CN116149298A - Detection system and method of aircraft weapon launch control system based on simulation - Google Patents
Detection system and method of aircraft weapon launch control system based on simulation Download PDFInfo
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- CN116149298A CN116149298A CN202310108846.6A CN202310108846A CN116149298A CN 116149298 A CN116149298 A CN 116149298A CN 202310108846 A CN202310108846 A CN 202310108846A CN 116149298 A CN116149298 A CN 116149298A
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- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B23/00—Testing or monitoring of control systems or parts thereof
- G05B23/02—Electric testing or monitoring
- G05B23/0205—Electric testing or monitoring by means of a monitoring system capable of detecting and responding to faults
- G05B23/0218—Electric testing or monitoring by means of a monitoring system capable of detecting and responding to faults characterised by the fault detection method dealing with either existing or incipient faults
- G05B23/0221—Preprocessing measurements, e.g. data collection rate adjustment; Standardization of measurements; Time series or signal analysis, e.g. frequency analysis or wavelets; Trustworthiness of measurements; Indexes therefor; Measurements using easily measured parameters to estimate parameters difficult to measure; Virtual sensor creation; De-noising; Sensor fusion; Unconventional preprocessing inherently present in specific fault detection methods like PCA-based methods
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P90/00—Enabling technologies with a potential contribution to greenhouse gas [GHG] emissions mitigation
- Y02P90/02—Total factory control, e.g. smart factories, flexible manufacturing systems [FMS] or integrated manufacturing systems [IMS]
Abstract
The invention relates to the technical field of avionics, in particular to a detection system and a detection method of an aircraft weapon launching and controlling system based on simulation, wherein the system comprises at least one weapon simulation device which is arranged on an aircraft bullet frame and connected with the aircraft weapon launching and controlling system and is used for simulating the real weapon function; the signal processing and controlling device is used for converting the state information of the aircraft weapon launching and controlling system and the weapon simulating device into wireless radio frequency signals; and the display control terminal is used for displaying state information and test instructions of the aircraft weapon launching and control system and the weapon simulation device, and a measurement and control module used for detecting the ground state of the aircraft weapon launching and control system is arranged in the display control terminal. The detection system and the method of the aircraft weapon launching and controlling system can realize complete detection of the aircraft weapon launching and controlling system through wireless signal transmission, realize rapid detection, reduce cost and work around the clock.
Description
Technical Field
The invention relates to the technical field of avionics, in particular to a detection system and a detection method of an aircraft weapon launch control system.
Background
Regarding a detection method of an aircraft weapon launch and control system, the current detection method usually uses a carrier vehicle to carry a weapon beside an aircraft, interconnects the weapon system and the aircraft through a cable, sends a test instruction to the aircraft launch and control system through a ground or on-board command control center, and sends the launch and control instruction to the weapon system after the command is analyzed by the launch and control system, and the weapon system returns test state information to the launch and control system, so that whether the launch and control function of the aircraft launch and control system is normal is verified. The current detection method mainly has the following defects:
1) The weapon is easy to damage due to the influence of vibration, impact and the like in the transportation process, if the weapon is damaged, the weapon is abnormal when being communicated with the aircraft weapon launching and control system, and the fault of the aircraft weapon launching and control system or the fault of the weapon itself cannot be rapidly positioned;
2) When the aircraft launching control system detects weapons, a large number of special test cables are needed, and the required cost is high. In addition, when the number of the weapons mounted on the aircraft is large, the weapons are connected to the aircraft, and the weapons and the aircraft are separated after detection, so that a lot of manpower and time are consumed, and the detection efficiency is low;
3) When encountering severe weather, the operation is inconvenient.
Along with the development of informatization and intelligence of weapon equipment, higher requirements are also put forward on a detection method. The traditional ground detection method of the aircraft weapon system can not meet the requirements of rapidness, high efficiency and convenience, and especially the defects are more prominent in the state of war.
Disclosure of Invention
The invention aims to provide a detection system of an aircraft weapon launch control system based on simulation, which solves the technical problems;
the invention also aims to provide a detection method of the aircraft weapon launch and control system based on the simulation, which solves the technical problems.
The technical problems solved by the invention can be realized by adopting the following technical scheme:
a detection system of an aircraft weapon launching and control system based on simulation comprises,
the weapon simulation device is arranged on the aircraft bullet frame and connected with the aircraft weapon launch control system and used for simulating the real weapon function, and the weapon simulation device outputs the state information of the aircraft weapon launch control system and the weapon simulation device based on the test instruction;
the signal processing and controlling device is connected with the weapon simulating device, receives and analyzes the downloaded data of the weapon simulating device through a wireless signal and records the downloaded data, and is used for converting the state information of the aircraft weapon initiating and controlling system and the weapon simulating device into a wireless radio frequency signal;
the display control terminal is connected with the signal processing and control device and used for receiving the wireless radio frequency signals output by the signal processing and control device, outputting the test instruction to the weapon simulation device through the signal processing and control device, displaying the state information of the aircraft weapon launching and control system and the weapon simulation device and the test instruction, and arranging a measurement and control module used for detecting the ground state of the aircraft weapon launching and control system in the display control terminal.
Preferably, the weapon simulator, the signal processing and controlling device and the display and control terminal are connected through wireless signals.
Preferably, the weapon simulator is provided with an aviation socket for plugging an aircraft bullet frame, the weapon simulator is internally provided with,
the aviation plug signal switching module is connected with the aviation socket;
the signal processing module is connected with the aviation plug signal switching module;
the first wireless communication module is connected with the signal processing module;
and the interface module is arranged on the side wall of the weapon simulation device and is connected with the signal processing module.
Preferably, a main processing module and a wireless data transmission module connected with the main processing module are arranged in the signal processing and control device.
Preferably, the display control terminal is provided with a display screen, the display control terminal is internally provided with a display screen,
the display screen is connected with the computer main board, and the measurement and control module is arranged in the computer main board;
the power module is connected with the computer main board;
the battery pack is connected with the power supply module;
the second wireless communication module is connected with the computer main board;
and a heat dissipation sleeve for dissipating heat is further arranged in the display control terminal.
Preferably, the measurement and control module outputs the measurement instruction and the receiving state signal to the aircraft weapon launching and control system and the weapon simulator within a certain distance through wireless signals.
Preferably, the downloaded data of the weapon simulator comprises state information of the weapon simulator and state information of the aircraft weapon firing system.
Preferably, the measurement and control module is provided with at least a log management unit for managing test logs of the detection system of the aircraft weapon control system, a system setting unit for setting the detection system of the aircraft weapon control system, a weapon simulator test unit for transmitting test instructions of the weapon simulator, a weapon control system test unit for transmitting test instructions of the aircraft weapon control system, and a health management unit for checking the health of equipment in the detection system of the aircraft weapon control system.
A detection method of an aircraft weapon launching and control system based on simulation is applied to the detection system of the aircraft weapon launching and control system, and comprises the following steps,
step S1, connecting the weapon simulation device to the aircraft frame based on weapon type;
step S2, the display control terminal sends a test instruction to the weapon simulator through the signal processing and control device, the weapon simulator analyzes and transmits the test instruction to the aircraft weapon control system, the weapon simulator and the aircraft weapon control system start the test, and state information of the aircraft weapon control system and the weapon simulator after the test instruction is processed is stored;
step S3, the signal processing and controlling device acquires the state information of the aircraft weapon launching and controlling system and the weapon simulating device through wireless signals, converts the state information of the aircraft weapon launching and controlling system and the weapon simulating device into wireless radio frequency signals and transmits the wireless radio frequency signals to the display and control terminal, and the display and control terminal displays the state information of the aircraft weapon launching and controlling system and the weapon simulating device and the test instruction.
Preferably, in step S3, the wireless data transmission module in the signal processing and controlling device reads the state information of the aircraft weapon trigger system and the weapon simulator stored locally in the weapon simulator by polling.
The invention has the beneficial effects that: by adopting the technical scheme, the detection system and the method for the aircraft weapon launching and controlling system can realize complete detection of the aircraft weapon launching and controlling system through wireless signal transmission, realize rapid detection, reduce cost and work around the clock.
Drawings
FIG. 1 is a block diagram of a detection system for an aircraft weapon-issuing system according to an embodiment of the present invention;
FIG. 2 is a schematic diagram of a measurement and control module according to an embodiment of the present invention;
FIG. 3 is a schematic diagram illustrating steps of a method for detecting a weapon control system of an aircraft in accordance with an embodiment of the present invention;
fig. 4 is a flowchart of a detection method according to a first embodiment of the present invention.
Detailed Description
The following description of the embodiments of the present invention will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present invention, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the invention without making any inventive effort, are intended to be within the scope of the invention.
It should be noted that, without conflict, the embodiments of the present invention and features of the embodiments may be combined with each other.
The invention is further described below with reference to the drawings and specific examples, which are not intended to be limiting.
A detection system of an aircraft weapon trigger system based on simulation, as shown in fig. 1 and 2, comprises,
at least one weapon simulator 1, which is arranged on the aircraft bullet rack 4 and is connected with an aircraft weapon launching and controlling system for simulating the real weapon function, wherein the weapon simulator 1 outputs the state information of the aircraft weapon launching and controlling system and the weapon simulator 1 based on the test instruction;
the signal processing and controlling device 2 is connected with the weapon simulating device 1, receives and analyzes the downloaded data of the weapon simulating device 1 through a wireless signal and records the downloaded data, and is used for converting the state information of the aircraft weapon initiating and controlling system and the weapon simulating device 1 into a wireless radio frequency signal;
the display control terminal 3 is connected with the signal processing and control device 2, receives the wireless radio frequency signal output by the signal processing and control device 2, outputs a test instruction to the weapon simulation device 1 through the signal processing and control device 2, and the display control terminal 3 is used for displaying state information and the test instruction of the aircraft weapon launching and control system and the weapon simulation device 1, and a measurement and control module 5 used for detecting the ground state of the aircraft weapon launching and control system is arranged in the display control terminal 3.
Specifically, the electric interface of the weapon simulation device 1 is completely consistent with the real weapon interface, so that the real weapon function can be simulated, the device can be directly inserted into the interface of the aircraft bullet frame 4, the device is small and portable, the operation is simple and convenient, the detection efficiency is high, and the defects of large weight, more cables, complex operation and lower detection efficiency of the real weapon in the traditional detection method are overcome;
the invention introduces the special wireless communication technology into the detection field of weapon launch control system, can realize remote wireless detection, is not affected by weather, can work around the clock, and overcomes the problem that the traditional detection method is easy to be restricted by weather; furthermore, the components of each unit device required by the invention are selected to be 100% domestic, the software and the hardware are completely and independently controllable, each device adopts a modularized design, and the device can be suitable for detecting different types of weapon equipment by replacing an internal module, has good expansibility, can greatly reduce the detection cost and can rapidly locate whether the device is a fault of an aircraft weapon launch control system or a weapon self fault.
In a preferred embodiment, the weapon simulator 1, the signal processing and control device 2 and the display and control terminal 3 are connected by wireless signals;
specifically, the weapon simulation device 1, the signal processing and controlling device 2 and the display and control terminal 3 provided by the invention are transmitted through wireless signals, a physical cable is not needed, the measurement and control module 5 is operated on the display and control terminal 3, the complete detection of the ground state of the aircraft weapon launching and control system within a certain distance (within 200 meters in the embodiment) can be realized, the detection system can realize remote detection and is not affected by climate, and the defects of heavy structure, high consumption of needed cables, inconvenient operation, high cost, great influence by climate and the like of the traditional detection device are overcome.
In a preferred embodiment, the side wall of the weapon simulator 1 is provided with an aviation socket for plugging in an aircraft spring frame 4, the weapon simulator 1 is internally provided with,
the aviation plug signal switching module is connected with the aviation socket;
the signal processing module is connected with the aviation plug signal switching module;
the first wireless communication module is connected with the signal processing module;
the interface module is arranged on one side wall of the weapon simulation device 1, which is far away from the aviation socket, and is connected with the signal processing module.
Specifically, the structural dimensions outside the weapon simulator 1 are 89mm 46mm, and the weapon simulator is composed of a J599 sequence aviation socket, an aviation plug signal switching module, a signal processing module, a wireless communication module, an interface module and a structural cavity. The components of each module in the weapon simulation device 1 are selected to realize 100% domestic, wherein the signal processing module is a core module, the processor is selected to be FMQL10S400 of the complex denier microelectronics, and an embedded Linux operating system is operated on the complex denier microelectronics.
Specifically, the weapon simulator 1 complies with the GJB1188A IIA specification on the external electrical interface signal, the weapon simulator 1 is directly inserted into the interface of the aircraft frame 4 through the J599 sequence aviation socket, and communicates with the signal processing and controlling device 2 through a wireless network, so as to transmit the state information of the aircraft weapon launching and controlling system and the state information thereof to the signal processing and controlling device 2, and simultaneously, receive the detection instruction from the display and controlling terminal 3 through the wireless network.
In a preferred embodiment, the signal processing and controlling device 2 is provided with a main processing module and a wireless data transmission module connected with the main processing module.
Specifically, the structural dimensions of the signal processing and control device 2 are 302mm (width) x281mm (depth) x80mm (thickness), which consists of a main processing module, a wireless data transmission module, a base plate and a structural cavity. The components of each module in the signal processing and controlling device 2 are selected to realize 100% domestic production, the main processing module is a core module of the signal processing and controlling device, the processor is selected to be Loongson central area LS2K1000, the FPGA is selected to be double denier microelectronic FMK50T4, and the processor runs a domestic antenna and vein second-generation real-time operating system, so that on one hand, the data are downloaded and recorded by the weapon simulating device 1, and meanwhile, the state information of the aircraft weapon launching and controlling system and the weapon simulating device 1 is converted into wireless radio frequency signals and transmitted to the display and control terminal 3, and on the other hand, the detection instruction transmitted by the display and control terminal 3 is received and transmitted to the weapon simulating device 1 through wireless transmission, and detection is started.
Further, the wireless data transmission module reads state information of the aircraft weapon trigger system and the weapon simulator 1 stored in the local area of the weapon simulator 1 in a polling mode; in this embodiment, 12 weapon simulator units 1 connected to the aircraft are provided, and each weapon simulator unit 1 is provided with a wireless communication node.
In a preferred embodiment, the display control terminal 3 is provided with a display screen, the display control terminal 3 is internally provided with,
the display screen is connected with the computer main board, and a measurement and control module 5 is arranged in the computer main board;
the power module is connected with the computer main board;
the battery pack is connected with the power supply module;
the second wireless communication module is connected with the computer main board;
and a heat dissipation sleeve for heat dissipation is further arranged in the display control terminal 3.
Specifically, the external structural dimension of the display control terminal 3 is 265mm (width) x165mm (depth) x35mm (thickness), the display control terminal is composed of components such as a computer main board, a power module, a battery pack, a wireless communication module, a liquid crystal display, a heat dissipation sleeve and the like, selected components of the components are 100% domestic, wherein the computer main board is used as a core component, a domestic Loongson 3A4000 processor is selected as an internal processor, an operating system is a winning kylin operating system, and based on the operating system, a self-grinding measurement and control module 5 is operated to display state information and output detection instructions of the aircraft weapon control system and the weapon simulation device 1.
In a preferred embodiment, the measurement and control module 5 outputs measurement instructions and receives status signals via wireless signals to the aircraft weapon control system and weapon simulator 1 over a distance.
In a preferred embodiment, the downloaded data of weapon simulator 1 includes state information of weapon simulator 1 and state information of an aircraft weapon control system.
In a preferred embodiment, referring further to fig. 2, the measurement and control module 5 is provided with a log management unit 51 for managing the detection system of the aircraft weapon control system, a system setting unit 52 for setting the detection system of the aircraft weapon control system, a weapon simulator testing unit 53 for sending test instructions of the weapon simulator 1, a weapon control system testing unit 54 for sending test instructions of the aircraft weapon control system, and a health management unit 55 for checking the health of equipment in the detection system of the aircraft weapon control system.
Specifically, the measurement and control module 5 runs on the display control terminal 3, is developed by adopting Qt5, and the display screen can support multi-point touch operation, can respond to user operation by the internal touch module of software, and is convenient for users to use.
A detection method of an aircraft weapon trigger system based on simulation, which is applied to the detection system of the aircraft weapon trigger system in any one embodiment, as shown in fig. 3, and comprises,
step S1, connecting the weapon simulator 1 to the aircraft frame 4 based on the weapon type;
step S2, the display control terminal 3 sends a test instruction to the weapon simulator 1 through the signal processing and control device 2, the weapon simulator 1 analyzes the test instruction and transmits the test instruction to the aircraft weapon launching and controlling system, the weapon simulator 1 and the aircraft weapon launching and controlling system start the test, and state information of the aircraft weapon launching and controlling system and the weapon simulator 1 after the test instruction is processed is stored;
step S3, the signal processing and controlling device 2 acquires the state information of the aircraft weapon launching and controlling system and the weapon simulating device 1 through wireless signals, converts the state information of the aircraft weapon launching and controlling system and the weapon simulating device 1 into wireless radio frequency signals, transmits the wireless radio frequency signals to the display and control terminal 3, and the display and control terminal 3 displays the state information and the test instruction of the aircraft weapon launching and controlling system and the weapon simulating device 1.
In a preferred embodiment, in step S3, the wireless data transmission module in the signal processing and control device 2 reads the state information of the weapon simulator 1 stored in the local aircraft weapon control system and weapon simulator 1 by polling; specifically, in the present embodiment, 12 weapon simulator apparatuses 1 connected to an aircraft are provided in total, and each weapon simulator 1 is provided with a wireless communication node.
In a first embodiment of the present invention,
in the detection method provided by the invention, the weapon simulator 1, the signal processing and controlling device 2 and the display and control terminal 3 are in wireless communication. The weapon simulator 1 is inserted on the aircraft bullet rack 4, the signal processing and controlling device 2 can be placed at any point within 200m distance from the aircraft, and the distance between the display and control terminal 3 and the signal processing and controlling device 2 is kept within 200 m. As shown in fig. 4, the detection flow is as follows:
step 1, selecting a corresponding bullet type according to the weapon type, and butting the weapon simulation device 1 with a plug of an aircraft bullet rack;
step 2, judging whether the aircraft weapon issuing control system issues an instruction to the weapon simulation device 1 according to the test instruction, if yes, executing step 3, otherwise, continuing to wait for the aircraft weapon issuing control system to issue the instruction;
step 3, after receiving and analyzing the instruction, the weapon simulator 1 processes the instruction and transmits corresponding information back to the aircraft weapon launching and controlling system, and at the same time, the aircraft weapon launching and controlling system instruction and the processed information are recorded in the local flash;
step 4, waiting for the wireless data transmission device of the signal processing and controlling device 2 to poll the node;
and 5, transmitting the information in the flash to the signal processing and control device 2 and recording the information in the flash on a hard disk, and simultaneously, transmitting the information to the portable display and control terminal 3 through a wireless network by the signal processing and control device 2 for displaying the state.
The foregoing description is only illustrative of the preferred embodiments of the present invention and is not to be construed as limiting the scope of the invention, and it will be appreciated by those skilled in the art that equivalent substitutions and obvious variations may be made using the description and illustrations of the present invention, and are intended to be included within the scope of the present invention.
Claims (10)
1. A detection system of an aircraft weapon launch control system based on simulation is characterized by comprising,
the weapon simulation device is arranged on the aircraft bullet frame and connected with the aircraft weapon launch control system and used for simulating the real weapon function, and the weapon simulation device outputs the state information of the aircraft weapon launch control system and the weapon simulation device based on the test instruction;
the signal processing and controlling device is connected with the weapon simulating device, receives and analyzes the downloaded data of the weapon simulating device through a wireless signal and records the downloaded data, and is used for converting the state information of the aircraft weapon initiating and controlling system and the weapon simulating device into a wireless radio frequency signal;
the display control terminal is connected with the signal processing and control device and used for receiving the wireless radio frequency signals output by the signal processing and control device, outputting the test instruction to the weapon simulation device through the signal processing and control device, displaying the state information of the aircraft weapon launching and control system and the weapon simulation device and the test instruction, and arranging a measurement and control module used for detecting the ground state of the aircraft weapon launching and control system in the display control terminal.
2. The system for detecting an aircraft weapon-initiating and controlling system according to claim 1, wherein the weapon simulator, the signal processing and controlling device and the display and control terminal are connected by wireless signals.
3. The system for detecting and controlling the weapon of an aircraft according to claim 1, wherein the weapon simulator is provided with an aviation socket for plugging in an aircraft frame, wherein the weapon simulator is provided with a plurality of sensors,
the aviation plug signal switching module is connected with the aviation socket;
the signal processing module is connected with the aviation plug signal switching module;
the first wireless communication module is connected with the signal processing module;
and the interface module is arranged on the side wall of the weapon simulation device and is connected with the signal processing module.
4. The system for detecting and controlling the weapon-issuing system according to claim 1, wherein the signal processing and controlling device is internally provided with a main processing module and a wireless data transmission module connected with the main processing module.
5. The detecting system of aircraft weapon triggering system according to claim 1, wherein the display and controlling terminal is provided with a display screen, the display and controlling terminal is internally provided with,
the display screen is connected with the computer main board, and the measurement and control module is arranged in the computer main board;
the power module is connected with the computer main board;
the battery pack is connected with the power supply module;
the second wireless communication module is connected with the computer main board;
and a heat dissipation sleeve for dissipating heat is further arranged in the display control terminal.
6. The aircraft weapon control system of claim 1, wherein the measurement and control module outputs the test command and the receive status signal to the aircraft weapon control system and the weapon simulator over a distance via wireless signals.
7. The aircraft weapon fire system detection system of claim 1, wherein the downloaded data of the weapon simulator includes status information of the weapon simulator and status information of the aircraft weapon fire system.
8. The system for detecting a weapon controlled system of an aircraft according to claim 1, wherein the measurement and control module is provided with at least a log management unit for managing test logs of the detection system of the aircraft weapon controlled system, a system setting unit for setting the detection system of the aircraft weapon controlled system, a weapon simulator testing unit for sending test instructions of the weapon simulator, a weapon controlled system testing unit for sending test instructions of the aircraft weapon controlled system and a health management unit for checking the health of equipment within the detection system of the aircraft weapon controlled system.
9. An aircraft weapon trigger system detection method based on simulation, which is applied to the aircraft weapon trigger system detection system according to any one of claims 1 to 8, and is characterized by comprising,
step S1, connecting the weapon simulation device to the aircraft frame based on weapon type;
step S2, the display control terminal sends a test instruction to the weapon simulator through the signal processing and control device, the weapon simulator analyzes and transmits the test instruction to the aircraft weapon control system, the weapon simulator and the aircraft weapon control system start the test, and state information of the aircraft weapon control system and the weapon simulator after the test instruction is processed is stored;
step S3, the signal processing and controlling device acquires the state information of the aircraft weapon launching and controlling system and the weapon simulating device through wireless signals, converts the state information of the aircraft weapon launching and controlling system and the weapon simulating device into wireless radio frequency signals and transmits the wireless radio frequency signals to the display and control terminal, and the display and control terminal displays the state information of the aircraft weapon launching and controlling system and the weapon simulating device and the test instruction.
10. The system according to claim 9, wherein in step S3, the wireless data transmission module in the signal processing and controlling device reads the state information of the aircraft weapon triggering system and the weapon simulator stored locally by the weapon simulator in a polling manner.
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| CN202310108846.6A CN116149298A (en) | 2023-02-10 | 2023-02-10 | Detection system and method of aircraft weapon launch control system based on simulation |
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| CN202310108846.6A CN116149298A (en) | 2023-02-10 | 2023-02-10 | Detection system and method of aircraft weapon launch control system based on simulation |
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