KR102051105B1 - Movable test equipment for Air Combat Maneuvering Instrumentation-POD integrated testing, Method for controlling the same - Google Patents

Abstract

The present invention relates to a mobile inspection equipment technology, and more specifically, ACMI-POD integration inspection (Air Combat Maneuvering Instrumentation-POD integrated) that can be mounted and operated in a real-time aircraft for the integration of Live-Virtual-Constructive (LVC) integration mobile inspection equipment for testing and its control method.
According to the present invention, the operation simulation and function check of the ACMI-POD can be performed on the ground even without installing the ACMI-POD (Air Combat Maneuvering Instrumentation-POD) directly on the aircraft.

Description

Movable test equipment for Air Combat Maneuvering Instrumentation-POD integrated testing, Method for controlling the same

The present invention relates to a mobile inspection equipment technology, and more specifically, an air combat maneuver measurement pod (Air Combat Maneuvering Instrumentation) that can be mounted and operated in a real-class aircraft for live-virtual-constructive (LVC) integration. Mobile inspection equipment for POD integrated testing and its control method.

In addition, the present invention is the operation simulation and functional check for the air combat start measurement pod of the CTP / AIM-9 (Captive Test Pod / Air Intercept Missile-9) shape that can be mounted and operated in a real-time aircraft for LVC integration interworking The present invention relates to a mobile inspection device for controlling an integrated function between the aviation combat start measurement pod and the integrated linkage system, and a control method thereof.

The Air Combat Maneuvering Instrumentation (ACMI) system currently used by the Air Force uses a Ford in the form of an Air Intercept Missile-9 (AIM-9) missile.

Ford's built-in equipment can be used to collect aircraft's position, attitude, speed and maneuverability. In addition, the data link can be used to perform transmission and reception between ACMI-PODs mounted on other aircraft and to transmit ground relay equipment (hereinafter referred to as GRS) to review real-time demonstrations and training on the ground. By using this ACMI-POD, he mainly conducts close combat-oriented training such as Dog Fighter.

However, recent military training requires multi-tasking and joint / union training, and the Air Force requires large-scale training, such as Beyond Visual Range (BVR) engagements.

Therefore, the LVC (Live-Virtual-Constructive) integrated synthetic battlefield training environment that can be integrated with practical, virtual, and component-level training systems that can replace the limited and obsolete current operating system and reflect the combat concept of modern warfare. Technology is required.

1. Korea Registered Patent No. 10-1461486 (2014.11.07) 2. Korean Patent Publication No. 10-2016-0046554 3. Korean Patent No. 10-1050424 (2011.07.13)

The present invention has been proposed to solve the problem according to the above background, ACMI-POD (Air Combat Maneuvering Instrumentation-POD) that can be mounted and operated in a real-class aircraft for the integration of Live-Virtual-Constructive (LVC) The purpose of the present invention is to provide a mobile inspection device for ACMI-POD integrated testing and a control method thereof.

In addition, the present invention is the operation simulation and functional check for the ACMI-POD of the CTP / AIM-9 (Captive Test Pod / Air Intercept Missile-9) shape that can be mounted and operated in a practical aircraft for interlocking LVC integration, ACMI Another object is to provide a mobile inspection device and a control method thereof for the integrated functional inspection between the POD and the integrated interlocking system.

In order to achieve the above-described problems, the present invention provides a CTP / AIM-9 (Captive Test Pod / Air Intercept Missile-) that can be mounted and operated in a real-time aircraft for interworking with Live-Virtual-Constructive (LVC) integration. 9) Provides mobile test equipment for operational simulation and function check of ACMI-POD (Air Combat Maneuvering Instrumentation-POD) and integrated function check between ACMI-POD and integrated linkage system.

The mobile inspection equipment,

A power supply 202 for turning on the power supply;

In order to simulate the actual flight, the aviation fighters can be simulated using the component function simulation information and the aircraft generation information of the Air Combat Maneuvering Instrumentation (POD) generated using input information input by the user. A check controller 120 for performing a condition check on the components of the measuring pod; And

And an interface box 203 providing an interface communication port between the check controller 120 and the air combat start measurement pod.

At this time, the mobile inspection equipment, the aviation combat start measurement pod is made of a plurality, an electronic switch 204 for selectively connecting a plurality of aviation combat start measurement pods with the interface box; may include a have.

In addition, the power supply 202, the inspection controller 120, the interface box 203, and the electronic switch 204, the housing 200 which is assembled in a stacking inner; may be characterized in that it comprises a.

In addition, the slot guide 240 is installed on the side of any one of the power supply 202, the inspection controller 120, the interface box 203, and the electronic switch 204 to be attached to and detached from the housing 200. It may be characterized by.

In addition, the mobile inspection equipment, covers 220-1, 220-2 fastened and assembled at both ends of the housing 200; may be characterized in that it comprises a.

In addition, the power supply 202, the inspection controller 120, the interface box 203, and the electronic switch 204 may be characterized in that the modular structure detachable in the housing 200 as a separate component.

The aviation combat start measurement pod may be at least one of a capacitive test pod (CTP) type pod and an air intercept missile-9 (AIM-9) type pod.

In addition, the inspection controller 120 simulates output of navigation information including aircraft position information and attitude information to match an interface of a GPS / INS (Global Positioning System / Inertial Navigation System) navigation device. Module 121; An aircraft simulation module 122 for simulating rocket impact point information of the aircraft; A data link simulation module 123 for simulating link information including a command and control (C2) command and other aircraft information transmitted and received between the air combat start measurement pod and the ground body; A check module for performing a self check, a check of components of the air combat start measurement pod; And an interface interworking module 125 for managing interworking of discrete signals, 1553B signals, RS-422 signals, and Ethernet signals generated by the mobile inspection equipment.

In addition, the condition check consists of a test support mode for operating and testing the air combat start measurement pod (ACMI-POD) on the ground and a check mode for checking the components of the air combat start measurement pod (ACMI-POD). It may be characterized by.

In addition, the mobile inspection equipment, the connector panel 423 is fastened to the fortune supply 202; The interface box 203; And

It may be characterized in that it comprises a; multi tab 421 is fastened to the electronic switch 204.

In addition, the portable inspection equipment may further include a display 850 for outputting the input information or status information.

On the other hand, another embodiment of the present invention, a plurality of mobile inspection equipment for the air combat start measurement pod integrated inspection described above; A plurality of air combat start measurement pods (ACMI-POD) 820-1, 820-2 connected to the mobile inspection equipment 100 for the air combat start measurement pod integrated inspection; After installing the ACMI-POD in component units, connect the ACMI-POD (or ACMI-POD in component units) to a Radio Frequency (RF) matrix so that the ACMI-POD (or ACMI-POD installed in component units) An integrated test bed 600 that simulates spatially separated from each other in the air; A management server 840 for generating and controlling a scenario according to a user input so as to simulate the track of the air combat start measurement pod in the mobile inspection equipment; After the aviation combat start measurement pod is installed as a component unit, it is connected to the RF (Radio Frequency) matrix and the integrated test bed 600 to simulate the air combat start measurement pods spatially separated from each other on the ground or in the air; It includes, the mobile inspection equipment 100 performs the state check according to the scenario through the integrated test bed 600, and generates the result information according to the execution result and transmits to the management server 840 An integrated interworking system can be provided.

On the other hand, another embodiment of the present invention provides a plurality of aero combat start measurement pods (ACMI-POD) (a) in which an integrated test bed 600 is connected to the mobile inspection equipment 100 described above ( 820-1 and 820-2; (b) generating and controlling a scenario according to a user input so that the management server 840 simulates the track of the air combat start measurement pod; (c) The air combat start measurement pod is installed in component units, connected by a Radio Frequency (RF) matrix, and the integrated test bed 600 simulates the air combat start measurement pods to be spatially separated from each other on the ground or in the air. Performing the state check according to the scenario by the mobile inspection equipment (100); And (d) generating, by the mobile inspection equipment 100, the result information according to the result of the state check, and transmitting the result information to the management server 840. It may provide a method.

On the other hand, another embodiment of the present invention can provide a computer readable storage medium storing program code for executing the control method of the integrated interlocking system described above.

 According to the present invention, even if the air combat maneuver measurement pod (ACMI-POD) is not directly mounted on the aircraft, the operation simulation and function check of the ACMI-POD can be performed on the ground.

In addition, another effect of the present invention is to utilize the mobile inspection equipment and the integrated test bed, so that the information between the virtual simulator and the component-grade mission-level combat system in the distributed environment of the ground considering the actual propagation environment is implemented. It is possible to integrate with the same aviation combat measurement pod in the same class.

1 is a block diagram of a mobile inspection equipment 100 according to an embodiment of the present invention.
FIG. 2A is an assembled perspective view of the mobile inspection assembly 110 shown in FIG. 1.
2B is a block diagram of the mobile inspection equipment 100 shown in FIG. 1.
3 is a perspective view illustrating a state in which the front cover is removed from the exterior of the housing 200 illustrated in FIG. 2.
4 is an assembled perspective view of the rear cover 220-2 shown in FIG. 2.
5 is a perspective view illustrating a state in which a rear cover is removed from an exterior of the housing 200 illustrated in FIG. 4.
FIG. 6 is a perspective view of an integrated test bed generally connected to an air combat measurement instrument pod (ACMI-POD). FIG.
FIG. 7 is a perspective view of a ground body 700 connected with the integrated test bed 600 shown in FIG. 6.
FIG. 8 is a block diagram of an integrated interworking system 800 to which the mobile inspection apparatus 100 illustrated in FIG. 1 is applied.
9 is a flow chart showing the procedure between the mobile inspection equipment and the integrated test bed according to an embodiment of the present invention.

As the invention allows for various changes and numerous embodiments, particular embodiments will be illustrated in the drawings and described in detail in the written description. However, this is not intended to limit the present invention to specific embodiments, it should be understood to include all changes, equivalents, and substitutes included in the spirit and scope of the present invention.

In describing each drawing, like reference numerals are used for like elements.

Terms such as first and second may be used to describe various components, but the components should not be limited by the terms. The terms are used only for the purpose of distinguishing one component from another.

For example, without departing from the scope of the present invention, the first component may be referred to as the second component, and similarly, the second component may also be referred to as the first component. The term “and / or” includes any combination of a plurality of related items or any item of a plurality of related items.

Unless defined otherwise, all terms used herein, including technical or scientific terms, have the same meaning as commonly understood by one of ordinary skill in the art.

Terms such as those defined in the commonly used dictionaries should be construed as having meanings consistent with the meanings in the context of the related art, and are not construed in ideal or excessively formal meanings unless expressly defined in this application. Should not.

With reference to the accompanying drawings will be described in detail the mobile inspection equipment and control method for the air Combat maneuvering instrumentation-POD integrated testing (Air Combat Maneuvering Instrumentation-POD integrated testing) according to an embodiment of the present invention.

1 is a block diagram of the mobile inspection equipment 100 according to an embodiment of the present invention. Referring to FIG. 1, the mobile inspection equipment 100 is configured in the mobile inspection assembly 110 and the mobile inspection assembly 110, and includes an air combat maneuvering instrumentation (POMI-POD). The component function simulation may be configured to include a check controller 120 for performing a state check on a component of the ACMI-POD.

The inspection controller 120 includes a GPS / INS (Global Positioning System / Inertial Navigation System) output simulation module 121, an aircraft simulation module 122, a data link simulation module 123, an inspection module 124, and an interface interworking module ( 125) and the like. GPS / INS output simulation module 121 is a simulated computer software component (CSC) that outputs navigation information (aircraft position information, attitude information) to match the interface of the GPS / INS navigation system, aircraft simulation module 122 is an aircraft Mock up rocket impact point information.

The data link simulation module 123 simulates link information transmitted and received between the ACMI-POD and the terrestrial body, such as a command and control (C2) command and other aircraft information. In addition, the inspection module 124 has a function for self-inspection, component inspection of the air combat start measurement pod (ACMI-POD). The interface interworking module 125 manages 1553B, RS-422, and Ethernet signal interworking as well as discrete signals.

In addition, terms such as "... module" described in the specification means a unit for processing at least one function or operation, which may be implemented as a combination of hardware and / or software. In hardware implementation, application specific integrated circuit (ASIC), digital signal processing (DSP), programmable logic device (PLD), field programmable gate array (FPGA), processor, check controller, micro It may be implemented in a processor, another electronic unit, or a combination thereof. In the software implementation, the module may be implemented as a module that performs the above-described function. The software may be stored in a memory unit and executed by a processor. The memory unit or processor may employ various means well known to those skilled in the art.

FIG. 2A is an assembled perspective view of the mobile inspection assembly 110 shown in FIG. 1. Referring to FIG. 2A, the movable inspection assembly 110 includes a housing 200, an electric power supply 202 inserted into the housing 200, an inspection controller 120, an interface box 203, and an electronic switch ( 204) and the like. The housing 200 may be integrally formed through a mold. Alternatively, the housing 200 may be configured by each plate and assembled by bolting.

The cloud feeder 202, the inspection controller 120, the interface box 203, the electronic switch 204, and the like have a modular structure for making parts and detaching them individually into the housing 200. In addition, the slot guide 240 may be configured to be detached from the housing 200. Of course, a slot (not shown) into which the slot guide 240 is inserted may be formed on the inner wall of the housing 200. Accordingly, the cloud feeder 202, the inspection controller 120, the interface box 203, the electronic switch 204, and the like are attached to and detached from the housing 200 by a sliding method.

In addition, the front cover 220-1 and the rear cover 220-2 are fastened and assembled at both ends of the housing 200, respectively. That is, the front cover 220-1 is assembled and fastened to the front of the housing 200, and the rear cover 220-2 is assembled and fastened to the rear of the housing 200.

The electronic switch 204 may be a KVM (Keyboard, Video Monitor, Mouse) switch or the like. The main function of the KVM switch is to control, switch, and / or manage multiple personal computers (PCs) through one keyboard, monitor, and mouse.

2B is a block diagram of the mobile inspection equipment 100 shown in FIG. 1. Referring to FIG. 2B, the power supply 202 for turning on the power supply, the airborne flight start measurement pod (ACMI-POD: Air Combat Maneuvering Instrumentation-POD) component function simulation information and aircraft generation information through the aircraft generation information A check controller 120 for performing a status check on components of the combat start measurement pod, an interface box 203 providing an interface communication port for interfacing the check controller 120 with the air combat start measurement pod, and a plurality of aeronautics And an electronic switch 204 for selectively connecting the combat start measurement pod with the interface box.

Of course, the power supply 202, the check controller 120, the interface box 203, and the electronic switch 204 shown in FIG. 2B may be configured with a microprocessor, an electronic circuit, a memory, and the like to perform a function. have. In addition, they may each have their own housing for being individualized.

3 is a perspective view illustrating a state in which the front cover is removed from the exterior of the housing 200 illustrated in FIG. 2. Referring to FIG. 3, the front cover 220-1 is removed from the housing 200, and only the rear cover 220-2 is assembled and fastened.

4 is an assembled perspective view of the rear cover 220-2 shown in FIG. 2. Referring to Figure 4, the mobile inspection equipment is a test support mode for operating and testing the air combat start measurement pod (ACMI-POD) on the ground and the check mode for checking the components of the air combat start measurement pod (ACMI-POD) Can be operated as.

In test support mode, MIL-STD-1553B, RS-422, Discrete signals, Ethernet (Ethernet) from the interface box 203 in the mobile inspection equipment 100 for interfacing with the ACMI-POD. It provides interface communication port such as signal, and simulated signals such as navigation information and armed information are transmitted to ACMI-POD.

MIL-STD-1553B, RS-422, Discrete Signal, Ethernet in interface box 203 in mobile inspection equipment 100 for interfacing with ACMI-POD in inspection mode. It provides an interface communication port, such as a signal, which allows the mobile inspection equipment to receive BIT results for components of the ACMI-POD.

To this end, a multi tap 421, a connector panel 423, and the like are configured. One end of the multi tap 421 is connected to the electronic switch 204 and the other end is connected to the air combat start measurement pod ACMI-POD. The interface box 203 is connected to the air combat start measurement pod (ACMI-POD). In addition, the connector panel 423 is connected to the air combat start measurement pod (ACMI-POD).

The multi tap 421 is a tap that performs a function of supplying power when power is required to external equipment of the mobile inspection equipment. Here, the external equipment of the mobile inspection equipment may be, for example, a laptop, a media converter and other measurement equipment.

The test pointer panel (not shown) may be integrated in the interface box 203. Accordingly, the interface box 203 directly processes signals passing through the existing test point panel, and the connector panel 423 is equipped with a connector for providing a power supply signal for pod supply to perform power supply to the pod.

The multi tab 421 and the connector panel 423 are inserted into and fastened to the rear of the housing 200, and in this state, the rear cover 220-2 is fastened and assembled to the housing 200. Of course, the multi-taps 421 and the connector panel 423 may be assembled to the housing 200 while being inserted into the rear cover 220-2.

5 is a perspective view illustrating a state in which a rear cover is removed from an exterior of the housing 200 illustrated in FIG. 4. Referring to FIG. 5, the multi-tab 421 and the connector panel 423 are assembled and fastened inside the rear side of the housing 200.

FIG. 6 is a perspective view of an integrated test bed 600 generally connected to an air combat measurement pod (ACMI-POD). Referring to FIG. 6, the integrated test bed 600 is connected to a power supply 610 for supplying power and an ACMI-POD to check the state of the mobile inspection equipment (100 in FIG. 1). And a first control computer 620 to perform monitoring and / or control of Pod components, a Pod component mounting portion 601, an RF matrix 630, and the like. The power supply 610 supplies rated power for the Pod components, and the first control computer 620 performs monitoring and / or control for the Pod components. The RF matrix 630 is a module configured with an internal RF attenuator for RF transmission and reception without an antenna.

FIG. 7 is a perspective view of a ground body 700 connected with the integrated test bed 600 shown in FIG. 6. Referring to FIG. 7, the ground body 700 is connected with the integrated test bed 600 to perform the test support mode and / or the check mode of the mobile check equipment (100 in FIG. 1) according to the scenario of the management server side. A second control computer 740 for controlling the integrated test bed 600, a ground radio station (GRS) 730, a terrestrial data link power supply 720 for supplying power to the terrestrial data link, A terrestrial data link 710 or the like. Ground relay equipment 730 is a device installed to interlock data between the Pod (POD) and the management server. Terrestrial data link 710 is a data link equipment operated on the ground to communicate with data link equipment in a floating Pod.

8 is a block diagram of an integrated ground inspection system 800 to which the mobile inspection equipment 100 shown in FIG. 1 is applied. Referring to FIG. 8, a plurality of mobile inspection equipment 100, an air combat start measurement pod (ACMI-POD) 820-1 and 820-2 connected to the mobile inspection equipment 100, and a ground body data link 710. And an integrated test bed 700 comprising a ground body 700, a power supply 610, a control computer 620, a Pod component mounting site 601, and an RF matrix 610, including ground relay equipment 730. It may be configured to include a management server 840 for generating scenarios and controlling the ground body 700 so as to simulate the track of the ACMI-POD in the mobile inspection equipment.

The integrated test bed 600 is installed in the ACMI-POD (or component units) by installing the ACMI-POD in component units, and then connecting the ACMI-POD (or ACMI-POD installed in component units) in a radio frequency (RF) matrix. It simulates that ACMI-PODs are spatially separated from each other on the ground or in the air.

The mobile inspection equipment 100 may include a display 850 for outputting input information or status information. The display 850 may be a liquid crystal display (LCD), a light emitting diode (LED) display, a plasma display panel (PDP), an organic LED (OLED) display, a touch screen, a cathode ray tube (CRT), a flexible display, or the like. have.

In addition, the inspection software 870 is installed in the mobile inspection equipment 100, and the inspection software may be installed with a PDU (Pilot Display Unit) software. In addition, the mobile inspection equipment 100 is capable of aviation combat start measurement pods 820-1, 820-2, aircraft interworking 801-1, and inspection window interworking 802-1. Aircraft linkage can be 1553B linkage, PDU linkage, armed launch, and audio playback. Inspection window interworking 802-1 may be interlocking of a navigational hat.

The air combat start measurement pods 820-1 and 820-2 are composed of a captive test pod (CTP) pod (820-1) and an air intercept missile-9 (AIM-9) pod (820-2). Of course, there may be more than two.

Captive Test Pod (CTP) Pods (820-1) include ETC (Embedded Training Computer), MPS (Main Power Supplier), DPS (Datalink Power Supplier), EGI ( Embedded GPS / INS ) D / L (Datalink) Have components. Similarly, the Air Intercept Missile-9 (AIM-9) type pod 820-2 also has components such as ETC, MPS, DPS, EGI, and D / L.

In other words, the present invention implements a live-virtual-constructive (LVC) integrated synthetic battlefield training environment technology capable of integrated interworking of real-world, virtual, component equipment and these training systems. In particular, the ACMI-POD in the form of an AIM-9, a practical training equipment, has three existing line-replaceable units (LRUs), unlike the AIM-9, which is operated by the existing air force, to improve equipment manufacturing and / or operational efficiency. The integrated remote control unit (RCU), analog digital interface unit (ADIU), and overlapped block motion compensation (OBMC) are integrated into one ETC.

That is, the AIM-9 type pod 820-2 integrates LRUs that are separately operated as a global positioning system (GPS) and an inertial measurement unit (IMU) into one GPS / INS device. In order to test this in the KO-1, the CTP (Captive Test Pod) pod 820-1 has a shape of a KO-1 aircraft external fuel tank having the same internal components as an AIM-9-shaped ACMI-POD.

Since components such as ETC, MPS, DPS, EGI, D / L, etc. are well known, further description will be omitted for a clear understanding of the present invention.

8, CTP-type pods 820-1 and AIM-9-type pods 820-2 are connected to the integrated test bed 600, 700 via wireless communication such as DL Data Link Radio Frequency (RF). . As shown in FIG. 8, the components of the air combat start measurement pod (ACMI-POD) are divided into the component sets of the air combat start measurement pod (ACMI-POD) within the integrated test bed (600,700). Formulas are connected to each other.

The set of components of each ACMI-POD is connected to each other via the RF MATRIX at the bottom of the machine, and the ACMI-PODs connected to the management server through the GRS. This connection configuration allows for the functional check of the component set of each ACMI-POD in a test environment that takes into account the actual propagation environment. In addition, the CTP / AIM-9 configuration of the ACMI-POD and RF MATRIX are also available.

The integrated test bed 600, 700 performs a test according to the test support mode and / or the check mode of the mobile inspection equipment (100 of FIG. 1) and generates the result information according to the result and transmits the result information to the management server 840. In addition, the management server creates and controls scenarios to simulate the track of ACMI-POD in mobile inspection equipment.

To this end, the management server 840 is composed of a microprocessor, a memory, a display, and the like. Of course, the management server 840 is connected with the integrated test bed 600,700 through wired communication and / or wireless communication.

In other words, two ACMI-POD components are installed in an external space, and then two mobile inspection equipment are connected with CTP-type Pods and AIM-9-type Pods, respectively, for navigation simulation. By integrating ACMI-POD components with terrestrial datalink racks, GRS simulators and integrated interlocking systems, a complete integrated interlocking inspection is possible on the ground.

9 is a flow chart showing the procedure between the mobile inspection equipment 100 and the integrated test bed 600,700 according to an embodiment of the present invention. 9, the mobile inspection equipment 100 and the integrated test beds 600 and 700 are powered on (S910 and S920). The power-on sequence may be simultaneous or may proceed with a time difference.

Thereafter, the mobile inspection equipment 100 drives the equipment test software 870 and enters the equipment control page (steps S911 and S913). In other words, as the power is turned on, the mobile inspection equipment 100 drives the equipment test software 870 and outputs a page for the equipment inspection on the display 850.

Accordingly, the user generates input information by using a mouse, a keyboard, and the like on the equipment control page, and accordingly the equipment control start command is transmitted to the integrated test bed 600, 700 (step S915).

On the other hand, the integrated test bed (600, 700) also turns on the test body as the power is turned on, and sets the attenuator gain of the RF matrix (steps S921, S923). Thereafter, according to the start command, the integrated test bed 600 or 700 starts to drive the test body, and drives the test body according to the aircraft generation information according to the external input simulation of the mobile inspection apparatus 100 (steps S917 and S927). Aircraft generation information is generated according to the A-external input simulation (ex, tester manipulation).

Accordingly, the mobile inspection equipment 100 receives the result information from the integrated test beds 600 and 700 and monitors the test specimen (step S918).

Of course, when the mobile inspection equipment 100 ends the control of the equipment, receiving the integrated test bed (600, 700) also terminates the driving of the test specimen (steps S919, S930).

In addition, the steps of a method or algorithm described in connection with the embodiments disclosed herein may be embodied in a program instruction form that can be executed by various computer means and recorded in a computer-readable medium. The computer readable medium may include program (instruction) code, data file, data structure, etc. alone or in combination.

The program (command) code recorded on the medium may be those specially designed and configured for the present invention, or may be known and available to those skilled in computer software. Examples of computer-readable recording media include magnetic media such as hard disks, floppy disks, and magnetic tapes, optical media such as CD-ROMs, DVDs, Blu-rays, etc., and ROMs and RAMs. Semiconductor memory devices specifically configured to store and execute program (command) code, such as RAM), flash memory, and the like.

Here, examples of program (instruction) code include not only machine code generated by a compiler, but also high-level language code that can be executed by a computer using an interpreter or the like. The hardware device described above may be configured to operate as one or more software modules to perform the operations of the present invention, and vice versa.

100: mobile inspection equipment
110: inspection assembly
120: check controller
202: power supply
203: interface box
204: electronic switch
200: housing
220-1: front cover
220-2: back cover

Claims (14)

A power supply 202 for turning on the power supply;
In order to simulate the actual flight, the air fighter jets can be simulated using the component function simulation information and aircraft generation information of the Air Combat Maneuvering Instrumentation (POD) generated using input information input by the user. A check controller 120 for performing a condition check on the components of the measuring pod; And
An interface box 203 providing an interface communication port between the check controller 120 and the air combat start measurement pod;
Mobile inspection equipment for aviation combat start measurement pod integrated inspection comprising a.
The method of claim 1,
The air combat start measurement pod is made of a plurality,
And an electronic switch (204) for selectively connecting the plurality of air combat start measurement pods to the interface box (203).
The method of claim 2,
And a housing 200 in which the power supply 202, the check controller 120, the interface box 203, and the electronic switch 204 are stacked inwardly assembled. Portable inspection equipment for integrated inspection.
The method of claim 3, wherein
In order to attach and detach the housing 200, the slot guide 240 is installed on one side of the power supply 202, the inspection controller 120, the interface box 203, and the electronic switch 204. Features mobile inspection equipment for air combat start measurement pod combined inspection.
The method of claim 3, wherein
Cover (220-1, 220-2) is fastened and assembled at both ends of the housing 200; Mobile inspection equipment for aviation combat start measurement pod integrated inspection further comprises.
The method of claim 3, wherein
The power supply 202, the inspection controller 120, the interface box 203, and the electronic switch 204 is a modular structure that is a modular structure that is detachable into the housing 200 as a separate component. Portable inspection equipment for inspection.
The method of claim 1,
The air combat start measurement pod is at least one of a capacitive test pod (CTP) -type pod and an air intercept missile-9 (AIM-9) -type pod, the mobile inspection equipment for the integrated aviation combat start measurement pod.
The method of claim 1,
The inspection controller 120, GPS / INS output simulation module for simulating the output to match the interface of the GPS / INS (Global Positioning System / Inertial Navigation System) navigation device, including the aircraft position information and attitude information ( 121); An aircraft simulation module 122 for simulating rocket impact point information of the aircraft; A data link simulation module 123 for simulating link information including a command and control (C2) command and other aircraft information transmitted and received between the air combat start measurement pod and the ground body; An inspection module 124 for performing a self check and a component check of the air combat start measurement pod; And an interface interworking module (125) for managing interworking of discrete (Discrete), 1553B, RS-422 and Ethernet signals.
The method of claim 1,
The condition check comprises a test support mode for operating and testing the air combat start measurement pod (ACMI-POD) on the ground and a check mode for checking the components of the air combat start measurement pod (ACMI-POD). Mobile inspection equipment for the Ford Combined Inspection.
The method of claim 2,
A connector panel 423 coupled to the power supply 202; And
And a multi-tap 421 engaged with the electronic switch 204. The mobile inspection equipment for aviation combat start measurement pod integrated inspection.
The method of claim 1,
And a display (850) for outputting the input information or the status information. A plurality of mobile inspection equipment (100) for aeronautical combat start measurement pod integrated inspection according to any one of claims 1 to 11;
A plurality of air combat start measurement pods (ACMI-POD) 820-1, 820-2 connected to the mobile inspection equipment 100 for the air combat start measurement pod integrated inspection;
A management server 840 for generating and controlling a scenario according to a user input so as to simulate the tracks of the aviation combat start measurement pods 820-1 and 820-2 in the mobile inspection equipment 100; And
After the aviation combat start measurement pod is installed as a component unit, connected to an RF (Radio Frequency) matrix and the integrated test bed 600 to simulate the air combat start measurement pods spatially separated from each other on the ground or in the air; Include,
The mobile inspection equipment 100 performs a state check according to the scenario through the integrated test bed 600, generates the result information according to the execution result and transmits to the management server 840 Interlock system.
(a) a plurality of aero combat start measurement pods (ACMI-PODs) 820-1,820-2, in which the integrated test bed 600 is connected with the mobile inspection equipment 100 according to any one of claims 1-11. Coupled to;
(b) generating and controlling a scenario according to a user input so that the management server 840 simulates the track of the air combat start measurement pod;
(c) The air combat start measurement pod is installed in component units, connected by a Radio Frequency (RF) matrix, and simulates the air combat start measurement pods to be spatially separated from each other on the ground or in the air. Performing the state check according to the scenario by the mobile inspection equipment (100); And
(d) generating, by the mobile inspection equipment (100), result information according to a result of the state check, and transmitting the result information to the management server (840);
Control method of the integrated interlocking system comprising a.
A computer-readable storage medium storing program code for executing a control method of an integrated interlocking system according to claim 13.

Images