CN104776761A - Guided missile with pre-destroying and anti-interception functions and construction method for guided missile - Google Patents
Guided missile with pre-destroying and anti-interception functions and construction method for guided missile Download PDFInfo
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- CN104776761A CN104776761A CN201510173396.4A CN201510173396A CN104776761A CN 104776761 A CN104776761 A CN 104776761A CN 201510173396 A CN201510173396 A CN 201510173396A CN 104776761 A CN104776761 A CN 104776761A
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- guided missile
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Abstract
The invention discloses a guided missile with pre-destroying and anti-interception functions and a construction method for the guided missile. The guided missile mainly comprises a guided missile body, a pre-destroying and anti-interception body and a guide cover, wherein the guided missile body further comprises a guide head, a battle part, an auxiliary device, a front fin, a propelling device and a tail fin. The guided missile with pre-destroying and anti-interception functions has the characteristics of being simple to construct, obvious in resisting opposite-side interferences and intercepting effect, and relatively low in cost, a pre-destroying and anti-interception device can be driven to work as long as the guided missile flies and gets close to a target or an attacked part is sensed to be interfered and intercepted, the pre-destroying and anti-interception functions of the guided missile body before an attack are realized due to the fact that barrage is formed in front of the guided missile, so that the viability of the guided missile before the attack and the destroying effects of the guided missile in attack are improved, not only can the guided missile be applied to upgrading and modifying a current large-diameter guided missile, but also an additional protective and attack means can be provided for developing a novel large-diameter guided missile.
Description
Technical field
The present invention relates to a kind of guided missile, more particularly, relate to a kind of guided missile and the constructive method thereof with pre-destruction and anti-interception function.
Background technology
Guided missile is that a kind of power set that rely on advance, guided by guidance system and control its flight path, and then realize the weapon of target goal, its main task the warhead of powder charge is directed to the ignition of target place injure target, or rely on self kinetic energy directly to smash target when not having warhead.Current guided missile is improve the destruction effect in the middle of the survival ability before attacking, attack, and kills and wounds successful probability, and in tactics, normal employing many pieces of guided missiles hit a target; Technically, usually adopt continuous conversion or improvement aiming means, change warhead explosive manner and improve warhead brisance, and the counter such as interference, interception that raising guided missile self flying speed is dealt with by attacker implements is taken action.But the development of these technology application is close to extreme, cause existing missilery research and development, produce and the difficulty of application aspect increasing, and cost is also more and more higher.Namely from aspects such as financial cost, tactical effect and formation fighting capacity cycles, particularly running under the counter capabilities might being had stronger interference and interception by attacker, the guided missile its own existence ability implementing to attack can be caused relatively to weaken, if use guided missile to hit a target in large quantities, neither calculate, differ again and obtain the damage effectiveness that strikes target preferably surely.
Summary of the invention
In view of known technology Problems existing, the present invention aims to provide a kind of simplicity of design, scientific structure, effectively can overcome the method that existing guided missile exists above-mentioned defect.
To achieve these goals, the present invention specifically provides a kind of missilery scheme with destruction in advance and anti-interception function, comprises Missile Body, pre-destruction and anti-blocking apparatus, kuppe formation;
Described Missile Body mainly also comprises seeker, warhead, servicing unit, front wing, propulsion plant, empennage;
Described pre-destruction and anti-blocking apparatus, be attached on Missile Body, and be connected with the servicing unit in described Missile Body further;
Described kuppe is attached to described pre-destruction and anti-blocking apparatus is peripheral, and is connected on described Missile Body, for reducing missile flight resistance.
Preferably, for described pre-destruction and anti-blocking apparatus, adopt miniature missile.
Preferably, for described pre-destruction and anti-blocking apparatus, consider load-carrying ability and the pneumatic structure of guided missile, the miniature missile of some groups of assemblings side by side centered by Missile Body axis can be used, be beneficial to the balance of described Missile Body.
Preferably, described pre-destruction and anti-blocking apparatus, adopt pencil rocket.
Preferably, for described pre-destruction and anti-blocking apparatus, consider load-carrying ability and the pneumatic structure of guided missile, the pencil rocket of some groups of assemblings side by side centered by Missile Body axis can be used, be beneficial to the balance of described Missile Body.
Preferably, adopt the thin-wall construction containing controlled fragment for described kuppe, in order to increase Kill capability when missile armament is ignited.
The present invention also specifically provides a kind of missilery implementation with pre-destruction and anti-interception function in addition, comprises the following steps:
S100: redesign or select a bodice footpath and the stronger guided missile of load-carrying ability, correct position on described Missile Body, the pre-destruction described in loading and anti-blocking apparatus, and described servicing unit, kuppe;
S101: design and install the hardware relevant to guided missile seeker additional, there is perception whether implemented interference by attacker and tackle the function of actuating signal, approaching target distance, and can with described servicing unit, and described pre-destruction and anti-blocking apparatus realize interlock;
S102: design the software relevant with adding multiple missile seeker, in its target-seeking program, embed the control logic under 4 kinds of relevant mode of operations, namely guided missile in attack process, according to or without approaching target, with or without run into interference and interception situation, distinguish 4 kinds of conditions to carry out real-time judge, and then navigate missile enters corresponding 4 kinds of mode of operations, specifically comprises:
1) non-approaching target, the non-pattern running into interference and interception,
Reenter target-seeking program;
2) non-approaching target, run into interference and interception pattern,
Judge whether to reach the pre-destruction of guided missile and instead tackle range?
If not, then proceed to judge;
If so, then drive described servicing unit, and described pre-destruction and anti-blocking apparatus realize interlock, in order to injure interference and the interception obstacle of generation;
3) approaching target, the non-pattern running into interference and interception,
Can judge whether that the approaching target reaching guided missile attack distance?
If not, then proceed to judge;
If so, then drive described servicing unit, and described pre-destruction and anti-blocking apparatus realize interlock, merit is hit and injures target in advance, and in order to extend the time that target carries out breaking through, afterwards, conductor main body finally adds further target and injures;
4) approaching target, run into interference and interception pattern,
Judge whether to reach the approaching target distance of guided missile or destroy and instead tackle range in advance?
If not, then proceed to judge;
If so, then drive described servicing unit, and described pre-destruction and anti-blocking apparatus realize interlock, form barrage in the front of missile attack, merit is hit and injures target in advance, and produces the obstacle of interference and interception action, afterwards, conductor main body finally adds further target and injures.
The invention has the beneficial effects as follows, on existing Missile Design basis, relevant pre-destruction and anti-blocking apparatus are set, in missile target process, as long as approaching target, or perception has been carried out by attacker the action implementing interference and interception, just drive pre-destruction and anti-blocking apparatus work, namely achieve in the pre-destruction of guided missile body before attack and instead tackle function, and then the destruction effect that improve in the middle of the survival ability before missile attack and attack, not only can be applied to current conventional major diameter guided missile and rise pole transformation, also for the research and development of Novel major diameter guided missile provide a kind of additional protection and attack means, in general technical difficulty and realize cost on very not high.
Accompanying drawing explanation
Fig. 1, for having the pre-guided missile composition schematic diagram with anti-interception function that destroys.
Fig. 2, for having the pre-periphery assembling schematic diagram with a kind of specific embodiment of guided missile of anti-interception function that destroys.
Fig. 3, for having pre-destruction and the kuppe controlled fragment partial schematic diagram in the guided missile of anti-interception function.
Fig. 4, for having the pre-flow chart of steps with a kind of detailed description of the invention of guided missile of anti-interception function of destroying.
In figure, 1. Missile Body, 11. seekers, 12. warheads, 2. pre-destruction and anti-blocking apparatus, 3. kuppe, 21. servicing units, 13. front wings, 14. propulsion plants, 15. empennages.
Detailed description of the invention
Below in conjunction with accompanying drawing, describe in detail according to structure provided by the invention, characteristic sum embodiment.
As depicted in figs. 1 and 2, for having the pre-guided missile system composition schematic diagram with anti-interception function that destroys, and a kind of periphery assembling schematic diagram of specific embodiment.There is the pre-guided missile with anti-interception function that destroys, comprising:
Comprise Missile Body 1, pre-destruction and anti-blocking apparatus 2, kuppe 3 to form;
Missile Body 1 mainly also comprises seeker 11, warhead 12, servicing unit 21, front wing 13, propulsion plant 14, empennage 15;
Pre-destruction and anti-blocking apparatus 2, be attached on Missile Body 1, and be connected with the servicing unit 21 in above-mentioned Missile Body 1 further;
Kuppe 3 is attached to above-mentioned pre-destruction and anti-blocking apparatus 2 is peripheral, and is connected on above-mentioned Missile Body 1, for reducing missile flight resistance.
As one of the present invention preferably specific embodiment, for above-mentioned pre-destruction and anti-blocking apparatus 2, adopt miniature missile.
As one of the present invention preferably specific embodiment, for above-mentioned pre-destruction and anti-blocking apparatus 2, consider load-carrying ability and the pneumatic structure of guided missile, the miniature missile of some groups of assemblings side by side centered by Missile Body 1 axis can be used, be beneficial to the balance of described Missile Body 1; And the present embodiment employing is one group of miniature missile launched side by side.
As one of the present invention preferably specific embodiment, for above-mentioned pre-destruction and anti-blocking apparatus 2, adopt pencil rocket.
As one of the present invention preferably specific embodiment, for above-mentioned pre-destruction and anti-blocking apparatus 2, consider load-carrying ability and the pneumatic structure of guided missile, the pencil rocket of some groups of assemblings side by side centered by Missile Body 1 axis can be used, be beneficial to the balance of described Missile Body 1.
As shown in Figure 3, as one of the present invention preferably specific embodiment, above-mentioned kuppe 3 adopts the thin-wall construction containing controlled fragment, in order to increase Kill capability when missile armament is ignited.
As shown in Figure 4, a kind of have the pre-guided missile specific embodiment with anti-interception function that destroys, and comprises the following steps:
S100: redesign or select a bodice footpath and the stronger guided missile of load-carrying ability, correct position on above-mentioned Missile Body 1, loads above-mentioned pre-destruction and anti-blocking apparatus 2, and above-mentioned servicing unit 21, kuppe 3;
S101: design and install additional the hardware relevant to guided missile seeker 11, there is perception whether implemented interference by attacker and tackle the function of actuating signal, approaching target distance, and can with above-mentioned servicing unit 21, and described pre-destruction and anti-blocking apparatus 2 realize interlock;
S102: design and add the relevant software of multiple missile seeker 11, in its target-seeking program, embed the control logic under 4 kinds of relevant mode of operations, namely guided missile in attack process, according to or without approaching target, with or without run into interference and interception situation, distinguish 4 kinds of conditions to carry out real-time judge, and then navigate missile enters corresponding 4 kinds of mode of operations, specifically comprises:
1) non-approaching target, the non-pattern running into interference and interception,
Reenter target-seeking program;
2) non-approaching target, run into interference and interception pattern,
Judge whether to reach the pre-destruction of guided missile and instead tackle range?
If not, then proceed to judge;
If so, then drive above-mentioned servicing unit 21, and above-mentioned pre-destruction and anti-blocking apparatus 2 realize interlock, in order to injure interference and the interception obstacle of generation;
3) approaching target, the non-pattern running into interference and interception,
Can judge whether that the approaching target reaching guided missile attack distance?
If not, then proceed to judge;
If so, then drive above-mentioned servicing unit 21, and above-mentioned pre-destruction and anti-blocking apparatus 2 realize interlock, merit is hit and injures target in advance, and in order to extend the time that target carries out breaking through, afterwards, conductor main body finally adds further target and injures;
4) approaching target, run into interference and interception pattern,
Judge whether to reach the approaching target distance of guided missile or destroy and instead tackle range in advance?
If not, then proceed to judge;
If so, then drive above-mentioned servicing unit 21, and above-mentioned pre-destruction and anti-blocking apparatus 2 realize interlock, merit is hit and injures target in advance, and produces the obstacle of interference and interception action, and afterwards, conductor main body finally adds further target and injures.
Above-described embodiments of the present invention; not become the restriction of scope; if carry out various distortion or amendment to embodiment of the present invention, but still within the spirit and principles in the present invention, all should be included within claims of the present invention.
Claims (7)
1. there is the pre-guided missile with anti-interception function that destroys, it is characterized in that:
Comprise Missile Body (1), pre-destruction and anti-blocking apparatus (2), kuppe (3) to form;
Described Missile Body (1) mainly also comprises seeker (11), warhead (12), servicing unit (21), front wing (13), propulsion plant (14), empennage (15);
Described pre-destruction and anti-blocking apparatus (2), be attached on Missile Body (1), and be connected with the servicing unit (21) in described Missile Body (1) further;
Described kuppe (3) is attached to described pre-destruction and anti-blocking apparatus (2) is peripheral, and is connected on described Missile Body (1), for reducing missile flight resistance.
2., according to a kind of guided missile with pre-destruction and anti-interception function described in claim 1, it is characterized in that:
Described pre-destruction and anti-blocking apparatus (2), adopt miniature missile.
3. a kind of guided missile with pre-destruction and anti-interception function according to claim 2, is characterized in that:
Described pre-destruction and anti-blocking apparatus (2), consider load-carrying ability and the pneumatic structure of guided missile, can use the miniature missile of some groups of assemblings side by side centered by Missile Body (1) axis, be beneficial to the balance of described Missile Body (1).
4., according to a kind of guided missile with pre-destruction and anti-interception function described in claim 1, it is characterized in that:
Described pre-destruction and anti-blocking apparatus (2), adopt pencil rocket.
5. a kind of guided missile with pre-destruction and anti-interception function according to claim 4, is characterized in that:
Described pre-destruction and anti-blocking apparatus (2), consider load-carrying ability and the pneumatic structure of guided missile, can use the pencil rocket of some groups of assemblings side by side centered by Missile Body (1) axis, be beneficial to the balance of described Missile Body (1).
6., according to a kind of guided missile with pre-destruction and anti-interception function described in claim 1, it is characterized in that:
Described kuppe (3) adopts the thin-wall construction containing controlled fragment, in order to increase Kill capability when described warhead (12) is ignited.
7. there is the pre-guided missile constructive method with anti-interception function that destroys, it is characterized in that, comprise the following steps:
S100: redesign or select a bodice footpath and the stronger guided missile of load-carrying ability, (1) correct position on described Missile Body, the pre-destruction described in loading and anti-blocking apparatus (2), and described servicing unit (21), kuppe (3);
S101: design and install additional the hardware relevant to guided missile seeker (11), there is perception whether implemented interference by attacker and tackle the function of actuating signal, approaching target distance, and can with described servicing unit (21), and described pre-destruction and anti-blocking apparatus (2) realize interlock;
S102: design and add the relevant software of multiple missile seeker (11), in its target-seeking program, embed the control logic under 4 kinds of relevant mode of operations, namely guided missile in attack process, according to or without approaching target, with or without run into interference and interception situation, distinguish 4 kinds of conditions to carry out real-time judge, and then navigate missile enters corresponding 4 kinds of mode of operations, specifically comprises:
1) non-approaching target, the non-pattern running into interference and interception,
Reenter target-seeking program;
2) non-approaching target, run into interference and interception pattern,
Judge whether to reach the pre-destruction of guided missile and instead tackle range?
If not, then proceed to judge;
If so, then drive described servicing unit (21), and described pre-destruction and anti-blocking apparatus (2) realize interlock, in order to injure interference and the interception obstacle of generation;
3) approaching target, the non-pattern running into interference and interception,
Can judge whether that the approaching target reaching guided missile attack distance?
If not, then proceed to judge;
If so, then drive described servicing unit (21), and described pre-destruction and anti-blocking apparatus (2) realize interlock, merit is hit and injures target in advance, in order to extend the time that target carries out breaking through, afterwards, conductor main body finally adds further target and injures;
4) approaching target, run into interference and interception pattern,
Judge whether to reach the approaching target distance of guided missile or destroy and instead tackle range in advance?
If not, then proceed to judge;
If so, then drive described servicing unit (21), and described pre-destruction and anti-blocking apparatus (2) realize interlock, merit is hit and injures target in advance, and produce the obstacle of interference and interception action, afterwards, conductor main body finally adds further target and injures.
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| Application Number | Priority Date | Filing Date | Title |
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| CN201510173396.4A CN104776761A (en) | 2015-04-14 | 2015-04-14 | Guided missile with pre-destroying and anti-interception functions and construction method for guided missile |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201510173396.4A CN104776761A (en) | 2015-04-14 | 2015-04-14 | Guided missile with pre-destroying and anti-interception functions and construction method for guided missile |
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| CN104776761A true CN104776761A (en) | 2015-07-15 |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109682257A (en) * | 2018-09-13 | 2019-04-26 | 西安理工大学 | A kind of Cruise Missile Interception device based on netting capture |
| CN109708535A (en) * | 2019-01-28 | 2019-05-03 | 西安深瞳智控技术有限公司 | A kind of coaxial double-oar tail portion push type miniature missile |
| CN114502907A (en) * | 2019-07-31 | 2022-05-13 | Bae系统信息和电子系统集成有限公司 | Wing-mounted seeker |
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| CN109682257A (en) * | 2018-09-13 | 2019-04-26 | 西安理工大学 | A kind of Cruise Missile Interception device based on netting capture |
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| CN114502907B (en) * | 2019-07-31 | 2023-06-16 | Bae系统信息和电子系统集成有限公司 | Wing mounted seeker |
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