CN113721090A - Universal weapon system input and output line checking method - Google Patents
Universal weapon system input and output line checking method Download PDFInfo
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- CN113721090A CN113721090A CN202110904688.6A CN202110904688A CN113721090A CN 113721090 A CN113721090 A CN 113721090A CN 202110904688 A CN202110904688 A CN 202110904688A CN 113721090 A CN113721090 A CN 113721090A
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- G01R—MEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
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Abstract
The application relates to the technical field of design of a weapon system of a fighter plane, in particular to a universal method for checking input and output lines of a weapon system, which comprises the steps of S1, sending operation prompts of a weapon control switch in an cockpit to a display, and collecting input switching values at the display end; step S2, after receiving the input switching value of the display end, supplying a first electric signal to a hanging point associated with the universal signal inspection equipment of the weapon system, and acquiring hanging point information fed back by the universal signal inspection equipment of the weapon system; step S3, continuously supplying a second electric signal to the hanging point, and acquiring hanging point execution information fed back by the universal signal inspection equipment of the weapon system; and step S4, interpreting the hanging point information and the hanging point execution information, and determining whether the input and output circuit of the weapon system is abnormal. The application can save the cost of the inspection tester, can greatly shorten the power-on inspection time of the weapon system, and has the advantage of simplifying the operation flow of operators.
Description
Technical Field
The application relates to the technical field of design of weapon systems of fighters, in particular to a universal method for checking input and output lines of a weapon system.
Background
The existing aircraft weapon system line inspection needs to be carried out by depending on the firing control flow of the weapon, and the inspection method has the following two defects:
a) when a plurality of weapons are matched with a hanging scheme at a single hanging point, all signals of the hanging point can be checked completely only by carrying out power-on check on a plurality of weapons;
b) depending on the inspection of the weapon flow, the next inspection can be carried out only by waiting for the heating time of the real weapon.
The two points directly cause the power-on inspection operation steps of the weapon system to be complicated, the consumed time is long, and the requirement on operators is high. .
Disclosure of Invention
Aiming at the problems existing in the conventional weapon system power-on inspection, the invention provides a novel method for inspecting the power-on of the weapon system, so as to achieve the simple and rapid inspection of the input and output lines of the weapon system.
The application provides a universal weapon system input and output line checking method, which mainly comprises the following steps:
step S1, sending an operation prompt of a weapon control switch in the cabin to the display, and collecting input switching value of the display end;
step S2, after receiving the input switching value of the display end, supplying a first electric signal to a hanging point associated with a universal signal inspection device of the weapon system, wherein the first electric signal is an electric signal for enabling the hanging point to be in a standby state, and acquiring hanging point information fed back by the universal signal inspection device of the weapon system;
step S3, continuously supplying a second electric signal to the hanging point, wherein the second electric signal comprises a plurality of electric signals which are set for a short time and used for controlling the hanging point, and hanging point execution information fed back by the universal signal inspection equipment of the weapon system is obtained;
and step S4, interpreting the hanging point information and the hanging point execution information, and determining whether the input and output circuit of the weapon system is abnormal.
Preferably, step S1 is preceded by the step of obtaining a command stimulus from the display and a hard-wire stimulus from the ground preparation device of the onboard weapon, and determining that both are valid signals.
Preferably, in step S2, the first electric signal is a first direct current of the set voltage.
Preferably, in step S2, the obtained hanging point information includes hanging object description information of the hanging point, a ground signal, an address signal, and signal state information of the first electrical signal.
Preferably, in step S3, the second electrical signal includes: a second direct current of a set voltage, an electrical signal for enabling the dosing, an electrical signal for dosing, and a 115 vac electrical signal.
Preferably, in step S3, the set short time is 2S.
Preferably, when steps S2 and S3 are executed, the method further includes sending a control command to the crosslinking system for controlling the crosslinking system to send a signal excitation to the weapon system universal signal inspection device.
Preferably, after step S4, the method further includes sending the detection result to a display terminal for displaying.
Another aspect of the present application provides an electronic device, which includes a memory, a processor, and a computer program stored in the memory and capable of running on the processor, and when the processor executes the computer program, the method for checking input/output lines of a weapon system is implemented as above.
Another aspect of the present application provides a computer-readable storage medium storing a computer program, which when executed by a processor can implement the above general weapon system input/output line inspection method.
The existing power-on check of the weapon system needs to be connected with a multiple weapon detector, the correctness of the input and output signals of the weapon system can be verified only by carrying out the power-on check of multiple weapons according to the weapon flow, and the input and output signals of all weapon systems can be checked only by connecting one universal signal check device of the weapon system according to the check method provided by the invention. The cost of the inspection tester can be saved, the power-on inspection time of a weapon system can be greatly shortened, the operation requirement on operators is low, and only corresponding switches need to be switched on according to the prompt of a display.
Drawings
FIG. 1 is a sampling flow diagram of a weapon system input/output line inspection method, as generally described herein.
Fig. 2 is a schematic view of a preferred embodiment of the electronic device 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 a universal weapon system input and output line checking method, which mainly comprises the following steps:
step S1, sending an operation prompt of a weapon control switch in the cabin to the display, and collecting input switching value of the display end;
step S2, after receiving the input switching value of the display end, supplying a first electric signal to a hanging point associated with a universal signal inspection device of the weapon system, wherein the first electric signal is an electric signal for enabling the hanging point to be in a standby state, and acquiring hanging point information fed back by the universal signal inspection device of the weapon system;
step S3, continuously supplying a second electric signal to the hanging point, wherein the second electric signal comprises a plurality of electric signals which are set for a short time and used for controlling the hanging point, and hanging point execution information fed back by the universal signal inspection equipment of the weapon system is obtained;
and step S4, interpreting the hanging point information and the hanging point execution information, and determining whether the input and output circuit of the weapon system is abnormal.
The method comprises the steps that the onboard weapon control assembly executes the steps, as shown in fig. 1, receives instruction excitation and hard-line excitation signals, enters a maintenance inspection process, gives an operation prompt to be displayed on a display of a cockpit, an operator operates a weapon control switch according to the prompt, the onboard weapon control assembly collects the state of the control switch, sends the collection result to the display in the cockpit to be displayed, then the weapon control assembly gives the next operation prompt, and inspection of input switch signals of all weapon systems is sequentially realized; after the input switch signals of the weapon system are checked, the onboard weapon control component automatically enters the checking of the universal signals of the weapon system. Connecting universal signal inspection equipment of a weapon system at a weapon interface end, giving out a signal excitation to the weapon interface end by an onboard weapon control assembly, carrying out signal acquisition by the universal signal inspection equipment of the weapon system, and sending an acquisition result to the onboard weapon control assembly to realize the inspection of the universal signal of the weapon system interface end; after the onboard weapon control assembly enters a maintenance inspection state, the system simultaneously sends out a weapon maintenance inspection instruction to other cross-linking systems, the other systems send high-bandwidth signals to a weapon system line, a weapon interface end is connected with universal signal inspection equipment of the weapon system, the high-bandwidth signals are acquired, an acquisition result is sent to the onboard weapon control assembly, and the inspection of the high-bandwidth signals of the weapon interface end is realized. And after integrating the signal acquisition results of the hanging point end by the weapon control assembly, transmitting the acquisition results to a display in the cabin for displaying.
The specific inspection flow is as follows:
a) the onboard weapon control assembly firstly collects instruction excitation given by an operator in a cabin, collects hard-line excitation given by an onboard weapon ground preparation device, and enters a maintenance inspection flow after the instruction excitation and the hard-line excitation are both met.
b) The onboard weapon control component sends an indication of the operation of the weapon control switch in the cabin to the display, awaiting the collection of the switch state.
c) And the onboard weapon control component judges the input switching values, wherein the selection position of the emergency jettison knob is 1, the non-selection position is 0, the judgment result is correct, the acquisition results of other switching values are changed from 0 to 1 and judged to be correct, and the onboard weapon control component judges the inspection result and then sends the inspection result to a display in the cabin for displaying.
d) After the input switch signals of the weapon system are checked, the onboard weapon control component automatically enters the checking of the universal signals of the weapon system.
e) And the on-board weapon control component supplies a first electric signal to a hanging point existing in interlocking, the first electric signal is a first direct current, and the universal signal inspection equipment of the weapon system reports suspension description information, a ground signal, an address signal and signal state information of the first direct current to the on-board weapon control component after receiving the power supply of the first direct current.
f) If the hanging object is received and a hanging point is described not to be the universal signal checking equipment of the weapon system or the identification is failed, the onboard weapon control component finishes the maintenance and inspection process. If the identification is the universal signal inspection equipment of the weapon system, the onboard weapon control component judges the acquisition result, records the inspection result, and reports the inspection result uniformly after all the signals are inspected.
The onboard weapon control module then supplies a second electrical signal to the hang point where the interlock exists, including the following steps g-n.
g) And the onboard weapon control component supplies direct current 2 electricity to a hanging point existing in the universal signal check equipment of the weapon system, withdraws the pin by 2s, and reports the DC2 state to the onboard weapon control component.
h) And the onboard weapon control component judges the checking result, the DC2 state is changed from 0 to 1 and then to 0, the judging result is correct, otherwise, the onboard weapon control component is in failure, records the checking result, and reports the checking result uniformly after all signals are checked.
i) And the onboard weapon control component supplies throwing permission power to a hanging point existing in the universal signal inspection equipment of the weapon system, withdraws the pin by 2s, and reports a throwing permission state to the onboard weapon control component.
j) And the onboard weapon control component judges the checking result, the throwing permission state is changed from 0 to 1 and then to 0, the judging result is correct, otherwise, the onboard weapon control component is in failure, records the checking result, and reports the checking result uniformly after all signals are checked.
k) And the onboard weapon control component supplies normal throwing and discharging to a hanging point existing in the universal signal inspection equipment of the weapon system, the pin is withdrawn for 2s, and the universal signal inspection equipment of the weapon system reports a normal throwing state to the onboard weapon control component.
l) the onboard weapon control component judges the inspection result, the normal throwing state is changed from 0 to 1 and then to 0, the judgment result is correct, otherwise, the onboard weapon control component is in failure, records the inspection result, and reports the inspection result uniformly after all signals are inspected.
m) supplying alternating current 115V power to a hanging point existing in universal signal inspection equipment of a weapon system by the onboard weapon control component, withdrawing the pin by 2s, and reporting the 115V power state to the onboard weapon control component by the universal signal inspection equipment of the weapon system.
n) the onboard weapon control component judges the inspection result, the alternating current 115V state is changed from 0 to 1 and then to 0, the judgment result is correct, otherwise, the onboard weapon control component is in failure, records the inspection result, and reports the inspection result uniformly after all signals are inspected.
o) after the onboard weapon control component enters a maintenance inspection state, the system simultaneously sends out weapon maintenance inspection instruction excitation to other cross-linked systems. Other cross-linking systems transmit high bandwidth signals to weapons systems universal signal inspection devices.
p) weapon system universal signal inspection equipment interprets the high bandwidth signal and reports on-board weapon control component high bandwidth signal status.
And q) after the maintenance inspection is finished, reporting the maintenance inspection result of each weapon hanging point by an onboard weapon control assembly, sequentially displaying the inspection completion condition of each weapon hanging point on the onboard, and inquiring a health picture of a display if a fault occurs.
By adopting the inspection method, the input and output signals of all weapon system systems can be inspected, an operator only needs to switch on or off the related weapon control switches in the cabin according to the operation prompt on the display, the inspection of other signals is completed by automatic control of the system, and after the inspection is finished, the operator can check the inspection result on the display in the cabin, and if fault information exists, the inspection can be carried out through the display.
The application also provides an electronic device, which comprises a memory, a processor and a computer program stored in the memory and capable of running on the processor, wherein the processor executes the computer program to realize the universal weapon system input and output line checking method.
The present application also provides a computer-readable storage medium storing a computer program, which when executed by a processor, is capable of implementing the above general weapon system input/output line inspection method.
FIG. 2 is an exemplary block diagram of an electronic device capable of implementing functionality provided in accordance with one embodiment of the present application. As shown in fig. 2, the electronic device includes an input device 501, an input interface 502, a central processor 503, a memory 504, an output interface 505, and an output device 506. The input interface 502, the central processing unit 503, the memory 504 and the output interface 505 are connected to each other through a bus 507, and the input device 501 and the output device 506 are connected to the bus 507 through the input interface 502 and the output interface 505, respectively, and further connected to other components of the electronic device. Specifically, the input device 504 receives input information from the outside and transmits the input information to the central processor 503 through the input interface 502; the central processor 503 processes input information based on computer-executable instructions stored in the memory 504 to generate output information, temporarily or permanently stores the output information in the memory 504, and then transmits the output information to the output device 506 through the output interface 505; the output device 506 outputs the output information to the outside of the electronic device for use by the user.
That is, the electronic device shown in fig. 2 may also be implemented to include: a memory storing computer-executable instructions; and one or more processors that when executing computer executable instructions may implement the unmanned aerial vehicle autonomous homing model training method described in connection with fig. 1.
In one embodiment, the electronic device shown in fig. 2 may be implemented to include: a memory 504 configured to store executable program code; one or more processors 503 configured to execute executable program code stored in the memory 504 to perform the universal weapon system input output line checking method in the above-described embodiments.
In a typical configuration, a computing device includes one or more processors (CPUs), input/output interfaces, network interfaces, and memory.
The memory may include forms of volatile memory in a computer readable medium, Random Access Memory (RAM) and/or non-volatile memory, such as Read Only Memory (ROM) or flash memory (flash RAM). Memory is an example of a computer-readable medium.
Computer-readable media include both non-transitory and non-transitory, removable and non-removable media that implement information storage by any method or technology. The information may be computer readable instructions, data structures, modules of a program, or other data. Examples of computer storage media include, but are not limited to, phase change memory (PRAM), Static Random Access Memory (SRAM), Dynamic Random Access Memory (DRAM), other types of Random Access Memory (RAM), Read Only Memory (ROM), Electrically Erasable Programmable Read Only Memory (EEPROM), flash memory or other memory technology, compact disc read only memory (CD-ROM), Digital Versatile Discs (DVD) or other optical storage, magnetic cassettes, magnetic tape, magnetic disk storage or other magnetic storage devices, or any other non-transmission medium that can be used to store information that can be accessed by a computing device.
As will be appreciated by one skilled in the art, embodiments of the present application may be provided as a method, system, or computer program product. Accordingly, the present application may take the form of an entirely hardware embodiment, an entirely software embodiment or an embodiment combining software and hardware aspects. Furthermore, the present application may take the form of a computer program product embodied on one or more computer-usable storage media (including, but not limited to, disk storage, CD-ROM, optical storage, and the like) having computer-usable program code embodied therein.
Furthermore, it will be obvious that the term "comprising" does not exclude other elements or steps. A plurality of units, modules or devices recited in the device claims may also be implemented by one unit or overall device by software or hardware. The terms first, second, etc. are used to identify names, but not any particular order.
The flowchart and block diagrams in the figures illustrate the architecture, functionality, and operation of possible implementations of systems, methods and computer program products according to various embodiments of the present application. In this regard, each block in the flowchart or block diagrams may represent a module, segment, or portion of code, which comprises one or more executable instructions for implementing the specified logical function(s). It should also be noted that, in some alternative implementations, the functions noted in the block may occur out of the order noted in the figures. For example, two blocks identified in succession may, in fact, be executed substantially concurrently, or the blocks may sometimes be executed in the reverse order, depending upon the functionality involved. It will also be noted that each block of the block diagrams and/or flowchart illustration, and combinations of blocks in the block diagrams and/or flowchart illustration, can be implemented by special purpose hardware-based systems which perform the specified functions or acts, or combinations of special purpose hardware and computer instructions.
The Processor in this embodiment may be a Central Processing Unit (CPU), other general purpose Processor, a Digital Signal Processor (DSP), an Application Specific Integrated Circuit (ASIC), an off-the-shelf Programmable Gate Array (FPGA) or other Programmable logic device, a discrete Gate or transistor logic device, a discrete hardware component, and so on. A general purpose processor may be a microprocessor or the processor may be any conventional processor or the like.
The memory may be used to store computer programs and/or modules, and the processor may implement various functions of the apparatus/terminal device by running or executing the computer programs and/or modules stored in the memory, as well as by invoking data stored in the memory. The memory may mainly include a storage program area and a storage data area, wherein the storage program area may store an operating system, an application program required by at least one function (such as a sound playing function, an image playing function, etc.), and the like; the storage data area may store data (such as audio data, a phonebook, etc.) created according to the use of the cellular phone, and the like. In addition, the memory may include high speed random access memory, and may also include non-volatile memory, such as a hard disk, a memory, a plug-in hard disk, a Smart Media Card (SMC), a Secure Digital (SD) Card, a Flash memory Card (Flash Card), at least one magnetic disk storage device, a Flash memory device, or other volatile solid state storage device.
In this embodiment, the module/unit integrated with the apparatus/terminal device may be stored in a computer-readable storage medium if it is implemented in the form of a software functional unit and sold or used as a separate product. Based on such understanding, all or part of the flow in the method according to the embodiments of the present invention may also be implemented by a computer program, which may be stored in a computer-readable storage medium and used by a processor to implement the steps of the above-described embodiments of the method. Wherein the computer program comprises computer program code, which may be in the form of source code, object code, an executable file or some intermediate form, etc. The computer readable medium may include: any entity or device capable of carrying computer program code, recording medium, U.S. disk, removable hard disk, magnetic disk, optical disk, computer Memory, Read-Only Memory (ROM), Random Access Memory (RAM), electrical carrier wave signals, telecommunications signals, software distribution media, and the like.
It should be noted that the computer readable medium may contain content that is appropriately increased or decreased as required by legislation and patent practice in the jurisdiction. Although the present application has been described with reference to the preferred embodiments, it is not intended to limit the present application, and those skilled in the art can make variations and modifications without departing from the spirit and scope of the present application.
Although the invention has been described in detail hereinabove with respect to a general description and specific embodiments thereof, it will be apparent to those skilled in the art that modifications or improvements may be made thereto based on the invention. Accordingly, such modifications and improvements are intended to be within the scope of the invention as claimed.
Claims (10)
1. A universal weapon system input/output line checking method is characterized by comprising the following steps:
step S1, sending an operation prompt of a weapon control switch in the cabin to the display, and collecting input switching value of the display end;
step S2, after receiving the input switching value of the display end, supplying a first electric signal to a hanging point associated with a universal signal inspection device of the weapon system, wherein the first electric signal is an electric signal for enabling the hanging point to be in a standby state, and acquiring hanging point information fed back by the universal signal inspection device of the weapon system;
step S3, continuously supplying a second electric signal to the hanging point, wherein the second electric signal comprises a plurality of electric signals which are set for a short time and used for controlling the hanging point, and hanging point execution information fed back by the universal signal inspection equipment of the weapon system is obtained;
and step S4, interpreting the hanging point information and the hanging point execution information, and determining whether the input and output circuit of the weapon system is abnormal.
2. The method of checking input/output lines of a universal weapon system according to claim 1, wherein step S1 is preceded by the steps of obtaining command stimuli from the display and hard-wired stimuli from the ground preparation device of the on-board weapon, and determining that both are valid signals.
3. The method for inspecting input/output lines of a universal weapon system according to claim 1, wherein in step S2, said first electrical signal is a first direct current of a set voltage.
4. The universal weapon system input-output line inspection method according to claim 1, wherein in step S2, the acquired hanging point information includes hanging object description information of the hanging point, a ground signal, an address signal, and signal status information of the first electrical signal.
5. The universal weapon system input output line inspection method according to claim 1, wherein in step S3, said second electrical signal comprises: a second direct current of a set voltage, an electrical signal for enabling the dosing, an electrical signal for dosing, and a 115 vac electrical signal.
6. The method for checking input/output lines of a universal weapon system according to claim 1, wherein in step S3, the set time is 2S.
7. The universal weapon system input-output line inspection method according to claim 1, wherein when executing steps S2 and S3, further comprising sending control instructions to the cross-linking system for controlling the cross-linking system to send signal stimuli to the weapon system universal signal inspection device.
8. The method for checking input/output lines of a universal weapon system according to claim 1, wherein after step S4, the method further comprises sending the detection result to a display terminal for displaying.
9. An electronic device, comprising a memory, a processor, and a computer program stored in the memory and capable of running on the processor, wherein the processor executes the computer program to implement the above general weapon system input/output line checking method.
10. A computer-readable storage medium, characterized in that the computer-readable storage medium stores a computer program, which when executed by a processor, is capable of implementing the universal weapon system input output line checking method as above.
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Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5614896A (en) * | 1995-03-23 | 1997-03-25 | Hughes Missile Systems Company | Method and system for aircraft weapon station testing |
| US20050030006A1 (en) * | 2003-04-28 | 2005-02-10 | Leonard James V. | Test adapter for a weapon store test set |
| US20050081733A1 (en) * | 2003-08-13 | 2005-04-21 | Leonard James V. | Methods and apparatus for testing and diagnosis of weapon control systems |
| RU2008102709A (en) * | 2008-01-29 | 2009-08-10 | Открытое акционерное общество "Корпорация "Тактическое ракетное вооружение" (RU) | METHOD FOR SIMULATING ELECTRICAL AND INFORMATION INTERACTION OF ROCKET WITH CARRIER EQUIPMENT AND DEVICE FOR ITS IMPLEMENTATION |
| US7768444B1 (en) * | 2008-01-29 | 2010-08-03 | Rourk Christopher J | Weapon detection and elimination system |
| US20120078554A1 (en) * | 2010-09-27 | 2012-03-29 | Gagnon Reinhard J | Systems And Methods For Determining A Status Of An Electrical Coupling |
| CN103760439A (en) * | 2013-09-24 | 2014-04-30 | 中国航空工业集团公司沈阳飞机设计研究所 | Automatic test system of avionic system |
| CN105866578A (en) * | 2016-04-01 | 2016-08-17 | 中航飞机股份有限公司西安飞机分公司 | Airplane standard hanger management system detection method |
| CN111323734A (en) * | 2020-03-28 | 2020-06-23 | 芜湖航翼集成设备有限公司 | General detection system and detection method for conductivity of external hanging device of airplane weapon |
-
2021
- 2021-08-07 CN CN202110904688.6A patent/CN113721090B/en active Active
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5614896A (en) * | 1995-03-23 | 1997-03-25 | Hughes Missile Systems Company | Method and system for aircraft weapon station testing |
| US20050030006A1 (en) * | 2003-04-28 | 2005-02-10 | Leonard James V. | Test adapter for a weapon store test set |
| US20050081733A1 (en) * | 2003-08-13 | 2005-04-21 | Leonard James V. | Methods and apparatus for testing and diagnosis of weapon control systems |
| RU2008102709A (en) * | 2008-01-29 | 2009-08-10 | Открытое акционерное общество "Корпорация "Тактическое ракетное вооружение" (RU) | METHOD FOR SIMULATING ELECTRICAL AND INFORMATION INTERACTION OF ROCKET WITH CARRIER EQUIPMENT AND DEVICE FOR ITS IMPLEMENTATION |
| US7768444B1 (en) * | 2008-01-29 | 2010-08-03 | Rourk Christopher J | Weapon detection and elimination system |
| US20120078554A1 (en) * | 2010-09-27 | 2012-03-29 | Gagnon Reinhard J | Systems And Methods For Determining A Status Of An Electrical Coupling |
| CN103760439A (en) * | 2013-09-24 | 2014-04-30 | 中国航空工业集团公司沈阳飞机设计研究所 | Automatic test system of avionic system |
| CN105866578A (en) * | 2016-04-01 | 2016-08-17 | 中航飞机股份有限公司西安飞机分公司 | Airplane standard hanger management system detection method |
| CN111323734A (en) * | 2020-03-28 | 2020-06-23 | 芜湖航翼集成设备有限公司 | General detection system and detection method for conductivity of external hanging device of airplane weapon |
Non-Patent Citations (3)
| Title |
|---|
| ZHANG LI 等: "Design and analysis of electronic lock workflow for weapon starting based on timed Petri net", 《2010 INTERNATIONAL CONFERENCE ON COMPUTER APPLICATION AND SYSTEM MODELING (ICCASM 2010)》, pages 8 * |
| 李国帅 等: "某型飞机武器模拟训练系统的设计与实现", 《长春理工大学学报(自然科学版)》, vol. 33, no. 1, pages 137 - 140 * |
| 李青 等: "某型军用飞机外挂物管理系统应用潜力分析", 《火力与指挥控制》, vol. 26, no. 1, pages 47 - 50 * |
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