug system of Aerial Electronic Equipment is in the past all test respectively to various interface, and various interface works often in truly using simultaneously, so just be difficult to realize the real-time testing to various interface synchronization, test is made to be difficult to cover real use procedure, cause test comprehensive, increase later stage change cost.
Therefore, wish a kind of technical scheme to overcome or at least alleviate at least one the problems referred to above of prior art.
Summary of the invention
A kind of list inspection debug system with real-time simulation power of test is the object of the present invention is to provide to overcome or at least alleviate at least one the problems referred to above of the prior art.
For achieving the above object, the invention provides a kind of list inspection debug system with real-time simulation power of test, described in there is real-time simulation power of test list inspection debug system comprise: testing and control computing machine; Switch, described switch is connected with described testing and control computing machine; Discrete magnitude simulation testing device, described discrete magnitude simulation testing device is connected with described switch; Analog quantity simulation testing device, described analog quantity simulation testing device is connected with described switch; Bus simulator proving installation, described Bus simulator proving installation is connected with described switch; Clock synchronization device, described clock synchronization device is connected with switch; Switching conditioning case, described switching conditioning case is connected with described discrete magnitude simulation testing device, analog quantity simulation testing device, Bus simulator proving installation and avionics device to be measured respectively; Wherein, described testing and control computing machine and described switch are used for mutual transmission of signal; Described switch is used for the control signal that described testing and control computing machine transmits being passed to described discrete magnitude simulation testing device, analog quantity simulation testing device and/or Bus simulator proving installation and the feedback signal of described discrete magnitude simulation testing device, analog quantity simulation testing device and/or Bus simulator proving installation being passed to described testing and control computing machine; Described discrete magnitude simulation testing device, analog quantity simulation testing device and Bus simulator proving installation are used for the control signal according to described testing and control computing machine, and are transmitted or collecting work signal to described avionics device to be measured by described switching conditioning case; Described clock synchronization device is used for the working signal that synchronous described discrete magnitude simulation testing device, analog quantity simulation testing device and Bus simulator proving installation transmit or gather.
Preferably, described switching conditioning case is connected with switch further, described testing and control computing machine is used for debug signal to pass to described switch, and by switch, debug signal is passed to switching conditioning case, thus by switching conditioning case, debug signal is passed to avionics device to be measured.
Preferably, the described list inspection debug system with real-time simulation power of test comprises serial server further, described serial server is respectively with switch and transfer and nurse one's health case and be connected, the debug signal passing to switch that described serial server is used for being sent by testing and control computing machine passes to described switching conditioning case, thus by switching conditioning case, debug signal is passed to avionics device to be measured.
Preferably, described switch is Ethernet switch.
The list inspection debug system with real-time simulation power of test of the present invention can to single check system of various interface synchronization real-time simulation test, meanwhile, this list inspection debug system with real-time simulation power of test can realize following advantage: 1) possess the comprehensive real-time simulation power of test to many types of signals such as discrete magnitude, analog quantity, buses; 2) the on-line debugging ability of network interface to equipment under test and RS232 serial ports is possessed; 3) by switching conditioning case, the connection to distinct interface equipment under test can conveniently be realized.
Accompanying drawing explanation
Fig. 1 is the schematic annexation figure with the list inspection debug system of real-time simulation power of test according to a first embodiment of the present invention.
Reference numeral:
1 Testing and control computing machine 5 Bus simulator proving installation
2 Switch 6 Clock synchronization device
3 Discrete magnitude simulation testing device 7 Switching conditioning case
4 Analog quantity simulation testing device 8 Avionics device to be measured
Embodiment
For making object of the invention process, technical scheme and advantage clearly, below in conjunction with the accompanying drawing in the embodiment of the present invention, the technical scheme in the embodiment of the present invention is further described in more detail.In the accompanying drawings, same or similar label represents same or similar element or has element that is identical or similar functions from start to finish.Described embodiment is the present invention's part embodiment, instead of whole embodiments.Be exemplary below by the embodiment be described with reference to the drawings, be intended to for explaining the present invention, and can not limitation of the present invention be interpreted as.Based on the embodiment in the present invention, those of ordinary skill in the art, not making the every other embodiment obtained under creative work prerequisite, belong to the scope of protection of the invention.Below in conjunction with accompanying drawing, embodiments of the invention are described in detail.
In describing the invention; it will be appreciated that; term " " center ", " longitudinal direction ", " transverse direction ", "front", "rear", "left", "right", " vertically ", " level ", " top ", " end " " interior ", " outward " etc. instruction orientation or position relationship be based on orientation shown in the drawings or position relationship; be only the present invention for convenience of description and simplified characterization; instead of instruction or imply indication device or element must have specific orientation, with specific azimuth configuration and operation, therefore can not be interpreted as limiting the scope of the invention.
Fig. 1 is the schematic annexation figure with the list inspection debug system of real-time simulation power of test according to a first embodiment of the present invention.
The list inspection debug system with real-time simulation power of test as shown in Figure 1 comprises testing and control computing machine 1, switch 2, discrete magnitude simulation testing device 3, analog quantity simulation testing device 4, clock synchronization device 6, switching conditioning case 7 and Bus simulator proving installation 5.Switch 2 is connected with testing and control computing machine 1; Discrete magnitude simulation testing device 3 is connected with switch 2; Analog quantity simulation testing device 4 is connected with switch 2; Bus simulator proving installation 5 is connected with switch 2; Clock synchronization device 6 is connected with switch 2; Switching conditioning case 7 is connected with discrete magnitude simulation testing device 3, analog quantity simulation testing device 4, Bus simulator proving installation 5 and avionics device 8 to be measured respectively; Wherein, testing and control computing machine 1 and switch 2 are for mutual transmission of signal; Switch 2 passes to discrete magnitude simulation testing device 3, analog quantity simulation testing device 4 and/or Bus simulator proving installation 5 for the control signal transmitted by testing and control computing machine 1 and the feedback signal of discrete magnitude simulation testing device 3, analog quantity simulation testing device 4 and/or Bus simulator proving installation 5 is passed to testing and control computing machine 1; Discrete magnitude simulation testing device 3, analog quantity simulation testing device 4 and Bus simulator proving installation 5 for the control signal according to testing and control computing machine 1, and are transmitted or collecting work signal to avionics device 8 to be measured by switching conditioning case 7; Clock synchronization device 6 for synchronization discrete amount simulation testing device 3, analog quantity simulation testing device 4 and Bus simulator proving installation 5 the working signal that transmits or gather.
In the present embodiment, switching conditioning case 7 is connected with switch 2 further, debug signal for debug signal is passed to switch 2, and is passed to switching conditioning case 7 by switch 2 by testing and control computing machine 1, thus by switching conditioning case 7, debug signal is passed to avionics device 8 to be measured.
In an alternative embodiment, the list inspection debug system with real-time simulation power of test comprises serial server further, serial server is respectively with switch and transfer and nurse one's health case and be connected, the debug signal passing to switch that serial server is used for being sent by testing and control computing machine passes to switching conditioning case, thus by switching conditioning case, debug signal is passed to avionics device to be measured.
Advantageously, described switch is Ethernet switch.
Finally it is to be noted: above embodiment only in order to technical scheme of the present invention to be described, is not intended to limit.Although with reference to previous embodiment to invention has been detailed description, those of ordinary skill in the art is to be understood that: it still can be modified to the technical scheme described in foregoing embodiments, or carries out equivalent replacement to wherein portion of techniques feature; And these amendments or replacement, do not make the essence of appropriate technical solution depart from the spirit and scope of various embodiments of the present invention technical scheme.

Claims (4)

1. have real-time simulation power of test list inspection a debug system, it is characterized in that, described in have real-time simulation power of test list inspection debug system comprise:
Testing and control computing machine (1);
Switch (2), described switch (2) is connected with described testing and control computing machine (1);
Discrete magnitude simulation testing device (3), described discrete magnitude simulation testing device (3) is connected with described switch (2);
Analog quantity simulation testing device (4), described analog quantity simulation testing device (4) is connected with described switch (2);
Bus simulator proving installation (5), described Bus simulator proving installation (5) is connected with described switch (2);
Clock synchronization device (6), described clock synchronization device (6) is connected with described switch (2);
Switching conditioning case (7), described switching conditioning case (7) is connected with described discrete magnitude simulation testing device (3), analog quantity simulation testing device (4), Bus simulator proving installation (5) and avionics device to be measured (8) respectively; Wherein,
Described testing and control computing machine (1) and described switch (2) are for mutual transmission of signal; Described switch (2) passes to described discrete magnitude simulation testing device (3), analog quantity simulation testing device (4) and/or Bus simulator proving installation (5) for the control signal described testing and control computing machine (1) transmitted and the feedback signal of described discrete magnitude simulation testing device (3), analog quantity simulation testing device (4) and/or Bus simulator proving installation (5) is passed to described testing and control computing machine (1); Described discrete magnitude simulation testing device (3), analog quantity simulation testing device (4) and Bus simulator proving installation (5) for the control signal according to described testing and control computing machine (1), and are transmitted or collecting work signal to described avionics device (8) to be measured by described switching conditioning case (7); The working signal that described clock synchronization device (6) transmits for synchronous described discrete magnitude simulation testing device (3), analog quantity simulation testing device (4) and Bus simulator proving installation (5) or gathers.
2. there is the list inspection debug system of real-time simulation power of test as claimed in claim 1, it is characterized in that, described switching conditioning case (7) is connected with switch (2) further, described testing and control computing machine (1) is for passing to described switch (2) by debug signal, and by switch (2), debug signal is passed to switching conditioning case (7), thus by switching conditioning case (7), debug signal is passed to avionics device (8) to be measured.
3. there is the list inspection debug system of real-time simulation power of test as claimed in claim 2, it is characterized in that, the described list inspection debug system with real-time simulation power of test comprises serial server further, described serial server is respectively with switch and transfer and nurse one's health case and be connected, the debug signal passing to switch that described serial server is used for being sent by testing and control computing machine passes to described switching conditioning case, thus by switching conditioning case, debug signal is passed to avionics device to be measured.
4. the list inspection debug system with real-time simulation power of test as described in claims 1 to 3, it is characterized in that, described switch is Ethernet switch.
CN201510828733.9A 2015-11-24 2015-11-24 Single test debugging system with real-time simulation test capability Pending CN105372530A (en)

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106526254A (en) * 2016-12-20 2017-03-22 中国航天空气动力技术研究院 Unmanned aerial vehicle airborne avionics device test signal switching device box
CN106844127A (en) * 2017-02-13 2017-06-13 北京航天发射技术研究所 A kind of highly reliable modular testing emulation platform
CN109270918A (en) * 2018-08-17 2019-01-25 国营芜湖机械厂 A kind of aircraft avionics floor synthetic debugging system based on performance test
CN110781557A (en) * 2019-10-14 2020-02-11 中国航空工业集团公司沈阳飞机设计研究所 Aircraft system model simulation test flow optimization method

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1949180A (en) * 2006-09-18 2007-04-18 中国航天时代电子公司第七七一研究所 Structuring method of distributed type simulated testing system series based on signal classification
CN101575011A (en) * 2009-05-05 2009-11-11 中国民航大学 Automatic test equipment of boeing series aircraft audio management unit and 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
CN101900772A (en) * 2010-06-18 2010-12-01 中国航天科技集团公司第五研究院第五一三研究所 Box equivalent device
CN201829074U (en) * 2010-09-28 2011-05-11 北京赛四达科技股份有限公司 Avionics simulation testing and training device
CN202275399U (en) * 2011-06-22 2012-06-13 北京航天自动控制研究所 Debugging verification system for embedded software
CN203012504U (en) * 2012-11-30 2013-06-19 中国航空工业集团公司沈阳飞机设计研究所 Distributed-type avionics integrated test system
CN203064208U (en) * 2013-02-07 2013-07-17 四川海特高新技术股份有限公司 Integral test equipment applied to aircraft instrument
CN104360188A (en) * 2014-11-10 2015-02-18 绵阳市维博电子有限责任公司 Testing device for telemetry system

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1949180A (en) * 2006-09-18 2007-04-18 中国航天时代电子公司第七七一研究所 Structuring method of distributed type simulated testing system series based on signal classification
CN101575011A (en) * 2009-05-05 2009-11-11 中国民航大学 Automatic test equipment of boeing series aircraft audio management unit and method thereof
CN101900772A (en) * 2010-06-18 2010-12-01 中国航天科技集团公司第五研究院第五一三研究所 Box equivalent device
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
CN201829074U (en) * 2010-09-28 2011-05-11 北京赛四达科技股份有限公司 Avionics simulation testing and training device
CN202275399U (en) * 2011-06-22 2012-06-13 北京航天自动控制研究所 Debugging verification system for embedded software
CN203012504U (en) * 2012-11-30 2013-06-19 中国航空工业集团公司沈阳飞机设计研究所 Distributed-type avionics integrated test system
CN203064208U (en) * 2013-02-07 2013-07-17 四川海特高新技术股份有限公司 Integral test equipment applied to aircraft instrument
CN104360188A (en) * 2014-11-10 2015-02-18 绵阳市维博电子有限责任公司 Testing device for telemetry system

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106526254A (en) * 2016-12-20 2017-03-22 中国航天空气动力技术研究院 Unmanned aerial vehicle airborne avionics device test signal switching device box
CN106526254B (en) * 2016-12-20 2023-11-03 中国航天空气动力技术研究院 Unmanned aerial vehicle airborne avionics test signal switching equipment box
CN106844127A (en) * 2017-02-13 2017-06-13 北京航天发射技术研究所 A kind of highly reliable modular testing emulation platform
CN106844127B (en) * 2017-02-13 2019-04-05 北京航天发射技术研究所 A kind of highly reliable modular testing emulation platform
CN109270918A (en) * 2018-08-17 2019-01-25 国营芜湖机械厂 A kind of aircraft avionics floor synthetic debugging system based on performance test
CN110781557A (en) * 2019-10-14 2020-02-11 中国航空工业集团公司沈阳飞机设计研究所 Aircraft system model simulation test flow optimization method
CN110781557B (en) * 2019-10-14 2023-04-07 中国航空工业集团公司沈阳飞机设计研究所 Aircraft system model simulation test flow optimization method

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