CN113721090B - Input/output circuit inspection method for universal weapon system - Google Patents
Input/output circuit inspection method for universal weapon system Download PDFInfo
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- CN113721090B CN113721090B CN202110904688.6A CN202110904688A CN113721090B CN 113721090 B CN113721090 B CN 113721090B CN 202110904688 A CN202110904688 A CN 202110904688A CN 113721090 B CN113721090 B CN 113721090B
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- 238000003860 storage Methods 0.000 claims description 18
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- 238000004132 cross linking Methods 0.000 claims description 7
- 238000001514 detection method Methods 0.000 claims description 4
- 238000002360 preparation method Methods 0.000 claims description 3
- 238000013461 design Methods 0.000 abstract description 2
- 238000012423 maintenance Methods 0.000 description 9
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- G01R—MEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
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Abstract
The application relates to the technical field of fighter aircraft weapon system design, in particular to a general weapon system input/output line inspection method, which comprises the following steps of S1, sending an operation prompt of a weapon control switch in a cockpit to a display, and collecting input switching value of the display; step S2, after receiving input switching value of a display end, supplying a first electric signal to a hanging point associated with weapon system general signal checking equipment, and acquiring hanging point information fed back by the weapon system general signal checking equipment; step S3, continuing to supply a second electric signal to the hanging point, and acquiring hanging point execution information fed back by the weapon system general signal checking equipment; and S4, judging the hanging point information and the hanging point execution information, and determining whether an input and output line of the weapon system is abnormal. The application can save the cost of the inspection instrument, greatly shorten the power-on inspection time of the weapon system and simplify the operation flow of operators.
Description
Technical Field
The application relates to the technical field of fighter aircraft weapon system design, in particular to a general weapon system input/output line inspection method.
Background
The existing aircraft weapon system line inspection needs to be carried out by relying on the weapon launching and controlling flow, and the inspection method has the following two defects:
a) When a plurality of weapon hanging schemes exist at a single hanging point, the electrifying inspection of the multi-type weapon is needed to be carried out, and all signals of the hanging point can be inspected completely;
b) Depending on the checking of the weapon flow, the next checking can be performed only by waiting for the heating time of the real weapon.
The two points directly lead to complicated operation steps of the power-on inspection of the weapon system, the time consumption is long, and the requirement on operators is high. .
Disclosure of Invention
Aiming at the problems existing in the current weapon system power-on inspection, the application provides a novel weapon system power-on inspection method, which achieves the simple and rapid inspection of input and output lines of the weapon system.
The application provides a general weapon system input/output line checking method, which mainly comprises the following steps:
step S1, sending an operation prompt of a weapon control switch in a cabin to a display, and collecting input switching value of the display end;
step S2, after receiving input switching value of a display end, supplying a first electric signal to a hanging point associated with weapon system general signal checking equipment, wherein the first electric signal is an electric signal enabling the hanging point to be in a standby state, and acquiring hanging point information fed back by the weapon system general signal checking equipment;
step S3, continuously supplying a second electric signal to the hanging point, wherein the second electric signal comprises a plurality of electric signals for controlling the hanging point in a short time, and acquiring hanging point execution information fed back by the weapon system universal signal checking equipment;
and S4, judging the hanging point information and the hanging point execution information, and determining whether an input and output line of the weapon system is abnormal.
Preferably, step S1 is preceded by further comprising obtaining an instruction excitation given by the display end and a hard wire excitation given by the ground preparation device of the weapon on board, and judging both as valid signals.
Preferably, in step S2, the first electrical signal is a first direct current of a set voltage.
Preferably, in step S2, the obtained hanging point information includes hanging object description information, a ground signal, an address signal, and signal state information of the first electrical signal of the hanging point.
Preferably, in step S3, the second electrical signal includes: a second direct current of set voltage, an electrical signal for allowing the delivery, an electrical signal for the delivery, and a 115V alternating current electrical signal.
Preferably, in step S3, the set short time is 2S.
Preferably, when executing step S2 and step S3, the method further comprises sending a control instruction to a crosslinking system for controlling the crosslinking system to send a signal excitation to the weapon system general purpose signal inspection device.
Preferably, after step S4, the method further includes sending the detection result to a display end for display.
In another aspect the application provides an electronic device comprising a memory, a processor and a computer program stored in the memory and capable of running on the processor, the processor implementing a weapon system input output line inspection method as above in general when executing the computer program.
Another aspect of the application provides a computer readable storage medium storing a computer program which, when executed by a processor, enables the implementation of a general weapon system input output line inspection method as described above.
The existing weapon system power-on inspection needs to be connected with a multi-type weapon inspection instrument, the correctness of input and output signals of the weapon system can be verified by carrying out the multi-type weapon power-on inspection according to the weapon flow. The cost of the inspection instrument can be saved, the electrifying inspection time of the weapon system can be greatly shortened, meanwhile, the operation requirement on operators is low, and the corresponding switch is only required to be turned on according to the prompt of the display.
Drawings
FIG. 1 is a sample flow chart of a method for checking input/output lines of a weapon system in accordance with the present application.
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 objects, technical solutions and advantages of the present application become more apparent, the technical solutions in the embodiments of the present application will be described in more detail 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 application. The embodiments described below by referring to the drawings are exemplary and intended to illustrate the present application and should not be construed as limiting the application. All other embodiments, based on the embodiments of the application, which are apparent to those of ordinary skill in the art without inventive faculty, are intended to be within the scope of the application. Embodiments of the present application will be described in detail below with reference to the accompanying drawings.
The application provides a general weapon system input/output line checking method, which mainly comprises the following steps:
step S1, sending an operation prompt of a weapon control switch in a cabin to a display, and collecting input switching value of the display end;
step S2, after receiving input switching value of a display end, supplying a first electric signal to a hanging point associated with weapon system general signal checking equipment, wherein the first electric signal is an electric signal enabling the hanging point to be in a standby state, and acquiring hanging point information fed back by the weapon system general signal checking equipment;
step S3, continuously supplying a second electric signal to the hanging point, wherein the second electric signal comprises a plurality of electric signals for controlling the hanging point in a short time, and acquiring hanging point execution information fed back by the weapon system universal signal checking equipment;
and S4, judging the hanging point information and the hanging point execution information, and determining whether an input and output line of the weapon system is abnormal.
The method comprises the steps that the on-board weapon control assembly executes the steps, as shown in fig. 1, the on-board weapon control assembly receives instruction excitation and hard wire excitation signals, enters a maintenance and inspection flow, gives out operation prompts to be displayed on a cabin display, an operator operates a weapon control switch according to the prompts, the on-board weapon control assembly collects the control switch state, sends the collection result to the cabin display to be displayed, and then the weapon control assembly gives out the next operation prompt to sequentially realize inspection of all weapon system input switch signals; after the input switch signal of the weapon system is checked, the on-board weapon control component automatically enters the checking of the general signal of the weapon system. Connecting weapon system general signal checking equipment at the weapon interface end, giving out signal excitation to the weapon interface end by the on-board weapon control component, carrying out signal acquisition by the weapon system general signal checking equipment, and sending the acquisition result to the on-board weapon control component to realize the checking of weapon system weapon interface end general signal; after the on-board weapon control component enters a maintenance and inspection state, the system simultaneously sends out weapon maintenance and inspection instructions to other crosslinking systems, other systems send high-bandwidth signals to a weapon system circuit, a weapon interface end is connected with weapon system general signal inspection equipment, the high-bandwidth signals are collected, and the collection result is sent to the on-board weapon control component, so that the inspection of the high-bandwidth signals at the weapon interface end is realized. And after integrating the acquisition results of the hanging point end signals, the weapon control assembly sends the acquisition results to a display in the cabin for displaying.
The specific inspection flow is as follows:
a) The on-board weapon control assembly firstly collects instruction excitation given by an operator in the cabin, and enters a maintenance and inspection flow after the instruction excitation and the hard wire excitation given by the on-board weapon ground preparation device are met.
b) The onboard weapon control component sends an operation prompt of a weapon control switch in the cockpit to the display, awaiting acquisition of the switch state.
c) The on-board weapon control component judges the input switching value, wherein the selection position of the emergency throwing knob is 1, the unselected position is 0, the judgment result is correct, the acquisition result of other switching values is judged to be correct from 0 to 1, and the on-board weapon control component judges the detection result and then sends the detection result to the display in the cabin for displaying.
d) After the input switch signal of the weapon system is checked, the on-board weapon control component automatically enters the checking of the general signal of the weapon system.
e) The on-board weapon control assembly supplies a first electric signal to the hanging points which are in interlocking, the first electric signal is a first direct current, and after receiving the power supply of the first direct current, the weapon system general signal checking equipment reports hanger description information, a ground signal, an address signal and signal state information of the first direct current to the on-board weapon control assembly.
f) If the received suspension describes that one hanging point is not the weapon system general signal checking equipment or the identification fails, the on-board weapon control component ends the maintenance checking process. If the identification is the general signal inspection equipment of the weapon system, the on-board weapon control component judges the acquisition result, the on-board weapon control component records the inspection result, and the inspection result is uniformly reported after all the signals are inspected.
Subsequently, the onboard weapon control component supplies a second electrical signal to the hanging point where the interlock exists, comprising the following steps g-n.
g) The on-board weapon control component supplies direct current 2 to a hanging point of the weapon system general signal checking equipment, and the weapon system general signal checking equipment reports a DC2 state to the on-board weapon control component after 2s withdrawal.
h) The on-board weapon control component judges the checking result, the DC2 state is changed from 0 to 1 to 0, the judging result is correct, otherwise, the on-board weapon control component records the checking result, and the checking result is uniformly reported after all signals are checked.
i) The on-board weapon control component supplies the allowable power to the hanging point of the weapon system general signal checking equipment, and the weapon system general signal checking equipment reports the allowable state to the on-board weapon control component after 2s of withdrawal.
j) The on-board weapon control component judges the checking result, the throwing permission state is changed from 0 to 1 to 0, the judging result is correct, otherwise, the on-board weapon control component records the checking result, and the checking result is uniformly reported after all signals are checked.
k) The on-board weapon control component supplies normal throwing and discharging to a hanging point of the weapon system general signal checking equipment, and the weapon system general signal checking equipment reports a normal throwing state to the on-board weapon control component after 2s withdrawal.
And l) judging the checking result by the on-board weapon control component, wherein the normal putting state is changed from 0 to 1 to 0, judging the result is correct, otherwise, recording the checking result by the on-board weapon control component, and reporting the checking result uniformly after all signal checking is finished.
m) the on-board weapon control component supplies 115V of alternating current to a hanging point existing in the weapon system general signal checking equipment, and the weapon system general signal checking equipment reports 115V of electric state to the on-board weapon control component after 2s of withdrawal.
n) the on-board weapon control component judges the checking result, the alternating current 115V state is changed from 0 to 1 to 0, the judging result is correct, otherwise, the on-board weapon control component records the checking result, and the checking result is uniformly reported after all signals are checked.
o) after the on-board weapon control component enters a maintenance inspection state, the system simultaneously sends out weapon maintenance inspection instruction excitation to other crosslinking systems. Other crosslinking systems send high bandwidth signals to weapon system general purpose signal checking equipment.
p) the weapon system general signal checking equipment interprets the high bandwidth signal and reports the high bandwidth signal state of the weapon control component on the aircraft.
q) after the maintenance inspection is finished, the on-board weapon control component reports the maintenance inspection result of each weapon hanging point, and the on-board weapon control component displays the inspection completion condition of each weapon hanging point in turn, and if faults exist, the on-board weapon control component can inquire on the display health picture.
By adopting the checking method, the input and output signals of all weapon system can be checked, an operator only needs to switch on or off related weapon control switches in the cabin according to the operation prompt on the display, the checking of other signals is finished by the automatic control of the system, and after the checking is finished, the operator can check the checking result on the display in the cabin, if fault information exists, the checking can be checked through the display.
The application also provides an electronic device comprising a memory, a processor and a computer program stored in the memory and capable of running on the processor, the processor implementing the general weapon system input output line inspection method as described above when executing the computer program.
The application also provides a computer readable storage medium, wherein the computer readable storage medium stores a computer program, and the computer program can realize the general weapon system input/output line checking method when being executed by a processor.
Fig. 2 is an exemplary block diagram of an electronic device capable of being provided in accordance with one embodiment of the 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 the 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 the computer-executable instructions, may implement the unmanned aerial vehicle autonomous tracking 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 the executable program code stored in memory 504 to perform the general purpose weapon system input output line inspection method of the above embodiments.
In one typical configuration, a computing device includes one or more processors (CPUs), input/output interfaces, network interfaces, and memory.
The memory may include volatile memory in a computer-readable medium, random Access Memory (RAM) and/or nonvolatile memory, such as Read Only Memory (ROM) or flash memory (flash RAM). Memory is an example of computer-readable media.
Computer-readable media include both permanent and non-permanent, removable and non-removable media, and the media may be implemented in any method or technology for storage of information. The information may be computer readable instructions, data structures, modules of a program, or other data. Examples of storage media for a computer 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 disk storage or other magnetic storage devices, or any other non-transmission medium, which can be used to store information that can be accessed by a computing device.
It will be appreciated by those skilled in the art that 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 is evident that the word "comprising" does not exclude other elements or steps. A plurality of units, modules or means recited in the apparatus claims can also be implemented by means of software or hardware by means of one unit or total means. The terms first, second, etc. are used to identify names, and not any particular order.
The flowcharts 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 shown 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 referred to in this embodiment may be a central processing unit (Central Processing Unit, CPU), or other general purpose processor, digital signal processor (Digital Signal Processor, DSP), application specific integrated circuit (Application Specific Integrated Circuit, ASIC), off-the-shelf programmable gate array (Field-Programmable Gate Array, FPGA) or other programmable logic device, discrete gate or transistor logic device, discrete hardware components, or the like. 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 perform various functions of the apparatus/terminal device by executing or executing the computer programs and/or modules stored in the memory, and 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 (such as a sound playing function, an image playing function, etc.) required for at least one function, and the like; the storage data area may store data (such as audio data, phonebook, etc.) created according to the use of the handset, etc. In addition, the memory may include high-speed random access memory, and may also include non-volatile memory, such as a hard disk, memory, plug-in hard disk, smart Media Card (SMC), secure Digital (SD) Card, flash Card (Flash Card), at least one disk storage device, flash memory device, or other volatile solid-state storage device.
In this embodiment, the modules/units of the apparatus/terminal device integration may be stored in a computer readable storage medium if implemented in the form of software functional units and sold or used as a separate product. Based on such understanding, the present application may implement all or part of the flow of the method of the above embodiment, or may be implemented by a computer program to instruct related hardware, where the computer program may be stored in a computer readable storage medium, and when the computer program is executed by a processor, the steps of each method embodiment described above may be implemented. Wherein the computer program comprises computer program code, which may be in the form of source code, object code, executable files or in some intermediate form, etc. The computer readable medium may include: any entity or device capable of carrying computer program code, a recording medium, a U disk, a removable hard disk, a magnetic disk, an optical disk, a computer Memory, a Read-Only Memory (ROM), a random access Memory (RAM, random Access Memory), an electrical carrier signal, a telecommunications signal, a software distribution medium, and so forth.
It should be noted that the content of the computer readable medium can be appropriately increased or decreased according to the requirements of the legislation and the practice of the patent in the jurisdiction. While the application has been described in terms of preferred embodiments, it is not intended to limit the application thereto, and any person skilled in the art can make variations and modifications without departing from the spirit and scope of the present application, and therefore the scope of the application is to be determined from the appended claims.
While the application has been described in detail in the foregoing general description and with reference to specific embodiments thereof, it will be apparent to one skilled in the art that modifications and improvements can be made thereto. Accordingly, such modifications or improvements may be made without departing from the spirit of the application and are intended to be within the scope of the application as claimed.
Claims (9)
1. A method for checking input/output lines of a general weapon system, comprising:
step S1, sending an operation prompt of a weapon control switch in a cabin to a display, and collecting input switching value of the display end;
step S2, after receiving input switching value of a display end, supplying a first electric signal to a hanging point associated with weapon system general signal checking equipment, wherein the first electric signal is an electric signal enabling the hanging point to be in a standby state, and acquiring hanging point information fed back by the weapon system general signal checking equipment;
step S3, continuously supplying a second electric signal to the hanging point, wherein the second electric signal comprises a plurality of electric signals for controlling the hanging point in a short time, and acquiring hanging point execution information fed back by the weapon system universal signal checking equipment;
s4, judging the hanging point information and the hanging point execution information, and determining whether an input and output line of the weapon system is abnormal or not;
when executing step S2 and step S3, the method also comprises the step of sending a control instruction to a crosslinking system for controlling the crosslinking system to send signal excitation to the weapon system general signal checking equipment.
2. The method of claim 1, further comprising, prior to step S1, obtaining command stimuli from a display and hard wire stimuli from an on-board weapon floor preparation device, and determining that both are valid signals.
3. The method of checking input/output lines of a general weapon system according to claim 1, wherein in step S2, the first electric signal is a first direct current of a set voltage.
4. The general weapon system input output line inspection method of claim 1, wherein in step S2, the obtained hanging point information includes hanging object description information, ground signal, address signal of the hanging point, and signal state information of the first electrical signal.
5. The method of checking input/output lines of a general weapon system according to claim 1, wherein in step S3, the second electrical signal comprises: a second direct current of set voltage, an electrical signal for allowing the delivery, an electrical signal for the delivery, and a 115V alternating current electrical signal.
6. The general weapon system input output line inspection method according to claim 1, wherein in step S3, the set short time is 2S.
7. The method for checking input/output lines of a general weapon system according to claim 1, further comprising sending the detection result to a display end for display after step S4.
8. An electronic device comprising a memory, a processor and a computer program stored in the memory and capable of running on the processor, the processor implementing the universal weapon system input output line inspection method according to any one of claims 1 to 7 when executing the computer program.
9. A computer readable storage medium storing a computer program which, when executed by a processor, is capable of implementing a general weapon system input output line inspection method according to any one of claims 1 to 7.
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| CN202110904688.6A CN113721090B (en) | 2021-08-07 | 2021-08-07 | Input/output circuit inspection method for universal weapon system |
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| CN202110904688.6A CN113721090B (en) | 2021-08-07 | 2021-08-07 | Input/output circuit inspection method for universal weapon system |
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