KR101978489B1 - Apparatus and method for managing launch control or guided weapon launch - Google Patents

Abstract

The present invention relates to a launch control management device of a guided weapon launcher and a method thereof, comprising: a launch procedure management part for receiving and managing a first launch procedure command transmitted from a user interface or a second launch procedure command transmitted from a launcher; a launch procedure execution part for generating a launch procedure execution command based on the received first launch procedure command or the second launch procedure command, and transmitting the launch procedure execution command to an external equipment which is subject of the generated launch procedure execution command; and an equipment state determination part for receiving state information transmitted from the external equipment, and determining whether or not the external equipment is normal in accordance with a preset state reference.

Description

[0001] APPARATUS AND METHOD FOR MANAGING LAUNCH CONTROL OR GUIDED WEAPON LAUNCH [0002]

The present invention relates to an apparatus and method for controlling launch control of an artillery launch vehicle, and more particularly, to an apparatus and method for controlling launch control of an artillery launch vehicle, and more particularly, And more particularly, to an apparatus and method for managing launch control of an artillery launch vehicle that manages command flow and equipment status information.

A guided weapon launch vehicle is a method designed to fly the payload from the launch point to the target point by unguided guidance and to position it at the target location. It modifies the flight path and speed by the function of the equipment installed on the outside of the projectile, It is a system to reach.

In addition, the launch control system is a real-time system in which a defined procedure must be executed within a predetermined time from the preparation of the launched weapon projectile to the launching time, and the command execution order is managed according to the procedure so that the projectile can be launched normally.

 In the conventional launch control system, the command received from the user is a structure for unilaterally transmitting commands to the launch vehicle, the launching platform, the measurement device, and the projectile power supply device. Such a structure has a problem that when the projectile needs to control the external equipment by transmitting commands to the launch control system during the process, it can not be operated in conjunction with the launch control system.

In this regard, Korean Patent Publication No. 2016-0030758 discloses " guided weapon control device, guided weapon system and guided weapon control method ".

SUMMARY OF THE INVENTION The present invention has been made to solve the above-mentioned problems, and it is an object of the present invention to provide an apparatus and method for controlling launch control of an articulated weapon launch vehicle which is interlocked with a user interface or a projectile and receives a launch procedure command.

It is another object of the present invention to provide a launch control management apparatus and method of an induced weapon launch vehicle for transmitting a launch procedure execution command to external equipment matched with a launch procedure execution command generated in the order of received launch procedure commands .

It is another object of the present invention to provide an apparatus and method for controlling the launch of an artillery launch vehicle that receives status information transmitted from external equipment and determines whether the external equipment is normal according to a predetermined status criterion .

According to another aspect of the present invention, there is provided an apparatus for managing launch control of an artillery launch vehicle, comprising: a launching procedure manager for receiving and managing a first launch procedure command transmitted from a user interface or a second launch procedure command transmitted from a launch vehicle; A launch procedure execution unit for generating a launch procedure execution command based on the received first launch procedure command or the second launch procedure command and transmitting a launch procedure execution command to the external equipment that is the subject of the generated launch procedure execution command; And an equipment status determination unit for receiving status information transmitted from external equipment and determining whether the external equipment is normal according to a predetermined status criterion.

In addition, the launching procedure management unit may include a launching procedure management unit for executing launching of the first object including the launching procedure information to be executed by the external equipment including at least one of the projectile, the launching platform, the measurement equipment, and the projectile power supply equipment, A first procedure command receiving unit for receiving a launch procedure command; And a second procedure command receiver for receiving a second launch procedure command including predefined launch procedure information for launching from the launch vehicle.

Also, the launching procedure management unit may include: a sequence scheduling unit for classifying a sequence of the launch procedure command by classifying the received first launch procedure command or the second launch procedure command according to a predefined priority; And a procedure command transmission unit transmitting the sequence command to the launch procedure execution unit in the order of the scheduled launch procedure command.

In addition, the launch procedure execution unit may include a procedure command storage unit for storing a launch procedure command value in the order of the received launch procedure command; A procedure execution command generator for generating a launch procedure execution command according to a stored launch procedure command value; An external equipment search unit for searching and matching external equipment corresponding to the generated launch procedure execution command; And a procedure execution command transmission unit for transmitting a launch procedure execution command to external equipment matched with the launch procedure execution command generated in the order of the received launch procedure command, respectively.

Also, the procedure command storage unit stores the launch procedure command value in the form of ID, and the external device search unit uses the ID of the launch procedure command value stored in the predefined external device search table as a key, And searching for the equipment.

The apparatus status determiner may further include: a status information receiver configured to receive at least one status information transmitted from external equipment; A status information determination unit for comparing received status information with predetermined status reference information of an external device corresponding to the received status information and determining whether the external device is normal or abnormal according to the comparison result; And a status information transmission unit for transmitting the determination result to the user interface.

In addition, the status information determination unit may be configured such that status reference information is set differently for each external device, and the status reference information is selected and compared according to the received status information.

According to another aspect of the present invention, there is provided a method for managing launch control of an artillery launch vehicle, comprising the steps of: receiving a first launch procedure command transmitted from a user interface or a second launch procedure command transmitted from a launch vehicle, ; The launch procedure execution unit generates a launch procedure execution command based on the received first launch procedure command or the second launch procedure command and transmits a launch procedure execution command to the external equipment that is the subject of the generated launch procedure execution command ; And a step of receiving status information transmitted from external equipment by the equipment status determination unit and determining whether the external equipment is normal according to a predetermined status criterion.

The step of receiving and managing the first launch procedure command transmitted from the user interface or the second launch procedure command transmitted from the launch vehicle may further include the steps of receiving a projectile command from the user interface, Receiving a first launch procedure command including launch procedure information to be performed by an external device including at least one of the devices; Receiving a second launch procedure command including predefined launch procedure information for launching from the launch vehicle; Classifying the received first launch procedure command or the second launch procedure command according to a predefined priority to schedule the order of the launch procedure command; And a scheduled launch procedure command to the launch procedure performing unit.

The step of generating the launch procedure execution command based on the received first launch procedure command or the second launch procedure command and transmitting the launch procedure execution command to the external equipment that is the subject of the generated launch procedure execution command includes receiving Storing a launch procedure command value in the order of the launch procedure command; Generating a launch procedure execution command according to the stored launch procedure command value; Searching for and matching external equipment corresponding to the generated launch procedure execution command; And transmitting a launch procedure execution command to external equipment matched with the launch procedure execution command generated in the order of the received launch procedure command, respectively.

The step of storing the launch procedure command values in the order of the received launch procedure commands may include storing the launch procedure command values in the form of an ID.

Also, the step of searching for and matching the external equipment corresponding to the generated launch procedure execution command may be performed by using an ID of the launch procedure command value stored in the predetermined external device search table as an external device corresponding to the launch procedure execution command And searching for the search result.

The step of receiving status information transmitted from external equipment and determining whether the external equipment is normal according to a predetermined status criterion includes receiving at least one status information transmitted from external equipment; Comparing the received status information with predetermined status reference information of an external device corresponding to the received status information, and determining whether the external device is normal or abnormal according to the comparison result; And transmitting the determination result to the user interface.

The step of comparing the received status information with predetermined status reference information of the external device corresponding to the received status information and determining whether the external device is normal or abnormal according to a result of the comparison, The reference information is set differently, and the state reference information is selected and compared with the received state information.

An apparatus and method for controlling an emission control of an artillery launch vehicle according to the present invention having the above-described configuration includes a control unit for receiving a launch procedure command in cooperation with a user interface or a projectile and receiving a launch procedure execution command It is possible to efficiently operate the launch procedure and the processing function of the guided weapon launch vehicle by satisfying the bi-directionality between the user interface and the launch vehicle.

Also, there is an effect that status of external equipment can be grasped in real time by receiving status information transmitted from external equipment and determining whether the external equipment is normal according to a preset status criterion.

FIG. 1 is a view for explaining a launch control management system of an induction weapon projectile according to the present invention.
FIG. 2 is a view for explaining the structure of an emission control and management apparatus of an induction weapon projectile according to the present invention.
FIG. 3 is a view for explaining a detailed configuration of a launching procedure management unit employed in the launch control management apparatus of the guided weapon launch vehicle according to the present invention.
4 is a detailed view for explaining the detailed structure of the launching procedure management unit of FIG.
FIG. 5 is a view for explaining the detailed configuration of a launching procedure performing unit employed in the launch control management apparatus of the guided weapon launch vehicle according to the present invention.
FIG. 6 is a diagram for explaining in detail the detailed structure of the launch procedure management unit of FIG. 5;
7 is a diagram for explaining a structure for searching external equipment in the launching procedure management unit of FIG.
FIG. 8 is a view for explaining the detailed structure of the equipment status determination unit employed in the launch control management apparatus of the guided weapon launch vehicle according to the present invention.
FIG. 9 is a flow chart for explaining a procedure of a fire control control method of an artillery launch vehicle according to the present invention.

While the invention is susceptible to various modifications and alternative forms, specific embodiments thereof are shown by way of example in the drawings and will herein be described in detail.

It should be understood, however, that the invention is not intended to be limited to the particular embodiments, but includes all modifications, equivalents, and alternatives falling within the spirit and scope of the invention. Like reference numerals are used for like elements in describing each drawing.

It is to be understood that when an element is referred to as being "connected" or "connected" to another element, it may be directly connected or connected to the other element, . On the other hand, when an element is referred to as being "directly connected" or "directly connected" to another element, it should be understood that there are no other elements in between.

The terminology used in this application is used only to describe a specific embodiment and is not intended to limit the invention. The singular expressions shall not preclude the presence or addition of a plurality of expressions, including combinations thereof, or combinations thereof, unless the context clearly dictates otherwise. In the present application, the terms "comprises" or "having" and the like are used to specify that there is a feature, a number, a step, an operation, an element, a component or a combination thereof described in the specification, Numbers, steps, operations, components, and components.

Hereinafter, preferred embodiments of the present invention will be described in detail with reference to the accompanying drawings. Hereinafter, the same reference numerals will be used for the same constituent elements in the drawings, and redundant explanations for the same constituent elements will be omitted.

FIG. 1 is a view for explaining a launch control management system of an induction weapon projectile according to the present invention.

1, the launch control management system of the guided weapon launch vehicle according to the present invention includes a user interface 10, a launch vehicle 20, a launching platform 30, a measurement device 40, and a projectile power supply device 50, And an emission control management device 100 of the guided weapon launch vehicle.

The user interface 10 transmits a launch procedure that must be performed by at least one of the launch vehicle, the launch pad, the measurement device, and the projectile power supply device according to a predefined launch procedure.

The projectile 20 must perform the procedure to be performed directly according to the predefined launch procedure within a predetermined time.

The launching platform 30 is a device used to launch a projectile (a rocket or a guided vehicle), such as a suspending type for mounting a projectile, a track type for sliding along a rail, and a cylindrical type for moving a cylindrical launching platform. These launchers range from large launchers used in the Apollo spacecraft to smaller ones in small rockets.

The measuring instrument 40 is a device for measuring the position and speed of a projectile by momentarily measuring the acceleration.

The projectile power supply equipment 50 is a device that supplies power to the projectile.

The launch control management device 100 of the guided weapon launch vehicle performs bidirectional communication with the user interface and the external devices and manages the command flow and the state information of the equipment for accurately launching the guided weapon launch vehicle. This will be described in detail later in the drawings.

FIG. 2 is a view for explaining the structure of an emission control and management apparatus of an induction weapon projectile according to the present invention.

2, the launch control management apparatus 100 of the present invention includes a launching procedure managing unit 110, a launching procedure performing unit 120, and an equipment state determining unit 130 .

The launching procedure management unit 110 receives and manages the first launch procedure command transmitted from the user interface or the second launch procedure command transmitted from the launch vehicle. Here, the first launch procedure command is launch procedure information to be performed by an external device including at least one of a projectile, a launch pad, a measurement device, and a projectile power supply device for launching a projectile transmitted from a user interface, The procedure command is predefined launch procedure information for launching from the launch vehicle.

The launching procedure management unit 110 classifies the received first launch procedure command or the second launch procedure command according to the predefined priority order to schedule the order of the launch procedure command and performs the launch procedure in the order of the scheduled launch procedure command And sends a launch procedure command to the terminal.

The launch procedure execution unit 120 generates a launch procedure execution command based on the received first launch procedure command or the second launch procedure command and sends a launch procedure execution command to the external equipment that is the subject of the generated launch procedure execution command send.

The launching procedure execution unit 120 stores the launching procedure command values in the order of the received launching procedure commands, searches for and matches the external equipment corresponding to the launching procedure execution command generated on the basis thereof, Respectively.

The equipment state determination unit 130 receives the state information transmitted from the external equipment and determines whether the external equipment is normal or not according to a preset state reference.

The apparatus state determination unit 130 receives at least one state information from the external apparatuses and compares predetermined state reference information of the external apparatuses corresponding to the received state information to determine whether the external apparatus is normal or abnormal .

FIG. 3 is a view for explaining the detailed configuration of a launching procedure management unit employed in the launch control management device of the guided weapon launch vehicle according to the present invention, and FIG. 4 is a detailed view for explaining the detailed structure of the launching procedure management unit of FIG. 3 .

Referring to FIG. 3, the launch procedure management unit 110 receives and manages a first launch procedure command transmitted from a user interface or a second launch procedure command transmitted from a launch vehicle.

The launching procedure management unit 110 includes a first procedure command receiving unit 111, a second procedure command receiving unit 112, a sequence scheduling unit 113, and a procedure command transmitting unit 114.

The first procedure command receiving unit 111 receives the first procedure command from the user interface and transmits the first procedure command to the first apparatus 100. The first procedure command receiving unit 111 receives the first procedure command from the user interface, 1 launch procedure command.

The second procedure command receiving unit 112 receives a second launch procedure command including predefined launch procedure information for launching from the launch vehicle.

The order scheduling unit 113 schedules the order of the launch procedure command by classifying the received first launch procedure command or the second launch procedure command according to the predefined priority order. That is, as shown in FIG. 4, the sequence scheduling unit 113 schedules the order of the launch procedure commands based on the predetermined priority irrespective of the order of the received first launch procedure command or the second launch procedure command .

The procedure command transmitting unit 114 transmits the command to the launch procedure performing unit in the order of the scheduled launch procedure command.

FIG. 5 is a view for explaining a detailed configuration of a launching procedure performing unit employed in the launch control management apparatus of the guided weapon launch vehicle according to the present invention, FIG. 6 is a view for explaining the detailed structure of the launching procedure managing unit of FIG. And FIG. 7 is a diagram for explaining a structure for searching for external equipment in the launching procedure management unit of FIG.

5, the launch procedure execution unit 120 according to the present invention generates a launch procedure execution command based on the received first launch procedure command or the second launch procedure command, And transmits the launch procedure execution command to the external equipment that is the subject of the launch procedure.

The launch procedure execution unit 120 includes a procedure command storage unit 121, a procedure execution command generation unit 122, an external equipment search unit 123, and a procedure execution command transmission unit 124.

The procedure command storage unit 121 stores the launch procedure command values in the order of the received launch procedure commands. At this time, the procedure command storage unit 121 stores the launch procedure command values in the ID form and stores them in the order of the launch procedure commands as shown in FIG.

The procedure execution command generation unit 122 generates a launch procedure execution command according to the stored launch procedure command value.

The external device search unit 123 searches for and matches external equipment corresponding to the generated launch procedure execution command. That is, as shown in FIG. 7, the external device search unit 123 searches for external equipment corresponding to the launch procedure execution command using the ID of the launch procedure command value stored in the predetermined external device search table as a key, Time can be lowered to improve real-time performance.

The procedure execution command transmission unit 124 transmits a launch procedure execution command to the external equipment matching the launch procedure execution command generated in the order of the received launch procedure command, respectively. For convenience of explanation, the procedure execution command transmitting unit 124 is described as being transmitted to one of the external apparatuses, but the present invention is not limited to this, and the execution command transmitting unit may be separately configured for each external apparatus.

In this manner, the projectile, the launching platform, the measurement equipment, and the projectile power supply equipment receiving the launch procedure execution command perform the defined operation according to the launch procedure.

FIG. 8 is a view for explaining the detailed structure of the equipment status determination unit employed in the launch control management apparatus of the guided weapon launch vehicle according to the present invention.

Referring to FIG. 8, the equipment status determination unit 130 according to the present invention receives status information transmitted from external equipment and determines whether the external equipment is normal according to a predetermined status criterion.

The apparatus state determination unit 130 includes a state information receiving unit 131, a state information determining unit 132, and a state information transmitting unit 133.

The status information receiving unit 131 receives at least one status information transmitted from external equipment. That is, the status information receiving unit 131 receives status information including at least one of status information transmitted from the launch vehicle, status information transmitted from the launcher, status information transmitted from the measurement equipment, and status information transmitted from the projectile power supply device .

The state information determination unit 132 compares the received state information with predetermined state reference information of the external equipment corresponding to the received state information, and determines whether the external equipment is normal or abnormal according to the comparison result.

The state information determination unit 132 selects state reference information according to the received state information, and the state reference information is selected for each external apparatus.

The status information transmission unit 133 transmits the determination result to the user interface.

FIG. 9 is a flow chart for explaining a procedure of a fire control control method of an artillery launch vehicle according to the present invention.

Referring to FIG. 9, the emission control management method of the guided weapon projectile according to the present invention uses the emission control management apparatus of the guided weapon projectile as described above, and a duplicate description will be omitted.

First, a first launch procedure command including launch procedure information to be performed by an external device including at least one of a projectile, a launch pad, a measurement device, and a projectile power supply device is received for launching a projectile transmitted from a user interface (S100).

Next, a second launch procedure command including predefined launch procedure information for launching transmitted from the projectile is received (S110).

Next, the received first launch procedure command or second launch procedure command is classified according to the predefined priority, and the order of the launch procedure command is scheduled (S120).

Next, the mobile terminal transmits to the launch procedure performing unit in the order of the scheduled launch procedure commands (S130).

Next, the procedure command storage unit stores the launch procedure command values in the order of the received launch procedure commands (S140).

Next, the launch procedure execution command is generated according to the stored launch procedure command value (S150).

Next, the external equipment corresponding to the generated launch procedure execution command is searched and matched (S160).

Next, a launch procedure execution command is transmitted to the external equipment matching the launch procedure execution command generated in the order of the received launch procedure command (S170).

Next, at least one of the status information transmitted from the external devices is received (S180). In operation S180, the status information receiving unit receives status information including at least one of status information transmitted from the launch vehicle, status information transmitted from the launcher, status information transmitted from the measurement equipment, and status information transmitted from the projectile power supply device .

Next, the received state information is compared with predetermined state reference information of the external equipment corresponding to the received state information, and it is determined whether the external equipment is normal or abnormal according to the comparison result (S190).

Next, the determination result is transmitted to the user interface (S200).

The launch control management device of the above-mentioned guided weapon launch vehicle can confirm the following satisfaction.

(1) Confirmation of bidirectional satisfaction

The bidirectional confirmation of the launch control management device of the guided weapon projectile is firstly that communication between the user interface SW and the projectile SW is possible, and secondly, the command processor is normally executed according to the procedure order.

The possibility of communication confirms the linkage between the physical communication connection and the logical communication protocol. In other words, in order to confirm the physical communication connection, the launch control management device, the user interface SW, and the projectile SW of the guided weapon launch object connect with the UDP using Ethernet to confirm that communication is normally performed, In order to check interworking, the contents of the response message received from the launch control management device of the guided weapon projectile in the user interface SW and the projectile SW could be confirmed.

In addition, the normal execution of the command handler sequentially transmits the procedure commands from the user interface SW and the projectile SW in accordance with the defined procedure sequence, and sequentially transmits the procedure SW, the launcher SW, and the measuring instrument SW , It can be confirmed that the state of the projectile power supply equipment is changed.

(2) Real-time satisfaction check

The real-time confirmation of the launch control management device of the guided weapon launch vehicle is performed in such a manner that a procedure command to be input non-periodically first is normally performed, a second normal abnormality state determination function of the external equipment status is periodically performed It is possible to check the real-time property.

 Normal execution of the aperiodic procedure command confirms that the state changes of the projectile SW, launcher SW, measurement equipment SW, and projectile power supply equipment are performed within the reference value and reference time defined in the launch procedure.

 The execution of the periodic state determination function can confirm that there is no omission of the throughput and the state determination result value for the periodic state information message set for each equipment. In other words, the total throughput of N1 + N2 + N3 + N4 messages can be confirmed with N1 projectiles, N2 launchers, N3 measurement devices, N4 power supply devices, and N5 As shown in FIG.

As such, the apparatus and method for controlling the launch of the guided weapon projectile according to the present invention can be implemented by a user interface or a projectile, interfacing with a launch vehicle, receiving a launch procedure command, By transmitting a command to execute the launch procedure to the equipment, it is possible to efficiently operate the launch procedure and the processing function of the guided weapon launch vehicle by satisfying the bi-directionality between the user interface and the launch vehicle.

In addition, it is possible to receive the status information transmitted from the external devices and determine the status of the external device in real time by determining whether the external device is normal according to the preset status criteria.

The functional operations described herein and the embodiments of the present subject matter may be implemented in digital electronic circuitry, computer software, firmware, or hardware, including any of the structures disclosed herein and their structural equivalents, It is possible.

Embodiments of the subject matter described herein may be implemented in a computer program product, in which one or more of the computer program products are encoded on a type of program medium for execution by, or in order to operate, the data processing apparatus May be implemented as a module. The type of program medium may be a propagated signal or a computer readable medium. A propagated signal is an artificially generated signal, such as a machine-generated electrical, optical or electromagnetic signal, generated to encode information for transmission to a suitable receiver device for execution by a computer. The computer-readable medium can be a machine-readable storage device, a machine-readable storage substrate, a memory device, a combination of materials that affect the machine readable propagation type signal, or a combination of one or more of the foregoing.

A computer program (also known as a program, software, software application, script or code) may be written in any form of programming language, including compiled or interpreted language, a priori or procedural language, Components, subroutines, or other units suitable for use in a computer environment.

The computer program does not necessarily correspond to the file of the file device. The program may be stored in a single file provided to the requested program or in a file that contains multiple interactive files (e.g., one or more of which store a module, subprogram, or portion of code) And may be stored in some (e.g., one or more scripts stored in a markup language document).

A computer program may be deployed to run on multiple computers or on one computer, located on a single site or distributed across multiple sites and interconnected by a communications network.

Additionally, the logic flows and structural block diagrams described in this patent document describe corresponding actions and / or specific methods supported by corresponding functions and steps supported by the disclosed structural means, It can also be used to build software structures and algorithms and their equivalents.

The processes and logic flows described herein may be performed by one or more programmable processors that execute one or more computer programs to perform functions by operating on input data and generating output.

Processors suitable for the execution of computer programs include, for example, any one or more of a general purpose and special purpose microprocessor and any kind of digital computer. Generally, a processor will receive instructions and data from read-only memory, random access memory, or both.

A core element of a computer is a processor for performing one or more memory devices and instructions for storing instructions and data. In addition, the computer is generally operable to receive data from, or transmit data to, one or more mass storage devices for storing data, such as magnetic, magneto-optical disks, or optical disks, Or < / RTI > However, the computer need not have such a device.

The description sets forth the best mode of the invention, and is provided to illustrate the invention and to enable those skilled in the art to make and use the invention. The written description is not intended to limit the invention to the specific terminology presented.

Thus, while the present invention has been described in detail with reference to the above examples, those skilled in the art will be able to make adaptations, modifications, and variations on these examples without departing from the scope of the present invention. In other words, in order to achieve the intended effect of the present invention, all the functional blocks shown in the drawings are separately included or all the steps shown in the drawings are not necessarily followed in the order shown, It can be in the range.

100: Launch control management system of guided weapon launch vehicle
110: Launch procedure management unit
120: Launching Procedure Performer
130: equipment state judging unit

Claims (14)

A launching procedure manager for receiving and managing a first launch procedure command transmitted from a user interface or a second launch procedure command transmitted from a launch vehicle;
A launch procedure execution unit for generating a launch procedure execution command based on the received first launch procedure command or the second launch procedure command and transmitting a launch procedure execution command to the external equipment that is the subject of the generated launch procedure execution command; And
And an equipment status determiner for receiving status information transmitted from external equipment and determining whether the external equipment is normal according to a predetermined status criterion,
The launching procedure management unit,
Receiving a first launch procedure command including launch procedure information to be performed by an external device including at least one of a launch vehicle, a launch pad, a measurement device, and a projectile power supply device for launching a projectile transmitted from a user interface A procedure command receiver; And
A second procedure command receiver for receiving a second launch procedure command including predefined launch procedure information for launching transmitted from a projectile;
And a control unit for controlling the launch control of the launched weapon projectile. delete The method according to claim 1,
The launching procedure management unit,
A sequence scheduling unit for classifying a sequence of the launch procedure command by classifying the received first launch procedure command or the second launch procedure command according to a predefined priority; And
A procedure command transmission unit for transmitting to the launch procedure performing unit in order of the scheduled launch procedure commands;
And a control unit for controlling the launch control of the launched weapon projectile. The method according to claim 1,
The launching procedure performing unit,
A procedure command storage for storing a launch procedure command value in the order of the received launch procedure command;
A procedure execution command generator for generating a launch procedure execution command according to a stored launch procedure command value;
An external equipment search unit for searching and matching external equipment corresponding to the generated launch procedure execution command; And
A procedure execution command transmission unit for transmitting a launch procedure execution command to external equipment matched with the launch procedure execution command generated in the order of the received launch procedure command, respectively;
And a control unit for controlling the launch control of the launched weapon projectile. 5. The method of claim 4,
The procedure command storage unit stores the launch procedure command value in the form of ID. The external equipment search unit uses the ID of the launch procedure command value stored in the predefined external equipment search table as a key, and stores the external equipment corresponding to the launch procedure execution command The launch control control device of the weapon launch vehicle. The method according to claim 1,
The apparatus state determination unit may determine,
A status information receiving unit for receiving at least one status information transmitted from external equipment;
A status information determination unit for comparing received status information with predetermined status reference information of an external device corresponding to the received status information and determining whether the external device is normal or abnormal according to the comparison result; And
A status information transmission unit for transmitting the determination result to the user interface;
And a control unit for controlling the launch control of the launched weapon projectile. The method according to claim 6,
Wherein the state information determination unit is configured such that state reference information is set differently for each external device, and selects and compares the state reference information according to the received state information. Receiving and managing a first launch procedure command transmitted from a user interface or a second launch procedure command transmitted from a launch vehicle by a launch procedure manager;
The launch procedure execution unit generates a launch procedure execution command based on the received first launch procedure command or the second launch procedure command and transmits a launch procedure execution command to the external equipment that is the subject of the generated launch procedure execution command ; And
Receiving status information transmitted from external equipment by the equipment status determination unit and determining whether the external equipment is normal according to a predetermined status criterion,
Receiving and managing the first launch procedure command transmitted from the user interface or the second launch procedure command transmitted from the launch vehicle,
Receiving a first launch procedure command including launch procedure information to be performed by an external device including at least one of a launch vehicle, a launch pad, a measurement device, and a projectile power supply device for launching a projectile transmitted from a user interface; And
Receiving a second launch procedure command including predefined launch procedure information for launching from the launch vehicle;
Wherein the launch control control method comprises the steps of: 9. The method of claim 8,
Receiving and managing the first launch procedure command transmitted from the user interface or the second launch procedure command transmitted from the launch vehicle,
Classifying the received first launch procedure command or the second launch procedure command according to a predefined priority to schedule the order of the launch procedure command; And
To the launch procedure performing unit in the order of the scheduled launch procedure command;
Wherein the launch control control method comprises the steps of: 9. The method of claim 8,
Generating the launch procedure execution command based on the received first launch procedure command or the second launch procedure command and transmitting the launch procedure execution command to the external equipment that is the subject of the generated launch procedure execution command,
Storing a launch procedure command value in the order of the received launch procedure command;
Generating a launch procedure execution command according to the stored launch procedure command value;
Searching for and matching external equipment corresponding to the generated launch procedure execution command; And
Transmitting a launch procedure execution command to external equipment matched with the launch procedure execution command generated in the order of the received launch procedure command, respectively;
Wherein the launch control control method comprises the steps of: 11. The method of claim 10,
The step of storing the launch procedure command value in the order of the received launch procedure command comprises:
Wherein the launch procedure command value is stored in an ID form. 12. The method of claim 11,
Searching for and matching the external equipment corresponding to the generated launch procedure execution command,
Wherein the external equipment corresponding to the launch procedure execution command is searched using the ID of the launch procedure command value stored in the predetermined external equipment search table as a key. 9. The method of claim 8,
The step of receiving status information transmitted from external equipment and determining whether the external equipment is normal according to a predetermined status criterion,
Receiving at least one status information transmitted from external equipment;
Comparing the received status information with predetermined status reference information of an external device corresponding to the received status information, and determining whether the external device is normal or abnormal according to the comparison result; And
Transmitting a determination result to a user interface;
Wherein the launch control control method comprises the steps of: 14. The method of claim 13,
Comparing the received state information with predetermined state reference information of the external equipment corresponding to the received state information and then determining whether the external equipment is normal or abnormal according to the comparison result,
Wherein the state reference information is set differently for each of the external devices, and the state reference information is selected and compared with the received state information.

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