KR20170024426A - Flying apparatus for droping weapon and aircraft including thereof - Google Patents

Flying apparatus for droping weapon and aircraft including thereof Download PDF

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Publication number
KR20170024426A
KR20170024426A KR1020150119694A KR20150119694A KR20170024426A KR 20170024426 A KR20170024426 A KR 20170024426A KR 1020150119694 A KR1020150119694 A KR 1020150119694A KR 20150119694 A KR20150119694 A KR 20150119694A KR 20170024426 A KR20170024426 A KR 20170024426A
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KR
South Korea
Prior art keywords
aircraft
unit
dropping
target
weapon
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Application number
KR1020150119694A
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Korean (ko)
Inventor
류춘하
조인제
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한국항공우주산업 주식회사
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Priority to KR1020150119694A priority Critical patent/KR20170024426A/en
Publication of KR20170024426A publication Critical patent/KR20170024426A/en

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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
    • B64D1/02—Dropping, ejecting, or releasing articles
    • B64D1/04—Dropping, ejecting, or releasing articles the articles being explosive, e.g. bombs
    • B64D1/06—Bomb releasing; Bombs doors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D43/00—Arrangements or adaptations of instruments
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

The present invention relates to an armed flight device and an aircraft including the same, in which an aircraft can be automatically operated and armed release can be performed, and a weapon-mounted flight device mounted on an aircraft for dropping a weapon toward a ground target, A generating unit for generating a driving point of the arming and a driving route of the aircraft on the basis of the position information of the target provided from the measuring unit, a measuring unit for measuring the position of the target, And a driving unit for automatically driving the aircraft to the unloading position based on the driving route provided from the generating unit. Accordingly, the armed delivery flight device and the aircraft including the armed dragging flight device are automatically operated and discharged when the armed force is dropped, so that safe aircraft operation and precise arming can be effected.

Figure P1020150119694

Description

FIELD APPARATUS FOR DROPING WEAPON AND AIRCRAFT INCLUDING THEREOF FIELD OF THE INVENTION [0001]

BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to an armed flight device and an aircraft including the same. More particularly, the present invention relates to an armed flight device and an aircraft including the same.

Generally, an aircraft is equipped with a flight control unit and a mission unit. Here, the flight control unit is involved in the overall control of the airplane flight, and the mission unit is involved in arming and navigation. Accordingly, the pilot who is aboard the aircraft can control the flight control unit and the mission unit during the armed release, thereby causing the target to be dropped on the target.

At this time, the pilot can control the control unit disposed in the aircraft, select the weapon release mode, and confirm the position of the target based on the air-to-ground laser. Then, the pilot recognizes the cover page screen shown in FIG. 7 so that the flight path mark (FPM) corresponds to the azimuth steering line (ASL), and the weapon release button (WRB: Weapon Release Button) and fly the weapon toward the target when the flight path mark reaches the Solution Cue (SC). After the armed release, the pilot controls the control unit to perform the ascending maneuver.

However, the conventional weapon drop technology has a problem that it is difficult for the pilot to operate the aircraft and to drop the weapon simultaneously, so that it is difficult to operate the aircraft safely and to drop the weapon accurately.

Korean Registered Patent No. 10-1492830 (Apparatus and method for analyzing armed release of an aircraft, 2015.02.04)

It is an object of the present invention to provide an armed flight device and an aircraft including the armed-flight device capable of automatic operation and armed release.

The present invention relates to an armed launching aircraft mounted on an aircraft that is capable of dropping armed toward a ground target, the armed launching aircraft having a measurement unit for measuring the position of the target and a position information of the target provided from the measurement unit A generating unit for generating a dropping point of the weapon and a driving route of the airplane based on the dropping point of the weapon and a dropping unit for automatically dropping the weapon from the aircraft toward the target at a dropping time provided from the generating unit, And an operating unit for automatically operating the aircraft to the armed release position based on the provided travel route.

Wherein the generating unit further comprises a flight path mark for marking the actual flight direction of the aircraft on the cover unit and a flag indicating a position of the flight path mark on the cover unit, The route to the target is marked on the marking section, and the travel route can be calculated based on the deviation of the flight route mark and the travel route.

Wherein the generating unit further includes a flight path mark for marking the actual flying direction of the aircraft on the marking unit, A discharge mark marking a position on the marking unit is generated and the discharge time point may be calculated based on a deviation between the flight path mark and the discharge mark.

The operating portion may cause the aircraft to automatically reach the armed release position after dropping the armed weapon.

The armed launching airfield may further include a conversion unit interlocked with the dropping unit and the driving unit so that the arming drop and the operation of the airplane are manually converted.

According to another aspect of the present invention, there is provided an aircraft for dropping a weapon toward a ground target, the aircraft comprising: a main body and a measurement unit for measuring a position of the target; A delivery portion for allowing the armed force to be automatically discharged from the aircraft toward the target at a delivery time provided by the generation portion and a delivery portion for delivering the delivery route from the delivery portion to the target, And an operation unit for allowing the aircraft to be automatically operated to the unloading position.

According to the present invention, the armed delivery flight device and the aircraft including the armed dragging flight device are capable of performing safe operation of the aircraft and precise dropping of the weapon by automatically performing the flight and armed release during the armed release.

The technical effects of the present invention are not limited to the effects mentioned above, and other technical effects not mentioned can be clearly understood by those skilled in the art from the following description.

1 is a view showing an aircraft and a target according to the present embodiment,
2 is a block diagram showing an aircraft according to the present embodiment,
3 is a view showing a cover screen of an aircraft according to the present embodiment,
4 to 6 are views showing automatic operation and automatic dispatching of an aircraft according to the present embodiment,
FIG. 7 is a view showing a conventional airplane cover screen.

Hereinafter, embodiments of the present invention will be described in detail with reference to the accompanying drawings. However, it should be understood that the present invention is not limited to the disclosed embodiments, but may be implemented in various forms, and the present embodiments are not intended to be exhaustive or to limit the scope of the invention to those skilled in the art. It is provided to let you know completely. The shape and the like of the elements in the drawings may be exaggerated for clarity, and the same reference numerals denote the same elements in the drawings.

FIG. 1 is a view showing an aircraft and a target according to the present embodiment, and FIG. 2 is a block diagram showing an aircraft according to the present embodiment.

As shown in FIGS. 1 and 2, the main body of the aircraft 100 according to the present embodiment is loaded with the armed flight device 100a. Here, the aircraft 100 may be provided as an unmanned aircraft or an aircraft that can drop an armed weapon 10 such as a surface-to-air missile toward a ground target 30, but the type of the aircraft 100 is Not limited.

However, in order to facilitate understanding of the airplane 100 according to the present embodiment, description will be made on the basis of popularity.

The armed flight device 100a may include a mission unit 110, a flight control unit 130 and a conversion unit 150. [

First, the mission unit 110 is involved in the control of the arming (10) dropping and navigating except for the control related to the flight of the aircraft 100. Here, the mission unit 110 may include a measuring unit 111, a dropping system control unit 113, a generating unit 115, and an automatic dropping unit 117.

The measuring unit 111 is for measuring the position of the target 30 located on the ground, and may be provided by an air-to-ground laser, but the type of the measuring unit 111 is not limited.

The dropping method control unit 113 controls the dropping manner of the weapon 10 dropped from the airplane 100. Here, the dropping method of the weapon 10 may be a Continuously Computed Impact Point (CCIP) dropping method, a DTOS (Dive Toss) dropping method, or the like.

First, the CCRP dropping method designates the position of the target 30 with the measuring unit 111, and while flying toward the target 30 while holding down the Weapon Release Button (WRB) So that the weapon 10 is released from the target 30 toward the target 30.

The CCIP dropping scheme allows the pilot to drop the weapon 10 from the aircraft 100 toward the target 30 by pressing the weapon release button on the basis of the weapon drop target point marked on the marker 170.

The DTOS release system allows the pilot to visually confirm the position of the target 30, control the target designation box marked on the marking unit 170, and press the weapon release button to move from the aircraft 100 toward the target 30, ) To be released.

The generating unit 115 uses the position information of the target 30 provided from the measuring unit 111 to set the dispensing time of the arming unit 10 and the travel route of the aircraft 100.

3 is a view showing a cover screen of an aircraft according to the present embodiment.

3, the generating unit 115 is interlocked with the dropping system control unit 113 and generates a flight path mark 171, a travel line 173, and a dropping mark 175, ) And information related to the release of the arming (10) may be marked on the marking unit 170. [

At this time, the flight path mark 171 may indicate a direction in which the aircraft 100 actually flows, and the flight line 173 may indicate a guide line so that the aircraft 100 can aim at the target 30 or a predetermined path. do. And the dropping mark 175 may mark the dropping position or point of time of the weapon 10 from which the weapon 10 can be dropped from the aircraft 100 towards the target 30. [

The generating unit 115 may generate an operation route that enables the aircraft 100 to be automatically operated based on the deviation of the flight path mark 171 and the operation line 173 displayed on the marking unit 170 And can calculate the dropping point of time at which the weapon 10 is automatically dropped from the aircraft 100 toward the target 30 based on the deviation of the flight path mark 171 and the drop mark 175.

The generating unit 115 generates a flight path mark 171, a travel line 173 and a dropping mark 175 displayed on the marking unit 170 when the dropping method control unit 113 operates in the CCRP dropping system The route of operation and the generation conditions of the delivery point of time are not limited.

1 and 2, the automatic unloading unit 117 is interlocked with the generating unit 115 so as to move from the aircraft 100 toward the target 30 at the dropping time provided by the generating unit 115 So that the weapon 10 is automatically dropped. That is, when the aircraft 100 arrives at the armed release position by flying along the route, the automatic dropping unit 117 causes the armed unit 10 to move from the aircraft 100 to the target 30 To be discharged automatically.

The flight control unit 130 is involved in the control related to the flight of the aircraft 100 and performs flight control such as takeoff and landing, direction change, speed change, etc. of the aircraft 100. Here, the flight control unit 130 may include the operation control unit 131 and the automatic operation unit 133. [

The operation control unit 131 generally controls the operation of the aircraft 100 so that the aircraft 100 can perform takeoff and landing, direction change, speed change, and the like.

The automatic operation unit 133 interlocks with the operation control unit 131, the automatic disposal unit 117 and the generation unit 115 so that the airplane 100 is automatically operated along the operation route provided from the generation unit 115 . Here, the automatic driving unit 133 is configured to automatically move the armed vehicle 10 toward the target 30 while the aircraft 100 reaches the armed release position along the operating route provided from the generating unit 115, ) Can be automatically raised. At this time. The aircraft 100 can perform the ascending maneuver to approximately 5 g.

On the other hand, the conversion unit 150 allows the flight and arming 10 of the aircraft 100 to be converted automatically or manually. Here, the conversion unit 150 includes a conversion unit 151.

The conversion unit 151 may be provided by a switch or a touch screen method and may be operated automatically or manually when the pilot 100 is operated or during the automatic operation of the aircraft 100, . ≪ / RTI >

However, in the present embodiment, the operation of the airplane 100 and the dropping of the airplane 10 are automatically or manually converted according to the input of the pilot, but the airplane 100 is automatically operated It is also possible to automatically convert the mode of operation of the airplane 100 from automatic operation to manual operation at the time of ascending operation after automatically dropping the armed weapon 10 toward the target 30.

Although the present embodiment describes that the conversion unit 150 is provided separately from the mission unit 110 and the flight control unit 130, the conversion unit 150 includes the mission unit 110 and the flight control unit 130 ) Itself.

Hereinafter, a detailed description will be given of a method of automatic operation and automatic arming and dropping of an aircraft with reference to the accompanying drawings. However, the detailed description of the above-described components will be omitted and the same reference numerals will be given.

FIGS. 4 to 6 are views showing automatic operation and automatic dispatching of an aircraft according to the present embodiment.

4 to 6, the aircraft 100 according to the present embodiment may drop the armed weapon 10 toward the target 30 during flight.

At this time, the pilot controls the mission unit 110 to prepare for the release of the armed unit 10. Here, the dropping scheme control unit 113 can select one of the dropping scheme such as the CCRP dropping scheme, the CCIP dropping scheme, and the DTOS dropping scheme according to the control of the pilot. However, in order to facilitate understanding of the airplane 100 according to the present embodiment, operation in the CCRP dropping method will be described below.

The pilot has to control the airplane 100 so as to correspond to the flight line 173 with the flight path mark 171 marked on the marking unit 170 and perform the operation to the target 30 do. In this embodiment, however, the generating unit 115 generates a driving route based on the deviation of the flight path mark 171 and the driving line 173, and the automatic driving unit 133 generates a driving route, Thereby allowing the airplane 100 to automatically travel to the unarmed position along the route.

At this time, the flight path mark 171 marked on the marking unit 170 is changed to correspond to the dropping mark 175, and the airplane 100 is changed so that the dropping mark 175 is displayed by the automatic driving unit 133 And can be operated automatically to the armed release position where it is being operated. Here, the automatic operation of the aircraft 100 can be performed 4 to 10 seconds before reaching the target 30 (see FIG. 4).

Before or during the automatic operation of the airplane 100, the generating unit 115 generates a target (target) image from the aircraft 100 based on the deviation between the flight path mark 171 marked on the marking unit 170 and the drop mark 175 30 at which the weapon 10 is automatically dropped. Thereafter, when the aircraft 100 reaches the unarmed position, the automatic unloading unit 117 allows the armed forces 10 to be automatically dropped from the aircraft 100 at the time of arming. At this time, the cover unit 170 may be marked with a weapon drop notification 177 informing the automatic weapon release. Here, the automatic disarming of the aircraft 100 may be performed one to three seconds before the aircraft 100 reaches the target 30 (see FIG. 5).

Thereafter, when the armed weapon 10 is dropped from the airplane 100 toward the target 30, the automatic operation unit 133 causes the airplane 100 to automatically ascend and start so that the airplane 100 can quickly escape from the blasting area (See Fig. 6).

Here, the conversion unit 151 may automatically convert the operation of the aircraft 100 from the automatic to the manual at the time when the aircraft 100 escapes from the blasting area, but the conversion unit 151 Manual control to convert the operation of the aircraft 100 from automatic to manual.

Thus, the armed delivery flight device and the aircraft including the armed dragging flight device are automatically operated and discharged when the armed force is dropped, so that the safe operation of the aircraft and the accurate dropping of the weapon are possible.

One embodiment of the invention described above and shown in the drawings should not be construed as limiting the technical idea of the present invention. The scope of protection of the present invention is limited only by the matters described in the claims, and those skilled in the art will be able to modify the technical idea of the present invention in various forms. Accordingly, such improvements and modifications will fall within the scope of the present invention as long as they are obvious to those skilled in the art.

10: Armed 30: Target
100: aircraft 100a: armed flight device
110: mission unit 111: measuring unit
113: Drop-off system control unit 115:
117: automatic dropper 130: flight control unit
131: Operation control unit 133: Automatic operation unit
150: conversion unit 151: conversion unit
170:

Claims (6)

A weapon-mounted flight device mounted on an aircraft that is aiming at a ground target,
A measuring unit for measuring a position of the target;
A generating unit for generating a dropping point of the weapon and a travel route of the aircraft based on position information of the target provided from the measuring unit;
A dropping unit for automatically dropping the weapon from the aircraft toward the target at a dropping time provided by the generator; And
And a driving unit for automatically operating the aircraft to the arming and discharging position based on the driving route provided from the generating unit.
The method according to claim 1,
Further comprising a marking unit disposed inside the aircraft for marking information related to the operation of the aircraft,
The generating unit
The control unit generates a flight path mark marking the actual flight direction of the aircraft on the cover and a flight line marking the route from the aircraft to the target on the cover, To calculate the travel route.
The method according to claim 1,
Further comprising a marker disposed inside the aircraft for marking information related to the weapon release,
The generating unit
A flight path mark for marking the actual flying direction of the aircraft on the marking unit and a dropping mark for marking the dropping position on the marking unit are generated and based on the deviation of the flight path mark and the dropping mark, Of the armed flight.
The method according to claim 1,
The traveling section
Wherein said aircraft is automatically raised after reaching said armed release position and releasing said armed forces.
The method according to claim 1,
Further comprising a conversion unit interlocked with the unloading unit and the driving unit to convert manually the operation of the weapon drop and the aircraft.
For an aircraft that drops a weapon toward a ground target,
main body;
A measuring unit for measuring a position of the target;
A generating unit for generating a dropping point of the weapon and a travel route of the aircraft based on position information of the target provided from the measuring unit;
A dropping unit for automatically dropping the weapon from the aircraft toward the target at a dropping time provided by the generator; And
And an operation unit for automatically operating the aircraft to the armed release position based on the travel route provided from the generation unit.




KR1020150119694A 2015-08-25 2015-08-25 Flying apparatus for droping weapon and aircraft including thereof KR20170024426A (en)

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20220055041A (en) * 2020-10-26 2022-05-03 한국항공우주산업 주식회사 Urgent decision system of aircraft

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR101492830B1 (en) 2013-07-04 2015-02-11 한국항공우주산업 주식회사 Apparatus and method for analyzing weapon delivery of aircraft

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR101492830B1 (en) 2013-07-04 2015-02-11 한국항공우주산업 주식회사 Apparatus and method for analyzing weapon delivery of aircraft

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20220055041A (en) * 2020-10-26 2022-05-03 한국항공우주산업 주식회사 Urgent decision system of aircraft

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