CN209588843U - Missile intercept device - Google Patents
Missile intercept device Download PDFInfo
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- CN209588843U CN209588843U CN201920023397.4U CN201920023397U CN209588843U CN 209588843 U CN209588843 U CN 209588843U CN 201920023397 U CN201920023397 U CN 201920023397U CN 209588843 U CN209588843 U CN 209588843U
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
- F41H11/00—Defence installations; Defence devices
- F41H11/02—Anti-aircraft or anti-guided missile or anti-torpedo defence installations or systems
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- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
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- General Engineering & Computer Science (AREA)
- Radar Systems Or Details Thereof (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
The utility model provides a kind of missile intercept device, comprising: signal receiver, controller, propulsive mechanism, ammunition dispense mechanism；Wherein the ammunition dispenses mechanism storage primary and secondary ammunition.The signal receiver is for receiving igniting command signal, and the controller is for controlling the propulsive mechanism igniting when the signal receiver receives firing command signal, to push missile intercept device to enter pre-set flight trajectory；The controller dispenses the mechanism release primary and secondary ammunition described in being also used to control in the pre-set flight trajectory, attacks the primary and secondary ammunition group of target to be formed for intercepting.The missile intercept device of the utility model, by come attack guided missile trajectory near dispose primary and secondary ammunition group, all kinds of suspicious objects of guided missile carrying can be removed on a large scale, thus safety of the protection by missile attack side.
Description
Technical field
The utility model relates to missile defense technology fields, and in particular to a kind of missile intercept device.
Background technique
With the rapid development of missile armament technology, the core sharp weapon that have been increasingly becoming in modern war.It can be said that leading
Play the epitome that weapon is a national military strength.In order to improve missile attack effect, usually there is certain penetration ability,
This is also the important indicator that whether can be survived concerning guided missile.
For defender, in order to avoid by missile attack, needing effectively to be intercepted to the guided missile of offense.Currently,
The military powers such as the United States, Russia are all in the foundation for accelerating propulsion defensive missile system.
In addition, guided missile usually carries the penetration techniques such as multiple bullets or a large amount of baits when target of attack, it is traditional
Missile intercept is usually too tired to deal in actual combat, and the missile intercept device for being equipped with a variety of penetration techniques can be intercepted by needing one kind, from
And protect one's own side safe.
Utility model content
For above-mentioned technical problem in the prior art, the utility model proposes a kind of missile intercept method devices.Guided missile blocks
Primary and secondary ammunition can disposed the trajectory or near zone of attacking guided missile by cutting device, can remove guided missile on a large scale in flight
All kinds of suspicious objects carried.
The utility model provides a kind of missile intercept device, comprising: signal receiver, controller, propulsive mechanism, ammunition cloth
Spread mechanism；Wherein the ammunition dispenses mechanism storage primary and secondary ammunition；The signal receiver is for receiving igniting command signal, institute
Controller is stated for controlling the propulsive mechanism igniting when the signal receiver receives firing command signal, is led with pushing
It plays blocker and enters pre-set flight trajectory；The controller is also used to dispense mechanism described in pre-set flight trajectory control and release
The primary and secondary ammunition is put, attacks the primary and secondary ammunition group of target to be formed for intercepting.
In one embodiment, the primary and secondary ammunition is furnished with time-delay fuze and/or contact fuze, and the controller is for controlling
It makes and quick-fried to attack the shrapnel efficacy-enhancing ingredient that target crosses, attacks target to destroy.
In one embodiment, missile intercept device further includes detector, and the detector is for detecting to attack the side of target
Boundary's range；The controller is used to control the ammunition according to the bounds and dispenses mechanism dispensing primary and secondary ammunition.
In one embodiment, the pre-set flight trajectory is at least partly overlapped with come the trajectory of attacking target；It is described
The controller control ammunition dispenses mechanism and launches primary and secondary ammunition before missile intercept device is contacted with the bounds, so that
The primary and secondary ammunition attacks target relative movement with described along the intersection, and the controller controls the shrapnel
Medicine is ignited when at least partly intersecting with the bounds.
In one embodiment, the detector is for bounds described in real-time detection, and the controller is according to
The shape and change in shape of bounds launch primary and secondary ammunition, thus the primary and secondary ammunition being launched with the first 3D shape with it is described
Moved toward one another to attack target, and the controller control the primary and secondary ammunition group with the bounds at least 50% each other
It is ignited when intersection.
In one embodiment, first 3D shape is umbrella shape, the cone direction that opening attacks guided missile towards described
It is described to attack the diamond shape of target and axis and the trajectory to attack target to attack the taper of target, water chestnut towards described
At least one of consistent cylinder in direction.
In one embodiment, size of first 3D shape at least in two spaces dimension is greater than the boundary
Range.
In one embodiment, the controller controls the primary and secondary ammunition and reaches in the registration with the bounds
It is ignited when maximum, with the suspicious object destroyed in the bounds.
In one embodiment, the detector for the movement speed of bounds in space described in real-time detection and
Change in shape, the controller calculate the delivering opportunity of the primary and secondary ammunition, launch according to the movement speed and change in shape
The quantity for the primary and secondary ammunition launched in batch and each batch is launched at interval；The controller controls the ammunition and dispenses machine
Structure according to the delivering opportunity, launch interval, release batch, the quantity of primary and secondary ammunition launched in batch is to the side each time
Boundary's range launches primary and secondary ammunition.
In one embodiment, the detector is also used to detect the relative velocity of the blocker Yu the bounds
And relative position, so that the controller, which controls the ammunition according to the relative velocity and the relative position, dispenses mechanism throwing
Put primary and secondary ammunition.
The missile intercept device that the embodiments of the present invention provide, by come attack guided missile trajectory on deployment it is a large amount of
Primary and secondary ammunition can remove all kinds of of extended threat region and attack target, protection one's own side's safety.
In reading specific embodiment and after checking attached drawing, those skilled in the art will recognize that other spy
It seeks peace advantage.
Detailed description of the invention
In order to illustrate the embodiment of the utility model or the technical proposal in the existing technology more clearly, below will be to embodiment
Needed in attached drawing be briefly described, it should be apparent that, the accompanying drawings in the following description is only the utility model
Some embodiments for those of ordinary skill in the art without creative efforts, can also be according to this
A little attached drawings obtain other attached drawings.
Fig. 1 is the block diagram according to the missile intercept device of the utility model embodiment.
Fig. 2 is the middle section hold-up interception method flow diagram according to the ballistic missile of the utility model embodiment.
Fig. 3 is the schematic diagram that the blocker of the utility model embodiment launches more batches of primary and secondary ammunition attacks to attack target.
Fig. 4 is the bounds schematic diagram according to the interception region of the utility model embodiment.
Fig. 5 be the utility model embodiment primary and secondary ammunition with attack target relative flight and trajectory is at least partly heavy
The schematic diagram of conjunction.
Fig. 6 a-6e is the schematic shapes that the primary and secondary ammunition of the utility model embodiment is disposed in space.
Specific embodiment
Further illustrate the technical solution of the utility model below with reference to the accompanying drawings and specific embodiments.Such as
" following ", " lower section ", " ... under ", " low ", " top ", " ... on ", the spatial relation term of "high" etc. is for making description side
Just, to explain positioning of the element relative to second element, indicate in addition to from shown in figure those be orientated different orientations
In addition, these terms are intended to cover the different orientation of device." element on the other element/under " can be in addition, for example
It indicates that two elements directly contact, can also indicate that also there are other elements between two elements.In addition, such as " first ", " the
Two " etc. term is also used for describing each element, area, part etc., and should not be regarded as limiting.Similar term is logical in description
Similar element is indicated in.
During describing the utility model, while following two similar words are used, i.e., to attack guided missile and to attack
Target.It will be understood by those skilled in the art that the entity that different nouns is referred to has no substantive difference.In the hair of ballistic missile
It penetrates initial stage, all suspicious objects that will be disposed are carried by ballistic missile.As ballistic missile is got at a distance from the earth
Come remoter, progresses into middle section mission phase.For example, after ballistic missile enters middle section mission phase, the load of carrying
For example true bullet of lotus, decoy warhead, bait and other Countermeasures are released, and these targets are flown together in space.Thus may be used
See, these targets are all a part that initial ballistic missile is isolated, therefore are referred to alternatively as to attack guided missile.Similarly, since these
Target belongs to suspicious object, therefore also referred to as suspicious object.Different terms used by the application are referred to specific
Entity may be considered similar.For example, it both can be only true bullet that these, which refer to word, it is also possible to comprising a large amount of false mesh
The true bullet of target can also be the combination etc. of multiple bullets or multiple bullets and several decoys.Those skilled in the art
The protection scope of the utility model must not be reduced, changes or twisted and making restrictive interpretation to above-mentioned word.
By taking ballistic missile as an example, defence includes section of taking off defence, ascent stage defence, midcourse defense and terminal defense.Bullet
Ballistic missile is relatively long in the time that middle section is flown, and defender takes the opportunity of defensive measure more, therefore, midcourse defense system
Foundation be also ballistic missile defense emphasis.However, ballistic missile is (especially in order to ensure the penetration ability of ballistic missile
Carrying the ballistic missile of nuclear weapon) usual situation is equipped with all kinds of penaids.These penaids include decoy warhead, lure
Bait, aluminium foil etc. make defender that can not identify true bullet target from all multiple targets to interfere the radar detection of defender, from
And true bullet can be under the shielding of these shielding apparatus, the missile defense systems for the side of breaking through the defence.In addition, being in payload
In the case where multiple warhead, traditional shock interception mode is almost impossible to intercept all guided missile warheads, to have a large amount of
To the territory of defender, this is seriously threatened to being caused by the national security of attacker the attack of true bullet.
The missile intercept device of the utility model, which can be used for intercepting, carries multiple bullets or a large amount of aluminium foils of outfit or bait
Equal Countermeasures attack guided missile, and a large amount of bullets and bait that can be attacked in the future are caught all in one draft, and especially suitable for blocking in middle section
The ballistic missile for cutting to attack.But the scope of application of the utility model is not limited to intercept trajectory guided missile, is also possible to other types of
To attack guided missile.
The utility model provides a kind of missile intercept device.Referring to Fig. 1, missile intercept device 2 may include: signal receiver
100, controller 200, propulsive mechanism 300, ammunition dispense mechanism 400.Wherein the ammunition dispenses mechanism 400 and stores shrapnel
Medicine.The signal receiver 100 is for receiving igniting command signal, and the controller 200 in the signal receiver for connecing
100 control the propulsive mechanism 300 when receiving firing command signal lights a fire, to push missile intercept device to enter pre-set flight bullet
Road.The controller 200, which is also used to dispense mechanism 400 described in pre-set flight trajectory control, discharges the primary and secondary ammunition,
The primary and secondary ammunition group of target is attacked to be formed for intercepting.The missile intercept device of the utility model, by pre-set flight trajectory
Primary and secondary ammunition group is dispensed, can be removed on a large scale to attack target, be greatly reduced to true and false and attack target identification demand.
For example, the primary and secondary ammunition is furnished with time-delay fuze and/or contact fuze, the controller 200 is for controlling and coming
It is quick-fried to attack the shrapnel efficacy-enhancing ingredient that target crosses, attacks target to destroy.Wherein, controller 200 can control the ignition of primary and secondary ammunition
Time, to destroy to the maximum extent to attack target.For example, primary and secondary ammunition exists when primary and secondary ammunition is equipped with contact fuze simultaneously
It is ignited when target contacts with to attack.
For example, propulsive mechanism 300 can be conventional solid propellant propulsion system, with Solid rocket propulsion system or can specifically consolidate
Body missile propulsion system.
In addition, the utility model additionally provides a kind of missile intercept method.Referring to fig. 2, missile intercept method includes: that S1 is visited
It surveys to attack the trajectory and flying speed of guided missile；S2 calculates the pre- of blocker according to the flying speed and the trajectory
If launch time and pre-set flight trajectory；Wherein the blocker carries primary and secondary ammunition；S3 makes the blocker described default
Launch time transmitting, and along the pre-set flight ballistic flight, to enter the bullet for attacking guided missile for described at the first moment
Medicine launches region；Blocker described in S4 launches region in the ammunition and attacks guided missile dispensing primary and secondary ammunition to described, thus described
Primary and secondary ammunition is ignited to destroy and described attack guided missile intercepting region.The middle section hold-up interception method of the ballistic missile of the utility model,
By disposing primary and secondary ammunition the trajectory of attacking guided missile, can destroy on a large scale includes suspicious object to attack guided missile, greatly
The big requirement reduced to the intersection accuracy of ballistic missile, improves the success rate of missile intercept.
For example, in step sl, the trajectory and flying speed of guided missile can be attacked using the radar detection of ground middle section.
For example, can determine that flying speed can pass through detection in the tracking of a period of time by radar to attack the trajectory of guided missile
It is calculated to attack guided missile in the position at two time points and by the time used in the two positions.In addition it is also possible to using being deployed in
The trajectory and speed of the reconnaissance satellite detection ballistic missile of space.In the case, for example, reconnaissance satellite can in real time to
Ground returns to the information about missile flight speed and trajectory, so that ground defense system can be in real time according to guided missile
Flying speed and trajectory emit blocker.
The primary and secondary ammunition of the utility model meaning, such as may include the bomblet that can be disposed in space large-range,
It is also possible to the small-sized nuclear bomb that can independently ignite.Primary and secondary ammunition selection can according to come attack target characteristic determine.
For example, coming from military power in the case where primary and secondary ammunition is bomblet to attack guided missile, then the explosion prestige of bomblet
Power tends to bigger (mainly in view of the bullet of military power mostly uses certain strengthening measure).For example, in primary and secondary
In the case that ammunition is small-sized nuclear bomb, since nuclear bomb can attack target with the destruction of maximum probability, the equivalent of small-sized nuclear bomb without
Specific requirement.But since nuclear bomb is in outer space explosion time, certain threat, therefore, the equivalent of small-sized nuclear bomb can be also constituted to native country
It is the smaller the better, and the nuclear bomb not ignite other side as far as possible is principle.In addition, it should be understood that passing through the destruction pair of small-sized nuclear bomb
The value for the nuclear bomb that the guided missile of hand carries, which is far longer than small-sized nuclear bomb, (or even may ignite the nuclear bomb pair of other side including small-sized nuclear bomb
National bring harm) harm brought by outer space explosion.In order to avoid the nuclear blast that may occur in the outer space as far as possible, this
The primary and secondary ammunition of utility model is preferably conventional ammunition.For example, these primary and secondary ammunitions can independent outfit guidance system (example
Such as, guidance system can be infrared guidance or satellite guidance), it is more accurately intercepted to attack a wide range of target implementation.
The missile intercept device and middle section hold-up interception method of the utility model, a large amount of primary and secondary ammunitions that wherein missile intercept device discharges
It can be dispensed in space, this is equivalent in a certain range of space, and interval is provided with a large amount of demolition points.These demolition points are not only
Target can be attacked by exploding directly destruction, and multiple demolition points can form high temperature center after explosion, to make to enter
All suspicious objects of high temperature center are destroyed or are burnt.For example, each demolition point can using delayed exploding or
It hits and ignites.And preferably, each demolition point is equipped with two kinds of detonation ways simultaneously, to avoid being ignited by single impacting type possible
Caused miss target phenomenon and the situation for avoiding as caused by single delayed exploding attack precision not high.
Referring to Fig. 3, for example, in order to improve to the destruction probability for threatening target target can also be being attacked (in Fig. 3
It in the range of rectangle structure, contains to attack guided missile and other suspicious objects, but rectangle structure is just to illustrate, to attack
The shape that target is formed by boundary is not limited to rectangle) on 1 heading S1, the multiple primary and secondary ammunition groups of the deployment at interval
21,22,23, to implement multistage destruction to attack target 1.For example, distance attacks first nearest primary and secondary ammunition group 21 of target 1
The primary and secondary ammunition for including can be most.For example, the quantity of the primary and secondary ammunition in the primary and secondary ammunition group of each batch can be attacked with distance
The increase of guided missile distance is reduced step by step.In the case, the primary and secondary ammunition for including in first primary and secondary ammunition group 21 can be to suspicious
Target implements first wave destruction.For example, suspicious object 1 is after destroying strike through first wave, it is most of to be destroyed.In special feelings
It, can be some by 22 pairs of primary and secondary ammunition group of second lot under condition (for example, some bullets use superpower explosion-proof, high temperature-proof measure)
Fish that has escape the net implements secondary destruction.At this point, due to suspicious object 1 after being destroyed by first primary and secondary ammunition group at least
By a degree of damage, therefore, after the second marble mother ammunition group strike, can easily be destroyed.For example, the
A small amount of primary and secondary ammunition only need to be disposed in three crowdes of primary and secondary ammunition groups 23, remaining target that may be present can be destroyed.This is practical new
The missile intercept device and hold-up interception method of the embodiment of type further improve guided missile by implementing multistage destruction to attack target
The success rate of interception, to preferably protect national Homeland Security.
In one embodiment, referring to fig. 4, with can also include other suspicious objects attack that guided missile 11 flies together
12.True bullet 11 can for example cover a certain range with other suspicious objects 12 in space.For example, disposing true bullet in guided missile
In the case where a variety of Countermeasures, it is difficult to detect the position of true bullet by conventional detection mode.Therefore, for general
All kinds of suspicious objects in above-mentioned coverage area are caught all in one draft, can be using the boundary of the coverage area 13 as the ginseng for intercepting range
Examine deployment primary and secondary ammunition.Specifically, detection device can draw according to the radar appearance region detected and be directed to suspicious object
Interception region bounds.The embodiments of the present invention, can be better by the bounds of drafting suspicious object
Primary and secondary ammunition is disposed, to improve the interception probability to all kinds of suspicious objects.
It in some embodiments, can also be real-time by the detector of missile intercept device for example, the bounds of suspicious object
Detector in detection or ground location device and missile intercept device, which cooperates, to be obtained, so that controller can be according to can be with mesh
Target bounds, control ammunition dispense mechanism and launch ammunition.
In one embodiment, the detection may include: detection institute come the trajectory and flying speed S1 for attacking guided missile
It states to attack the radar reflection of guided missile and its near zone, to calculate the bounds for intercepting region according to the radar reflection
13.The controller 200 of the blocker 2 can launch primary and secondary ammunition to the interception region 13 in the dispensing region, thus
The primary and secondary ammunition destroys in the interception region 13 come to attack guided missile S4 include: the controller 200 of the blocker 2 according to described
The bounds 13 for intercepting region control ammunition and dispense the dispensing primary and secondary ammunition of mechanism 400, thus what the control of controller 200 was launched
Primary and secondary ammunition is ignited when intersecting with the bounds 13 for intercepting region by time-delay fuze and/or contact fuze, to break
Ruin the suspicious object in the bounds 13.The missile intercept device of the embodiments of the present invention, passes through the side of suspicious object
Boundary's range, and being ignited using delay and/or contact fuze, can suspicious object in global purge bounds, thus greatly
The success rate for improving interception.
It should be noted that missile intercept device 2 launch primary and secondary ammunition region can except the bounds of suspicious object,
Launching region can also partially overlap or within bounds with bounds.For example, missile intercept device with it is suspicious
In the case where target relative movement, dispensing region can (front refers to transports in suspicious object in the front that suspicious object moves
Before suspicious object on dynamic direction), so that the primary and secondary ammunition being launched can have more fully, the time is dispersed and is disposed, with
Just it is realized with better space layout state and the entirety of suspicious object is destroyed.
Referring to Fig. 5, in one embodiment, the 200 pre-set flight trajectory of controller of the blocker 2 attacks mesh with described
Trajectory of the mark 11 in the middle section flight phase is at least partly overlapped (intersection is trajectory phase shown in figure label 3).It is described
The controller 200 of blocker 2, which can control ammunition and dispense mechanism 400, launches shrapnel before contacting with the bounds 13
Medicine 21,22, so that the primary and secondary ammunition attacks 1 relative motion of target, and controller 200 with described along the intersection 13
The primary and secondary ammunition 21,22 is controlled to ignite when at least partly intersecting with the bounds 13.
In this embodiment, blocker 2 shown in fig. 5 launches primary and secondary ammunition before reaching coincidence trajectory part, thus
These primary and secondary ammunitions are intersected in intersection 3 with to attack target 1 after entering intersection 3.For example, being reached in blocker 2
It is overlapped before trajectory 3, blocker 2 can discharge primary and secondary ammunition from the top down, so that primary and secondary ammunition, which enters, is overlapped trajectory 3.Hereafter,
For example, blocker 2 can enter be overlapped trajectory 3, thus by blocker be overlapped in trajectory 3 come attack target 1 shock, into one
Step, which improves, intercepts the probability of success.For example, in the case, blocker can be set that end is infrared or radar guidance, and by pushing away
The maximum target of dubiety is hit into device driving blocker.
In this embodiment, blocker 2 can also come attack target 1 trajectory in inversely fly, thus blocker 2
Primary and secondary ammunition can be being discharged to the front of the direction of motion of blocker 2 before target 1 intersects with to attack.Under normal conditions, conventional
The explosion velocity of explosive in 1000~8500 meter per seconds, speed of the ballistic missile during middle section is flown also in 3000-6000 meter per second, by
This as it can be seen that primary and secondary ammunition with attack ignition when target part intersects, explosion wave can quickly feed through to it is each come
Target is attacked, to achieve the purpose that destroy target.
In addition, controller 200 can also dispense the distance between situation, primary and secondary ammunition and each according to primary and secondary ammunition
The power of the explosion of primary and secondary ammunition, calculate these shrapnel efficacy-enhancing ingredients it is quick-fried when explosion wave shape and spread condition, to make
The center for intercepting region is met when shock wave is diffused into maximum (attacking true bullet can destroy as foundation) with shock wave, thus
It further increases to come the destruction effect of attacking target.
The embodiments of the present invention, by making the trajectory of blocker and to attack the trajectory part of target weight
It closes, and by both making relative flight, blocker, primary and secondary ammunition can be improved with come the impact force of attacking target, and ensure primary and secondary
The explosion wave of ammunition is to come the destruction effect of attacking target.
Referring to Fig. 6 a, in one embodiment, the controller 200 of blocker 2 can be according to the shape of the bounds
Mechanism 400 is dispensed with change in shape control ammunition and launches primary and secondary ammunition 21, so that the primary and secondary ammunition 21 being launched is with the first three-dimensional
Shape is attacked target 1 with described and is moved toward one another, and controller 200 can control these primary and secondary ammunitions 21 with the boundary model
Enclose at least 50% each other intersect after ignite.H is the length to attack target 1 on its heading in Fig. 6 a, and h1 is primary and secondary ammunition
21 intersect length with come attack target 1.The embodiments of the present invention by make primary and secondary ammunition and bounds at least 50% with
On ignition when intersecting each other, inside the bounds that suspicious object can be full of by entering a large amount of primary and secondary ammunitions, Ke Yigeng
All kinds of in good destruction bounds attack target, to further improve the probability for destroying true bullet.In order to improve pair
The ratio of the destruction effect of suspicious object, above-mentioned intersection part can be greater than 70%.
It should be pointed out that according to the signal of Fig. 6 a, primary and secondary ammunition and close to attack mutual distance after target intersection.But thing
In reality, (i.e. primary and secondary ammunition and each attack target range farther out) is often spread attacking target on a large scale in space, therefore, not
In the case where using navigational guidance method, each primary and secondary ammunition dispensed is difficult and directly hits to attack target, this is also traditional
Impacting type hold-up interception method attacks larger one of the reason of target difficulty in middle section interception.
Referring to Fig. 6 b-6e, in this embodiment, for example, first 3D shape is that opening attacks guided missile towards described
Umbrella shape, cone the taper of guided missile is attacked towards described, water chestnut attacked towards described guided missile diamond shape and axis and it is described come
Attack at least one of the consistent cylinder of trajectory direction of guided missile.The embodiments of the present invention pass through further cloth
The spatial form of primary and secondary ammunition is set, can preferably be destroyed to attack target.For example, when primary and secondary ammunition uses beveled structure, it can be
When most of suspicious object is fallen into umbrella opening, primary and secondary ammunition is ignited by time-delay fuze.Equally, when primary and secondary ammunition is with cylindrical shape
When arrangement, primary and secondary ammunition can be ignited after suspicious object fully enters in cylinder, to realize from the peripheral to suspicious of suspicious object
Target carries out surrounding explosion, to further increase the probability for destroying suspicious object.
It should be pointed out that the first 3D shape on the one hand can by compartment of terrain, in batches launch primary and secondary ammunition formed.But
Only with this interval, in batches the mode launched, primary and secondary ammunition can be only formed relatively simple arrangement mode.On the other hand,
First 3D shape can also dispense mechanism realization by ammunition.Release of the mechanism 400 to primary and secondary ammunition is dispensed by ammunition
Figuration makes primary and secondary ammunition form specific shape in release.For example, the first 3D shape can also pass through the control of blocker
Device sends flight control instruction to primary and secondary ammunition, is realized with controlling athletic posture and the speed of primary and secondary ammunition.
In the above-described embodiments, the size of first 3D shape at least on two dimensions is greater than the boundary model
It encloses.For example, size of first 3D shape in three dimensions can be respectively than the corresponding size of the bounds of suspicious object
It is big by 5%, to more preferably destroy these suspicious objects.For example, being greater than so that the umbrella finish dimensional of the primary and secondary ammunition of umbellate form deployment is suspicious
Bounds are in the size of the direction, and the diameter of cylindrical type opening is greater than the bounds of suspicious object in equidirectional maximum ruler
It is very little.By adjusting the size of the first 3D shape, suspicious object can be made to fully enter within the opening of disposed primary and secondary ammunition,
To make it further increase the destruction effect of suspicious object.
For example, controller 200, which can control the primary and secondary ammunition that is spread in the sky, to be overlapped with the bounds
Or ignition when reaching maximum of intersection degree, with the suspicious object destroyed in the bounds.For example, when the primary and secondary being distributed
When what ammunition was formed surrounds size of the space greater than suspicious object bounds, it can all enter in all suspicious objects and surround space
When ignite primary and secondary ammunition, to improve to the destruction effect of suspicious object.
In one embodiment, the blocker can also the second moment enter the suspicious object 1 bounds
Within 13, and primary and secondary ammunition 21 is launched and ignited within the bounds 13, to destroy in bounds 13
Target.When the ammunition entrained by the blocker 2 is conventional ammunition, due to blocker 2 with come the speed of related movement pole of attacking target 1
Height, therefore, the ammunition dispensed often have little time dispersion and are just detonated.In this case, the range that explosion can involve is big
Big to reduce, therefore, a part can be made to be located at can not be destroyed close to the suspicious object of bounds.Therefore, in this embodiment,
Preferably, blocker 2 can carry small-sized nuclear bomb, so as to small-sized nuclear bomb can be destroyed inside the bounds of suspicious object it is all can
Doubt target.
In one embodiment, the blocker further includes detector, and detector exists for monitoring the bounds
Movement speed and change in shape in space, and controller 200 calculates the son according to the movement speed and change in shape
The delivering opportunity of female ammunition launches interval, launches the quantity for the primary and secondary ammunition launched in batch and each batch.Controller
According to the delivering opportunity, the quantity control ammunition cloth launched interval, discharge the primary and secondary ammunition launched in batch, each time batch
Spread mechanism to the bounds launch primary and secondary ammunition, thus the primary and secondary ammunition being launched when being intersected with the bounds or
It is ignited before person's intersection by time-delay fuze and/or contact fuze.The embodiments of the present invention pass through the side according to suspicious object
The skyborne movement speed of boundary's range and change in shape determine delivering opportunity, launch interval, launch batch and each batch
The quantity etc. of the primary and secondary ammunition of middle dispensing can be further improved the destruction effect to suspicious object.
For example, detector 200 can calculate relative velocity and the relative position of the blocker and the bounds, control
Device processed selects the delivering opportunity of primary and secondary ammunition accordingly, and is launched and criticized according to the selection of the shape and change in shape of the bounds
The primary and secondary ammunition quantity at dispensing interval and each batch secondary, between each batch.It can be by the controller of blocker for example, calculating
200 voluntarily implement, and in the case, blocker can be equipped with computer.In addition, blocker can also pass through its signal receiver
100 receive ground radars or space reconnaissance satellite can be by measurement result, i.e., by ground radar or too to the detection of suspicious object
Empty reconnaissance satellite is completed, and later, detection result can be sent to the signal receiver 100 of blocker.In addition, the control of blocker
Device can be obtained by its detector and ground location system simultaneously to attack target information, to further increase the standard of detection
True property improves intercepting efficiency.
In one embodiment, the dispensing batch of the primary and secondary ammunition successively includes first batch, centre by the release time
Batch and final batch, and the quantity of primary and secondary ammunition launched of the intermediate batch is greater than the first batch and final batch described
Secondary primary and secondary ammunition injected volume.For example, the intermediate batch includes multiple batches, and the shrapnel that each intermediate batch is launched
The quantity of medicine is all larger than the quantity for the primary and secondary ammunition that the first batch and the final batch are launched respectively.The utility model
Embodiment is by launching primary and secondary ammunition in batches and adjusts the quantity for the primary and secondary ammunition that every batch of is launched, and may be implemented to can be with target
It is multistage destroy, in addition, by keeping the primary and secondary ammunition quantity of intermediate batch larger, can be improved and destroys the probability of true bullet (very
Bullet is usually hidden between decoy warhead and bait and flies).
For example, in one embodiment, the dispensing batch of primary and secondary ammunition includes multiple, and is criticized to the end from first batch
Secondary, the dispensing interval time of primary and secondary ammunition is first reduced to increase afterwards, and each batch launches the quantity first increases and then decreases of ammunition.Example
Such as, when enemy missile uses a variety of Countermeasures, in order to avoid being arrived by the detection of offense, true bullet tends to hidden
It is hidden in middle position.For example, first primary and secondary ammunition launched can be used for destroying and be deployed in front of true bullet (relative to attacking mesh
The target direction of motion) Countermeasures, later, in order to destroy the corresponding real target of missile intercept --- true bullet, shrapnel
The amount of medicine can be significantly increased.Probability due to true bullet in suspicious object tail portion reduces, the quantity of primary and secondary ammunition can be with
It reduces.
It should be noted that the utility model it is signified come to attack target may include that (true bullet can be one to true bullet
Or multiple), it also may include decoy warhead (for example, balloon camouflage bullet), all kinds of baits or aluminium foil etc..
The utility model another aspect provides a kind of middle section intercepting systems of ballistic missile.The middle section intercepting system
Including detecting module, control module and putting module.The detecting module is for detecting to attack the trajectory of guided missile and flight
Speed.The control module is used for: the default launch time of blocker is calculated according to the flying speed and the trajectory
And pre-set flight trajectory；Wherein the blocker carries primary and secondary ammunition；The blocker is controlled to send out in the default launch time
It penetrates, and along the pre-set flight ballistic flight, to enter for described the ammunition dispensing region for attacking guided missile at the first moment；
And the control putting module launches region in the ammunition and attacks guided missile dispensing primary and secondary ammunition to described, thus the primary and secondary
Ammunition is ignited to destroy and described attack guided missile intercepting region.The middle section intercepting system of the ballistic missile of the utility model, passes through
Primary and secondary ammunition is being disposed come the heading for attacking target, can hit with the destruction suspicious object of maximum probability to greatly reduce
Hit required precision of the formula interception to interceptor.
In one embodiment, the detecting module includes radar.Radar described attacks target in space for detecting
Radar reflection.The control module is used to calculate the bounds for intercepting region according to the radar reflection；And control
The putting module according to it is described intercept region bounds launch primary and secondary ammunition, thus the primary and secondary ammunition being launched with institute
It is ignited when stating the bounds intersection for intercepting region or before intersection, with the suspicious object destroyed in the bounds.This reality
The radar reflection of target is attacked by radar detection with novel embodiment, and calculates the boundary model of suspicious object according to reflection
Enclose, can preferably determine the delivering opportunity and putting mode of primary and secondary ammunition, thus further increase remove threaten target can
By property.
In one embodiment, the primary and secondary ammunition configuration time-delay fuze and/or contact fuze are ignited.It on the one hand, can root
With come the speed of attacking target the ignition time of primary and secondary ammunition is previously set, thus in son in the position and speed that is launched according to bullet
Ignition when female ammunition moves to the appropriate location relative to suspicious object attacks target with maximum destruction.On the other hand,
Primary and secondary ammunition can configure triggering ignition fuse simultaneously, so that a large amount of ammunitions dispensed in the sky can be contacted with each suspicious object
When ignite, improve to the destruction effect of suspicious object.For example, time-delay fuze can be according to pre- when contact fuze is not triggered
If the time (for the purpose of attacking target by better destruction) ignites, so that primary and secondary ammunition be avoided to fail.
In such an embodiment, it is preferable each primary and secondary ammunition configures time-delay fuze and contact fuze simultaneously.For example, can be with
Only when contact fuze is not acted upon within a certain period of time, start-up study fuse ignites primary and secondary ammunition, to further increase pair
The reliability that suspicious object is destroyed.
The embodiments of the present invention provide ballistic missile middle section hold-up interception method and system, by come attack guided missile fly
A large amount of primary and secondary ammunitions are disposed on row trajectory, the threat of the payload of ballistic missile carrying can be removed on a large scale, to protect
The under fire Homeland Security of state.
Another aspect of the utility model provides a kind of memory.Wherein, memory is stored with computer-readable finger
It enables.When computer-readable instruction is called, the method that the ballistic missile middle section of the utility model embodiment intercepts is executed.
The another aspect of the utility model provides a kind of server.Server includes memory and processor, described
Memory stores executable program, and the controller is for calling the executable program, thereby executing the utility model implementation
The ballistic missile middle section hold-up interception method of example.
Those of ordinary skill in the art may be aware that list described in conjunction with the examples disclosed in the embodiments of the present disclosure
Member and algorithm steps can be realized with the combination of electronic hardware or computer software and electronic hardware.These functions are actually
It is implemented in hardware or software, the specific application and design constraint depending on technical solution.Professional technician
Each specific application can be used different methods to achieve the described function, but this realization is it is not considered that exceed
The scope of the utility model.
It is apparent to those skilled in the art that for convenience and simplicity of description, the system of foregoing description,
The specific work process of device and unit, can refer to corresponding processes in the foregoing method embodiment, and details are not described herein.
In several embodiments provided herein, it should be understood that disclosed systems, devices and methods, it can be with
It realizes by another way.For example, the apparatus embodiments described above are merely exemplary, for example, the unit
It divides, only a kind of logical function partition, there may be another division manner in actual implementation, such as multiple units or components
It can be combined or can be integrated into another system, or some features can be ignored or not executed.Another point, it is shown or
The mutual coupling, direct-coupling or communication connection discussed can be through some interfaces, the indirect coupling of device or unit
It closes or communicates to connect, can be electrical property, mechanical or other forms.
The unit as illustrated by the separation member may or may not be physically separated, aobvious as unit
The component shown may or may not be physical unit, it can in one place.Or it may be distributed over multiple
In network unit.It can select some or all of unit therein according to the actual needs to realize the mesh of this embodiment scheme
's.
In addition, each functional unit in each embodiment of the utility model can integrate in one processing unit,
It can be each unit to physically exist alone, can also be integrated in one unit with two or more units.
It, can be with if the function is realized in the form of SFU software functional unit and when sold or used as an independent product
It is stored in a computer-readable access to memory.Based on this understanding, the technical solution of the utility model substantially or
Say that the part of the part that contributes to existing technology or the technical solution can be embodied in the form of software products, it should
Computer software product is stored in a memory, including some instructions are used so that a computer equipment (can be a
People's computer, server or network equipment etc.) execute all or part of step of each embodiment the method for the utility model
Suddenly.And memory above-mentioned includes: USB flash disk, mobile hard disk, read-only memory (ROM, Read-OnlyMemory).Arbitrary access is deposited
The various media that can store program ver-ify code such as reservoir (RAM, Random, Access, Memory), magnetic or disk.
The above embodiments of the present invention can be combined with each other, and have corresponding technical effect.
The above is only the preferred embodiment of the utility model only, is not intended to limit the utility model, all at this
Within the spirit and principle of utility model, any modification, equivalent replacement, improvement and so on should be included in the utility model
Protection scope within.
What patent application claims were submitted on 08 06th, 2018, application No. is 201810884735.3, application is artificial
Peking blue arrow space Science and Technology Ltd., the China of utility model entitled " the middle section hold-up interception method and system of ballistic missile " is specially
The priority of benefit application, the full text of this application are herein incorporated by reference in the application.
Claims (10)
1. a kind of missile intercept device characterized by comprising signal receiver, controller, propulsive mechanism, ammunition dispense mechanism；
Wherein the ammunition dispenses mechanism storage primary and secondary ammunition；
The signal receiver is for receiving igniting command signal, and the controller in the signal receiver for receiving a little
The propulsive mechanism igniting is controlled when fiery command signal, to push missile intercept device to enter pre-set flight trajectory；
The controller dispenses the mechanism release primary and secondary ammunition described in being also used to control in the pre-set flight trajectory, to be formed
The primary and secondary ammunition group of target is attacked for intercepting.
2. missile intercept device according to claim 1, which is characterized in that the primary and secondary ammunition equipped with time-delay fuze and/or
Contact fuze, the controller attack target for controlling and quick-fried to attack the shrapnel efficacy-enhancing ingredient that target crosses to destroy.
3. missile intercept device according to claim 1, which is characterized in that missile intercept device further includes detector, the spy
Device is surveyed for detecting to attack the bounds of target；The controller is used to control the ammunition according to the bounds and dispense
Primary and secondary ammunition is launched by mechanism.
4. missile intercept device according to claim 3, which is characterized in that the pre-set flight trajectory with come attack target fly
Row trajectory is at least partly overlapped；
The controller control ammunition dispenses mechanism and launches primary and secondary before missile intercept device is contacted with the bounds
Ammunition, so that the primary and secondary ammunition attacks target relative movement with described along the intersection, and the controller controls
The primary and secondary ammunition is ignited when at least partly intersecting with the bounds.
5. missile intercept device according to claim 4, which is characterized in that the detector is for boundary described in real-time detection
Range, the controller launches primary and secondary ammunition according to the shape and change in shape of the bounds, thus the primary and secondary being launched
Ammunition is attacked target with described with the first 3D shape and is moved toward one another, and the controller control the primary and secondary ammunition group with
The bounds at least 50% are ignited when intersecting each other.
6. missile intercept device according to claim 5, which is characterized in that first 3D shape is opening described in
The diamond shape and axis of target are attacked to attack the umbrella shape of guided missile, cone towards described to attack the taper of target, water chestnut towards described
At least one of the consistent cylinder in trajectory direction of target is attacked with described.
7. missile intercept device according to claim 6, which is characterized in that first 3D shape is at least in two spaces
Size in dimension is greater than the bounds.
8. according to the described in any item missile intercept devices of claim 4-7, which is characterized in that
The controller controls primary and secondary ammunition ignition when the registration with the bounds reaches maximum, to destroy place
Suspicious object in the bounds.
9. according to the described in any item missile intercept devices of claim 4-7, which is characterized in that
The detector is for the movement speed and change in shape of bounds in space described in real-time detection, the controller
According to the movement speed and change in shape, calculate the delivering opportunity of the primary and secondary ammunition, launch interval, launch batch and
The quantity for the primary and secondary ammunition launched in each batch；
The controller control ammunition dispenses mechanism and is spaced, release batch, is criticized each time according to the delivering opportunity, dispensing
The quantity of the primary and secondary ammunition of secondary middle dispensing launches primary and secondary ammunition to the bounds.
10. missile intercept device according to claim 9, which is characterized in that the detector is also used to detect the interception
The relative velocity of device and the bounds and relative position, so that the controller is according to the relative velocity and described opposite
Ammunition described in position control dispenses mechanism and launches primary and secondary ammunition.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2018108847353 | 2018-08-06 | ||
| CN201810884735.3A CN109141128A (en) | 2018-08-06 | 2018-08-06 | The middle section hold-up interception method and system of ballistic missile |
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| Publication Number | Publication Date |
|---|---|
| CN209588843U true CN209588843U (en) | 2019-11-05 |
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| CN201810884735.3A Pending CN109141128A (en) | 2018-08-06 | 2018-08-06 | The middle section hold-up interception method and system of ballistic missile |
| CN202011156095.8A Active CN112179213B (en) | 2018-08-06 | 2019-01-08 | Missile interception method, memory and server |
| CN201910226366.3A Active CN110145969B (en) | 2018-08-06 | 2019-01-08 | Missile interception method and server |
| CN201920023397.4U Active CN209588843U (en) | 2018-08-06 | 2019-01-08 | Missile intercept device |
| CN201910014107.4A Active CN109631675B (en) | 2018-08-06 | 2019-01-08 | Missile interceptor |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201810884735.3A Pending CN109141128A (en) | 2018-08-06 | 2018-08-06 | The middle section hold-up interception method and system of ballistic missile |
| CN202011156095.8A Active CN112179213B (en) | 2018-08-06 | 2019-01-08 | Missile interception method, memory and server |
| CN201910226366.3A Active CN110145969B (en) | 2018-08-06 | 2019-01-08 | Missile interception method and server |
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| CN201910014107.4A Active CN109631675B (en) | 2018-08-06 | 2019-01-08 | Missile interceptor |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN109631675A (en) * | 2018-08-06 | 2019-04-16 | 北京蓝箭空间科技有限公司 | Missile intercept device |
| CN114148520A (en) * | 2021-11-26 | 2022-03-08 | 航空工业信息中心 | Low-cost folding wing interceptor, machine group and method for intercepting attacking unmanned machine group |
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| CN111220034B (en) * | 2019-12-10 | 2022-05-31 | 李新其 | Intelligent evading method for small-thrust multiple-track transfer of controllable maneuvering warhead |
| CN110906795B (en) * | 2019-12-13 | 2022-07-05 | 谢勋 | Middle section interception missile, system and method |
| CN111141180B (en) * | 2020-01-09 | 2022-07-19 | 中国人民解放军海军大连舰艇学院 | Interception target method based on division of plane launching area of naval vessel formation naval-air missile |
| CN112325704B (en) * | 2020-10-20 | 2022-07-29 | 中国人民解放军海军工程大学 | Unmanned aerial vehicle-mounted optical fiber laser false target and use method thereof |
| CN113376612B (en) * | 2021-08-12 | 2021-11-23 | 成都众享天地网络科技有限公司 | Radar clutter generation method based on terrain matrixing and detection |
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| CN109631675A (en) * | 2018-08-06 | 2019-04-16 | 北京蓝箭空间科技有限公司 | Missile intercept device |
| CN109631675B (en) * | 2018-08-06 | 2024-03-26 | 蓝箭航天空间科技股份有限公司 | Missile interceptor |
| CN114148520A (en) * | 2021-11-26 | 2022-03-08 | 航空工业信息中心 | Low-cost folding wing interceptor, machine group and method for intercepting attacking unmanned machine group |
Also Published As
| Publication number | Publication date |
|---|---|
| CN110145969B (en) | 2020-10-27 |
| CN109631675B (en) | 2024-03-26 |
| CN109141128A (en) | 2019-01-04 |
| CN110145969A (en) | 2019-08-20 |
| CN112179213A (en) | 2021-01-05 |
| CN112179213B (en) | 2022-05-27 |
| CN109631675A (en) | 2019-04-16 |
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