CN111121536A - Shooting opportunity conflict resolution method for dual-ship vertical-launching first-launch naval-aircraft missile - Google Patents
Shooting opportunity conflict resolution method for dual-ship vertical-launching first-launch naval-aircraft missile Download PDFInfo
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Abstract
The embodiment of the invention discloses a method for clearing shooting opportunity conflicts of first-launched ship-air missiles with double-ship vertical launching, which comprises the steps of S1, determining a horizontal plane shooting area of each single-ship vertical-launching ship-air missile, wherein the horizontal plane shooting area of the single-ship vertical-launching ship-air missile is determined through a horizontal plane shooting area of the single-ship vertical-launching ship-air missile; s2, comparing the distance value between the two ships with the far-limit value of the horizontal plane launching area of the two-ship vertically launched ship-borne missile; and S3, adjusting the shooting time of the first ship air-borne missile vertically launched by the two single ships based on the set digestion mechanism. The invention can determine the shooting target time and sequence of the first ship air-borne missile vertically launched by the double ships when the shooting time conflicts occur under the condition that the double ships vertically launch the first ship air-borne missile to shoot the air target, thereby effectively eliminating the potential safety hazard of the first ship air-borne missile vertically launched by the double ships and ensuring the safe shooting of the first ship air-borne missile vertically launched by the double ships.
Description
Technical Field
The invention relates to the technical field of ship-air missile weapons, in particular to a shooting opportunity conflict resolution method for a first-launched ship-air missile launched by two ships vertically.
Background
When the dual-ship vertical launching first-ship air-borne missile shoots to attack air targets such as anti-ship missiles, airplanes and the like, if the shooting areas of the dual-ship vertical launching first-ship air-borne missiles are overlapped, shooting opportunity conflicts of the dual-ship vertical launching first-ship air-borne missile exist, if the shooting opportunity conflict resolution of the dual-ship vertical launching first-ship air-borne missile cannot be effectively implemented, shooting potential safety hazards such as mutual collision and accidental injury of the dual-ship vertical launching first-ship air-borne missiles exist, and the shooting target effect of the dual-ship vertical launching first-ship air-borne missile is influenced.
At present, a technology for effectively solving the shooting time conflict of the first-launched ship-air missile launched by two ships vertically is not found.
Disclosure of Invention
Based on the above, in order to solve the defects existing in the prior art when the shooting opportunity conflicts of the dual-ship vertical launching first ship air-borne missile, a method for clearing the shooting opportunity conflicts of the dual-ship vertical launching first ship air-borne missile is provided.
A shooting opportunity conflict resolution method for a dual-ship vertical-launching first-ship air-borne missile comprises the following steps:
s1, determining a horizontal plane shooting area of the single-ship vertical launching aircraft-based missile, wherein the horizontal plane shooting area of the single-ship vertical launching aircraft-based missile is determined through a horizontal plane launching area of the single-ship vertical launching aircraft-based missile;
s2, comparing the distance value between the two ships with a remote boundary value of a horizontal plane launching area of the two-ship vertically-launched naval missile, wherein the remote boundary value of the horizontal plane launching area of the two-ship vertically-launched naval missile comprises a remote boundary value of a horizontal plane launching area of a first single-ship vertically-launched naval missile and a remote boundary value of a horizontal plane launching area of a second single-ship vertically-launched naval missile;
s3, adjusting the shooting time of the first ship air-borne missile vertically launched by the two single ships based on the set digestion mechanism; and determining the shooting time and the shooting sequence of the first ship-based air-borne missile by the method.
Optionally, in one embodiment, the resolution mechanism is formed by a resolution scheme corresponding to a plurality of comparison results, where the comparison results refer to a size relationship between a relative position relationship of a horizontal plane shooting area of the dual-ship vertical-launch aircraft missile, that is, a dual-ship distance value, and a far-limit value of a horizontal plane launching area of the first single-ship vertical-launch aircraft missile and a far-limit value of a horizontal plane launching area of the second single-ship vertical-launch aircraft missile.
Optionally, in one embodiment, the resolution mechanism includes:
if the distance values between the two ships are larger than the far-limit value of the horizontal plane launching area of the first single-ship vertically-launched aircraft missile and the far-limit value of the horizontal plane launching area of the second single-ship vertically-launched aircraft missile; judging whether the incoming air target is located in a curved surface of an overlapping area of a horizontal plane launching area of a first single-ship vertical launching aircraft-borne missile and a horizontal plane launching area of a second single-ship vertical launching aircraft-borne missile, and enabling a later-launched single-ship vertical launching aircraft-borne missile to firstly shoot the target in the curved surface after a certain delay time, wherein the delay time is the sum of the average time required by the earlier-launched single-ship vertical launching aircraft-borne missile to reach the remote boundary value of the horizontal plane launching area of the corresponding vertical launching aircraft-borne missile and the weapon operational response time corresponding to the later-launched single-ship vertical launching aircraft-borne missile; if the distance values between the two ships are smaller than the far-limit value of the horizontal plane launching area of the first single-ship vertically-launched aircraft missile and the far-limit value of the horizontal plane launching area of the second single-ship vertically-launched aircraft missile, enabling the later-launched single-ship vertically-launched aircraft missile to firstly shoot the curved surface inner target after the delay time; if the distance value between the two ships is between the far-limit value of the horizontal plane launching area of the first single-ship vertical launching aircraft-borne missile and the far-limit value of the horizontal plane launching area of the second single-ship vertical launching aircraft-borne missile, judging whether an approaching aerial target is not located in a first area curved surface, and enabling a later-launched single-ship vertical launching aircraft-borne missile to firstly shoot the target in the curved surface after the delay time, wherein the first area curved surface is a curved surface area formed by a plurality of intersection points, and the intersection points comprise: the system comprises a first single-ship launching point, a second single-ship launching point, a directional line segment and an extension line, wherein the directional line segment is formed by the first single-ship launching point and takes the first single-ship launching point as a starting point, and the second single-ship launching point as an end point.
In addition, in order to solve the defects of the traditional technology, a shooting opportunity conflict resolution system for the first-launched ship-air missile launched by the double-ship vertical launch is also provided.
A shooting opportunity conflict resolution system for a dual-ship vertical-launching first-launch naval-aircraft missile comprises:
the first data acquisition unit is used for determining a horizontal plane shooting area of each single-ship vertical-launch aircraft-based missile, and the horizontal plane shooting area of the single-ship vertical-launch aircraft-based missile is determined by the horizontal plane shooting area of the single-ship vertical-launch aircraft-based missile;
the second data acquisition unit is used for comparing the distance value between the two ships with a remote boundary value of a horizontal plane launching area of the two-ship vertically-launched naval missile, wherein the remote boundary value of the horizontal plane launching area of the two-ship vertically-launched naval missile comprises a remote boundary value of a horizontal plane launching area of a first single-ship vertically-launched naval missile and a remote boundary value of a horizontal plane launching area of a second single-ship vertically-launched naval missile;
and the data output unit is used for adjusting the shooting time of the first ship vertically launching the first ship air-borne missile based on the set digestion mechanism, and further determining the shooting time and the shooting sequence of the first ship air-borne missile through the method.
Optionally, in one embodiment, the resolution mechanism is formed by a resolution scheme corresponding to a plurality of comparison results, where the comparison results refer to a size relationship between a relative position relationship of a horizontal plane shooting area of the dual-ship vertical-launch aircraft missile, that is, a dual-ship distance value, and a far-limit value of a horizontal plane launching area of the first single-ship vertical-launch aircraft missile and a far-limit value of a horizontal plane launching area of the second single-ship vertical-launch aircraft missile.
Optionally, in one embodiment, the resolution mechanism includes:
if the distance values between the two ships are larger than the far-limit value of the horizontal plane launching area of the first single-ship vertically-launched naval missile and the far-limit value of the horizontal plane launching area of the second single-ship vertically-launched naval missile; judging whether the incoming air target is located in a curved surface of an overlapping area of a horizontal plane launching area of a first single-ship vertical launching aircraft-borne missile and a horizontal plane launching area of a second single-ship vertical launching aircraft-borne missile, and enabling a later-launched single-ship vertical launching aircraft-borne missile to firstly shoot the target in the curved surface after a certain delay time, wherein the delay time is the sum of the average time required by the earlier-launched single-ship vertical launching aircraft-borne missile to reach the remote boundary value of the horizontal plane launching area of the corresponding vertical launching aircraft-borne missile and the weapon operational response time corresponding to the later-launched single-ship vertical launching aircraft-borne missile; if the distance values between the two ships are smaller than the far-limit value of the horizontal plane launching area of the first single-ship vertically-launched aircraft missile and the far-limit value of the horizontal plane launching area of the second single-ship vertically-launched aircraft missile, enabling the later-launched single-ship vertically-launched aircraft missile to firstly shoot the curved surface inner target after the delay time; if the distance value between the two ships is between the far-limit value of the horizontal plane launching area of the first single-ship vertical launching aircraft-borne missile and the far-limit value of the horizontal plane launching area of the second single-ship vertical launching aircraft-borne missile, judging whether an approaching aerial target is not located in a first area curved surface, and enabling a later-launched single-ship vertical launching aircraft-borne missile to firstly shoot the target in the curved surface after the delay time, wherein the first area curved surface is a curved surface area formed by a plurality of intersection points, and the intersection points comprise: the system comprises a first single-ship launching point, a second single-ship launching point, a directional line segment and an extension line, wherein the directional line segment is formed by the first single-ship launching point and takes the first single-ship launching point as a starting point, and the second single-ship launching point as an end point.
In addition, in order to solve the disadvantages of the conventional technology, a computer-readable storage medium is provided, which includes computer instructions, when the computer instructions are executed on a computer, the computer executes the method.
The embodiment of the invention has the following beneficial effects:
the invention provides a method for resolving shooting opportunity conflict of a dual-ship vertical-launch first-launch aircraft-based missile, which can determine the shooting target opportunity and the shooting target sequence of the dual-ship vertical-launch first-launch aircraft-based missile when the shooting opportunity conflict occurs under the condition that the dual-ship vertical-launch aircraft-based missile strikes an aerial target, effectively eliminate the potential safety hazard of the dual-ship vertical-launch first-launch aircraft-based missile, and ensure the shooting safety of the dual-ship vertical-launch first-launch aircraft-based missile.
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In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to the drawings without creative efforts.
Wherein:
FIG. 1 is a technical flow chart of an embodiment of a method for resolving a conflict of shooting time of a dual-ship vertical launching first-ship air-borne missile;
fig. 2 is a diagram of a launching area of an aircraft water guide plane of a single ship vertical launching ship and a horizontal plane shooting area in one embodiment;
FIG. 3 is a diagram of relative position of a horizontal plane firing zone in the case where both of the values of the inter-ship distances are greater than the far-limit value of the horizontal plane firing zone of the dual-ship vertically launched naval missile in one embodiment;
FIG. 4 is a diagram of relative position of a horizontal plane firing zone in the case where both of the values of the spacing between the two vessels are smaller than the far boundary value of the horizontal plane firing zone of the two-vessel vertically launched naval missile in one embodiment;
fig. 5 is a diagram of the relative position relationship of the horizontal plane firing zone in the case that the distance value between two vessels is between the far boundary values of the horizontal plane firing zones of the two-vessel vertical-firing aircraft missile in one embodiment.
Detailed Description
In order to make the objects, technical solutions and advantages of the present invention more apparent, the present invention is described in further detail below with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are merely illustrative of the invention and are not intended to limit the invention.
Unless defined otherwise, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this invention belongs. The terminology used in the description of the invention herein is for the purpose of describing particular embodiments only and is not intended to be limiting of the invention. It will be understood that, as used herein, the terms "first," "second," and the like may be used herein to describe various elements, but these elements are not limited by these terms. These terms are only used to distinguish one element from another. For example, a first element could be termed a second element, and, similarly, a second element could be termed a first element, without departing from the scope of the present application. The first and second elements are both elements, but they are not the same element.
When the double-ship vertical launching aircraft-based missile strikes an aerial target, the target in the aircraft-based missile launching area can be shot only, and the aircraft-based missile launching area is a space formed by all target positions encountered by the aircraft-based missile in the target killing area at the moment when the aircraft-based missile weapon launches the missile. That is, when a target enters the launching zone of an aircraft missile to launch the missile, the aircraft missile encounters the target in the killing zone. The naval-aircraft missile killing area refers to the space range of naval-aircraft missile weapons for killing air targets with given probability. The vertical section and the horizontal section of the launching area of the naval vessel missile are respectively called as a vertical plane launching area and a horizontal plane launching area. When the horizontal plane launching areas of the two-ship vertical launching aircraft guided missiles are overlapped, the vertical plane launching areas are overlapped certainly, and the shooting time conflict of the first-launching aircraft guided missiles launched by the two-ship vertical launching aircraft guided missiles is determined to exist. When the vertical plane launching areas of the dual-ship vertical launching aircraft-borne missiles are not overlapped, the horizontal plane launching areas of the dual-ship vertical launching aircraft-borne missiles are possibly overlapped, and shooting opportunity conflicts of the dual-ship vertical launching aircraft-borne missiles can exist, so that the dual-ship vertical launching aircraft-borne missiles can be mainly used through the horizontal plane launching areas, based on the principle, in the embodiment, the method for clearing the shooting opportunity conflicts of the dual-ship vertical launching aircraft-borne missiles is specially provided, so that when the shooting opportunity conflicts occur under the condition that the dual-ship vertical launching aircraft-borne missiles are shot to attack the air targets, the shooting opportunity of the dual-ship vertical launching aircraft-borne missiles is determined, the potential safety hazards of the dual-ship vertical launching aircraft-borne missiles are eliminated; as shown in fig. 1, the method comprises the steps of:
s1, determining a horizontal plane shooting area of the single-ship vertical launching aircraft-based missile, wherein the horizontal plane shooting area of the single-ship vertical launching aircraft-based missile is determined through a horizontal plane launching area of the single-ship vertical launching aircraft-based missile; the horizontal plane shooting area of the single-ship vertical-launch aircraft guided missile refers to the horizontal plane area of the single-ship vertical-launch aircraft guided missile capable of shooting the target. Because the single-ship vertical-launch aircraft-borne missile can intercept 360-degree omnibearing targets, the horizontal plane launching area of the single-ship vertical-launch aircraft-borne missile can be expressed by taking a point O as the center of a circle and a radius (R)1，R2AI represents the course line, see fig. 2; for the purposes of this description, the radius R is taken to be the center of the point O1The circle does not belong to the horizontal plane launching area of the single-ship vertical launching aircraft guided missile, but because the single-ship vertical launching aircraft guided missile flies R after being launched from the point O position1The distance can reach the corresponding near boundary of the horizontal plane launching area, and the circle and the horizontal plane launching area of the single-ship vertical launching naval missile jointly form an area, namely, the point O is taken as the circle center, and the radius is R2The circle of (2) is the horizontal plane launching area of the single-ship vertical launching aircraft missile, and is shown in figure 2.
S2, comparing the distance value between the two ships with a remote boundary value of a horizontal plane launching area of the two-ship vertically-launched naval missile, wherein the remote boundary value of the horizontal plane launching area of the two-ship vertically-launched naval missile comprises a remote boundary value of a horizontal plane launching area of a first single-ship vertically-launched naval missile and a remote boundary value of a horizontal plane launching area of a second single-ship vertically-launched naval missile; in some specific embodiments, when conflict resolution is performed on the fire firing opportunity of the dual-ship vertical launching first-ship aircraft missile, the fire firing opportunity of the dual-ship vertical launching first-ship aircraft missile needs to be determined according to the relative position relationship of the horizontal plane firing area of the dual-ship vertical launching first-ship aircraft missile; the specific relative position relation of the horizontal plane shooting area of the double-ship vertical launching aircraft guided missile mainly comprises the following 3 conditions; case 1: the distance values between the two ships are both greater than the far-limit value of the horizontal plane launching area of the first single-ship vertically-launched aircraft missile and the far-limit value of the horizontal plane launching area of the second single-ship vertically-launched aircraft missile; case 2: the distance values between the two ships are smaller than the far-limit value of the horizontal plane launching area of the first single-ship vertically-launched aircraft guided missile and the far-limit value of the horizontal plane launching area of the second single-ship vertically-launched aircraft guided missile; case 3: the distance value between the two ships is between the far-limit value of the horizontal plane launching area of the first single-ship vertical launching aircraft guided missile and the far-limit value of the horizontal plane launching area of the second single-ship vertical launching aircraft guided missile.
And S3, adjusting the shooting time of the first ship air-borne missile vertically launched by the two single ships based on the set digestion mechanism. And determining the shooting time and the shooting sequence of the first ship-based air-borne missile by the method.
In some specific embodiments, the resolution mechanism is composed of resolution schemes corresponding to a plurality of comparison results, and the comparison results refer to the size relationship between the relative position relationship of the horizontal plane shooting areas of the dual-ship vertical launching aircraft-borne missiles, namely the dual-ship distance value, and the far boundary value of the horizontal plane launching area of the first single-ship vertical launching aircraft-borne missiles and the far boundary value of the horizontal plane launching area of the second single-ship vertical launching aircraft-borne missiles. In some more specific embodiments, the resolution mechanism comprises: if the distance values between the two ships are larger than the far-limit value of the horizontal plane launching area of the first single-ship vertically-launched aircraft missile and the far-limit value of the horizontal plane launching area of the second single-ship vertically-launched aircraft missile; judging whether the incoming air target is located in a curved surface of an overlapping area of a horizontal plane launching area of a first single-ship vertical launching aircraft-borne missile and a horizontal plane launching area of a second single-ship vertical launching aircraft-borne missile, and enabling a later-launched single-ship vertical launching aircraft-borne missile to firstly shoot the target in the curved surface after a certain delay time, wherein the delay time is the sum of the average time required by the earlier-launched single-ship vertical launching aircraft-borne missile to reach the remote boundary value of the horizontal plane launching area of the corresponding vertical launching aircraft-borne missile and the weapon operational response time corresponding to the later-launched single-ship vertical launching aircraft-borne missile; if the distance values between the two ships are smaller than the far-limit value of the horizontal plane launching area of the first single-ship vertically-launched aircraft missile and the far-limit value of the horizontal plane launching area of the second single-ship vertically-launched aircraft missile, enabling the later-launched single-ship vertically-launched aircraft missile to firstly shoot the curved surface inner target after the delay time; if the distance value between the two ships is between the far-limit value of the horizontal plane launching area of the first single-ship vertical launching aircraft-borne missile and the far-limit value of the horizontal plane launching area of the second single-ship vertical launching aircraft-borne missile, judging whether an approaching aerial target is not located in a first area curved surface, and enabling a later-launched single-ship vertical launching aircraft-borne missile to firstly shoot the target in the curved surface after the delay time, wherein the first area curved surface is a curved surface area formed by a plurality of intersection points, and the intersection points comprise: the system comprises a first single-ship launching point, a second single-ship launching point, a directional line segment and an extension line, wherein the directional line segment is formed by the first single-ship launching point and takes the first single-ship launching point as a starting point, and the second single-ship launching point as an end point.
Based on the above design principle, the corresponding embodiments are as follows:
case 1: the distance values between the two ships are all larger than the far-limit value of the horizontal plane launching area of the two-ship vertical launching naval missile, wherein AxqThe ship is a first single ship, BxqThe ship is a second single ship; the relative position relation of the horizontal plane shooting area of the double-ship vertical-launching aircraft guided missile under the condition is that the distance values between the double ships are both larger than the far boundary value of the horizontal plane launching area of the double-ship vertical-launching aircraft guided missile, namely | A |yBy|＞RAy、|AyBy|＞RBySee fig. 3. Then the horizontal plane shooting area of the double-ship vertical launching aircraft missile can be divided into: overlap region curved surface Jy1Jy5Jy2Jy6Non-overlapping area curved surface Jy1Jy5Jy2Jy3And curved surface Jy1Jy6Jy2Jy4. And respectively implementing different digestion schemes according to the position relation between the three curved surfaces and the target in the coming air.
(1) Non-overlapping area curved surface Jy1Jy5Jy2Jy3
The curved surface is only located at AxqIn the horizontal plane area of the ship vertically-launched ship-air missile, when AxqWhen the ship vertical-launching air-borne missile carries out first-shot shooting on the air target attacking the curved surface, the ship vertical-launching air-borne missile cannot be subjected to BxqThe ship vertical-launching aircraft missile weapon has the effect of carrying out first-launch shooting on the target in the horizontal plane shooting area, so that the shooting time conflict of the double-ship vertical-launching aircraft missile at the moment does not exist, and once the target appears in the curved surface, AxqThe ship vertical launching ship-air missile weapon can immediately implement a first launching target;
(2) non-overlapping area curved surface Jy1Jy6Jy2Jy4
The curved surface is only located at BxqIn the horizontal plane area of the ship vertically-launched ship-air missile, when BxqWhen the ship vertical-launching air-borne missile carries out first-shot shooting on an air target attacking in the curved surface, the air-borne missile cannot be subjected to AxqThe ship vertical-launching aircraft missile weapon has the effect of carrying out first-launch shooting on the target in the horizontal plane shooting area, so that the shooting time conflict of the double-ship vertical-launching aircraft missile at the first-launch aircraft missile does not exist, and once the target appears in the curved surface, BxqThe ship vertical launching ship-air missile weapon can immediately implement a first launching target;
(3) overlap region curved surface Jy1Jy5Jy2Jy6
The curved surface is simultaneously positioned in a horizontal plane shooting area of the dual-ship vertical launching aircraft guided missile, the horizontal plane shooting areas of the dual-ship vertical launching aircraft guided missiles are overlapped, and shooting opportunity conflict and dual-ship vertical launching aircraft guided missiles of the first launching aircraft guided missile existThe method for clearing the firing opportunity conflict of the first warship aircraft missile comprises the following steps: if A isxqFirstly, the warship vertical-launching ship-air missile weapon carries out first-shot shooting on an approaching aerial target in the curved surface, and then BxqWarship vertical launching naval missile weapon needs to wait tAy+tBfThe target in the curved surface can be shot firstly after the time. Secondly, if B isxqThe ship vertically-launched air-borne missile weapon carries out first-shot shooting on an approaching air target in the curved surface, and A isxqWarship vertical launching naval missile weapon needs to wait tBy+tafThe target in the curved surface can be shot firstly after the time. Wherein, tAy＝RAy/VAy,tBy＝RBy/VBy。
Case 2: the distance values between the two ships are smaller than the far-limit value of the horizontal plane launching area of the two-ship vertically launched naval missile; the relative position relation of the horizontal plane shooting area of the double-ship vertical-launching aircraft guided missile under the condition is that the distance values between the double ships are smaller than the far boundary value of the horizontal plane launching area of the double-ship vertical-launching aircraft guided missile, namely | A |yBy|＜RAy、|AyBy|＜RBySee fig. 4. The overlapping area of the horizontal plane shooting area of the double-warship vertical-launching aircraft guided missile is a curved surface Jy1Jy5Jy2Jy6Non-overlapping area curved surface Jy1Jy5Jy2Jy3And curved surface Jy1Jy6Jy2Jy4. From these three surfaces, different resolution schemes are implemented.
(1) Non-overlapping area curved surface Jy1Jy5Jy2Jy3
Although the curved surface is located at A onlyxqWarship vertically launches air-borne missiles in the horizontal plane area, but when A isxqWhen the ship vertical-launching air-borne missile carries out first-shot shooting on an air target attacking in the curved surface, the ship vertical-launching air-borne missile is subjected to BxqThe impact of the ship vertical-launching aircraft missile weapon on the implementation of first-launch shooting of a target in a horizontal plane shooting area of the ship vertical-launching aircraft missile weapon is realized, at the moment, the double-ship vertical-launching aircraft-first-launch missile shooting opportunity conflict exists, and the conflict resolution method of the double-ship vertical-launching aircraft-first-launch missile shooting opportunity conflict is that if A is the first time, the first time is thatxqFirstly, the warship vertical-launching ship-air missile weapon carries out first-shot shooting on an approaching aerial target in the curved surface, and then BxqWarship vertical launching naval missile weapon needs to wait tAy+tBfThe target in the curved surface can be shot firstly after the time. Secondly, if B isxqThe ship vertically-launched air-borne missile weapon carries out first-shot shooting on an approaching air target in the curved surface, and A isxqWarship vertical launching naval missile weapon needs to wait tBy+tafThe target in the curved surface can be shot firstly after the time. Wherein, tAy＝RAy/VAy,tBy＝RBy/VBy。
(2) Non-overlapping area curved surface Jy1Jy6Jy2Jy4
Although the curved surface is located only at BxqWarship vertically launches air-borne missiles in the horizontal plane area, but when BxqWhen the ship vertical-launching air-borne missile carries out first-shot shooting on an air target attacking in the curved surface, the ship vertical-launching air-borne missile is subjected to AxqThe impact of the ship vertical-launching aircraft missile weapon on the implementation of first-launch shooting of a target in a horizontal plane shooting area of the ship vertical-launching aircraft missile weapon is solved if the first-launch aircraft missile of the ship vertical-launching exists in the moment when the shooting opportunity conflict exists, and the shooting opportunity conflict resolution method of the first-launch aircraft missile of the ship vertical-launching aircraft missile of the double ships is that if the first-launch aircraft missile of the double ships vertical-launching aircraftxqFirstly, the warship vertical-launching ship-air missile weapon carries out first-shot shooting on an approaching aerial target in the curved surface, and then BxqWarship vertical launching naval missile weapon needs to wait tBy+tafThe target in the curved surface can be shot firstly after the time. Secondly, if A isxqThe ship vertically-launched air-borne missile weapon carries out first-shot shooting on an approaching air target in the curved surface, and B isxqWarship vertical launching naval missile weapon needs to wait tAy+tBfThe target in the curved surface can be shot firstly after the time. Wherein, tAy＝RAy/VAy,tBy＝RBy/VBy。
(3) Overlap region curved surface Jy1Jy5Jy2Jy6
The curved surface is simultaneously positioned in the horizontal plane shooting area of the dual-ship vertical launching naval missileAt the moment, the horizontal plane shooting areas of the double-ship vertical-launching aircraft-borne missiles are overlapped, the shooting opportunity conflict of the double-ship vertical-launching first-launching aircraft-borne missiles exists, and the shooting opportunity conflict resolution method of the double-ship vertical-launching first-launching aircraft-borne missiles comprises the following steps: if A isxqFirstly, the warship vertical-launching ship-air missile weapon carries out first-shot shooting on an approaching aerial target in the curved surface, and then BxqWarship vertical launching naval missile weapon needs to wait tAy+tBfThe target in the curved surface can be shot firstly after the time. Secondly, if B isxqWhen the ship vertically launches the aircraft missile weapon to carry out first fire shooting on the target in the curved surface, AxqWarship vertical launching naval missile weapon needs to wait tBy+tAfThe target in the curved surface can be shot firstly after the time. t is tAy＝RAy/VAy，tBy＝RBy/VBy。
Case 3: the distance value between the two ships is between the far-limit values of the horizontal plane launching areas of the two-ship vertically launched ship-borne missiles; the relative position relation of the horizontal plane shooting area of the double-ship vertical-launching aircraft guided missile under the condition is that the distance value between the two ships is between the far boundary values of the horizontal plane launching area of the double-ship vertical-launching aircraft guided missile, namely | A |yBy|≤RAy、|AyBy|≥RBy，RAy≥RBySee figure 5. the overlapping area of the horizontal plane shooting area of the double-ship vertical launching naval missile is a curved surface Jy1Jy5Jy2Jy6Non-overlapping area curved surface Jy7Jy9Jy5Jy10Jy8Jy3、Jy1Jy7Jy9、Jy2Jy8Jy10And curved surface Jy1Jy4Jy2Jy6. From these 5 surfaces, different resolution protocols were implemented.
(1) Non-overlapping area curved surface Jy7Jy9Jy5Jy10Jy8Jy3
The curved surface is only located at AxqIn the horizontal plane area of the ship vertically-launched ship-air missile, when AxqWarship vertical-launching air-to-ship missile performs first launching on an approaching aerial target in the curved surfaceWhen hit, the hammer will not be affected by BxqThe ship vertical-launching aircraft missile weapon has the effect of carrying out first-launch shooting on the target in the horizontal plane shooting area, so that the shooting time conflict of the double-ship vertical-launching aircraft missile at the moment does not exist, and once the target appears in the curved surface, AxqThe ship vertical launching ship-air missile weapon can immediately implement a first launching target.
(2) Non-overlapping area curved surface Jy1Jy7Jy9And Jy2Jy8Jy10
Although the curved surface is located at A onlyxqWarship vertically launches air-borne missiles in the horizontal plane area, but when A isxqWhen the ship vertical-launching air-borne missile carries out first-shot shooting on an air target attacking in the curved surface, the ship vertical-launching air-borne missile is subjected to BxqThe impact of the ship vertical-launching aircraft missile weapon on the implementation of first-launch shooting of a target in a horizontal plane shooting area of the ship vertical-launching aircraft missile weapon is realized, at the moment, the double-ship vertical-launching aircraft-first-launch missile shooting opportunity conflict exists, and the conflict resolution method of the double-ship vertical-launching aircraft-first-launch missile shooting opportunity conflict is that if A is the first time, the first time is thatxqFirstly, the warship vertical-launching ship-air missile weapon carries out first-shot shooting on an approaching aerial target in the curved surface, and then BxqWarship vertical launching naval missile weapon needs to wait tAy+tBfThe target in the curved surface can be shot firstly after the time. Secondly, if B isxqThe ship vertically-launched air-borne missile weapon carries out first-shot shooting on an approaching air target in the curved surface, and A isxqWarship vertical launching naval missile weapon needs to wait tBy+tafThe target in the curved surface can be shot firstly after the time. Wherein, tAy＝RAy/VAy,tBy＝RBy/VBy。
(3) Non-overlapping area curved surface Jy1Jy4Jy2Jy6
Although the curved surface is located only at BxqWarship vertically launches air-borne missiles in the horizontal plane area, but when BxqWhen the ship vertical-launching air-borne missile carries out first-shot shooting on an air target attacking in the curved surface, the ship vertical-launching air-borne missile is subjected to AxqThe influence of the ship vertical launching aircraft missile weapon on the implementation of first firing on targets in the horizontal plane firing area,at the moment, shooting opportunity conflicts of the first-launched aircraft missiles vertically launched by the double ships exist, and the conflict resolution method of the shooting opportunity conflicts of the first-launched aircraft missiles vertically launched by the double ships comprises the following steps that if B is detectedxqFirstly, the warship vertical-launching ship-air missile weapon carries out first-shot shooting on an approaching aerial target in the curved surface, and then BxqWarship vertical launching naval missile weapon needs to wait tBy+tafThe target in the curved surface can be shot firstly after the time. Secondly, if A isxqThe ship vertically-launched air-borne missile weapon carries out first-shot shooting on an approaching air target in the curved surface, and B isxqWarship vertical launching naval missile weapon needs to wait tAy+tBfThe target in the curved surface can be shot firstly after the time. Wherein, tAy＝RAy/VAy,tBy＝RBy/VBy。
(3) Overlap region curved surface Jy1Jy5Jy2Jy6
The curved surface is simultaneously positioned in a horizontal plane shooting area of the double-ship vertical launching aircraft missile, the shooting areas of the double-ship vertical launching aircraft horizontal plane are overlapped, the shooting opportunity conflict of the double-ship vertical launching first-launch aircraft missile exists, and the shooting opportunity conflict resolution method of the double-ship vertical first-launch aircraft missile is as follows: if A isxqFirstly, the warship vertical-launching ship-air missile weapon carries out first-shot shooting on an approaching aerial target in the curved surface, and then BxqWarship vertical launching naval missile weapon needs to wait tAy+tBfThe target in the curved surface can be shot firstly after the time. Secondly, if B isxqThe ship vertically-launched air-borne missile weapon carries out first-shot shooting on an approaching air target in the curved surface, and A isxqWarship vertical launching naval missile weapon needs to wait tBy+tafThe target in the curved surface can be shot firstly after the time. Wherein, tAy＝RAy/VAy,tBy＝RBy/VBy。
Wherein, the two ships are respectively AxqWarship, BxqWarship, point AyIs AxqShip position, point ByIs BxqShip position, in point AyIs a circular point with a radius RAyIs axqWarship vertically launches aircraft missile horizontal plane shooting area, as point ByIs a circular point, radius RByIs BxqWarship vertical launch naval air guided missile horizontal plane shooting area, point Jy1Point Jy2Is AxqWarship, BxqIntersection point, point J of horizontal plane shooting area of warship vertical launching naval-aircraft missiley3Point Jy6Is a straight line AyByAnd AxqIntersection point, point J of horizontal plane shooting area of warship vertical launching naval-aircraft missiley4Point Jy5Is a straight line AyByAnd AxqIntersection point, t, of horizontal plane shooting area of warship vertical launching naval-aircraft missileAyIs AxqWarship vertical launching aircraft missile flight distance RAyAverage time required, tByIs BxqWarship vertical launching aircraft missile flight distance RByRequired average time, VAyIs AxqAverage speed of ship vertical launching ship-air missile, VByIs BxqAverage speed of ship vertical launching naval missile, TBfIs BxqThe warship vertical-launching naval air guided missile weapon operational reaction time is BxqThe time required for a ship vertical launching aircraft missile weapon to find that an incoming air target starts and the first aircraft missile takes off the carrier TAfIs AxqResponse time of warship vertical launching of air-to-ship missile weapons in battle, AxqThe horizontal shooting area of the ship vertical-launching aircraft guided missile surrounds BxqAfter the ship vertically launches the aircraft guided missile horizontal plane shooting area to sit tangent lines, the two tangent lines and AxqThe intersection points of the horizontal plane shooting areas of the warship vertical-launching naval-aircraft guided missile are respectively point Jy7Point Jy8And B isxqThe intersection points of the horizontal plane shooting areas of the warship vertical-launching naval-aircraft guided missile are respectively point Jy9Point Jy10。
In addition, in order to solve the defects of the traditional technology, a shooting opportunity conflict resolution system for the first-launched ship-air missile launched by the double-ship vertical launch is also provided.
A shooting opportunity conflict resolution system for a dual-ship vertical-launching first-launch naval-aircraft missile comprises:
the first data acquisition unit is used for determining a horizontal plane shooting area of each single-ship vertical-launch aircraft-based missile, and the horizontal plane shooting area of the single-ship vertical-launch aircraft-based missile is determined by the horizontal plane shooting area of the single-ship vertical-launch aircraft-based missile;
the second data acquisition unit is used for comparing the distance value between the two ships with a remote boundary value of a horizontal plane launching area of the two-ship vertically-launched naval missile, wherein the remote boundary value of the horizontal plane launching area of the two-ship vertically-launched naval missile comprises a remote boundary value of a horizontal plane launching area of a first single-ship vertically-launched naval missile and a remote boundary value of a horizontal plane launching area of a second single-ship vertically-launched naval missile;
and the data output unit is used for adjusting the shooting time of the first ship air-borne missile vertically launched by the two single ships based on the set digestion mechanism.
Optionally, in one embodiment, the resolution mechanism is formed by a resolution scheme corresponding to a plurality of comparison results, where the comparison results refer to a size relationship between a relative position relationship of a horizontal plane shooting area of the dual-ship vertical-launch aircraft missile, that is, a dual-ship distance value, and a far-limit value of a horizontal plane launching area of the first single-ship vertical-launch aircraft missile and a far-limit value of a horizontal plane launching area of the second single-ship vertical-launch aircraft missile.
Optionally, in one embodiment, the resolution mechanism includes:
if the distance values between the two ships are larger than the far-limit value of the horizontal plane launching area of the first single-ship vertically-launched aircraft missile and the far-limit value of the horizontal plane launching area of the second single-ship vertically-launched aircraft missile; judging whether the incoming air target is located in a curved surface of an overlapping area of a horizontal plane launching area of a first single-ship vertical launching aircraft-borne missile and a horizontal plane launching area of a second single-ship vertical launching aircraft-borne missile, and enabling a later-launched single-ship vertical launching aircraft-borne missile to firstly shoot the target in the curved surface after a certain delay time, wherein the delay time is the sum of the average time required by the earlier-launched single-ship vertical launching aircraft-borne missile to reach the remote boundary value of the horizontal plane launching area of the corresponding vertical launching aircraft-borne missile and the weapon operational response time corresponding to the later-launched single-ship vertical launching aircraft-borne missile; if the distance values between the two ships are smaller than the far-limit value of the horizontal plane launching area of the first single-ship vertically-launched aircraft missile and the far-limit value of the horizontal plane launching area of the second single-ship vertically-launched aircraft missile, enabling the later-launched single-ship vertically-launched aircraft missile to firstly shoot the curved surface inner target after the delay time; if the distance value between the two ships is between the far-limit value of the horizontal plane launching area of the first single-ship vertical launching aircraft-borne missile and the far-limit value of the horizontal plane launching area of the second single-ship vertical launching aircraft-borne missile, judging whether an approaching aerial target is not located in a first area curved surface, and enabling a later-launched single-ship vertical launching aircraft-borne missile to firstly shoot the target in the curved surface after the delay time, wherein the first area curved surface is a curved surface area formed by a plurality of intersection points, and the intersection points comprise: the system comprises a first single-ship launching point, a second single-ship launching point, a directional line segment and an extension line, wherein the directional line segment is formed by the first single-ship launching point and takes the first single-ship launching point as a starting point, and the second single-ship launching point as an end point.
In addition, in order to solve the disadvantages of the conventional technology, a computer-readable storage medium is provided, which includes computer instructions, when the computer instructions are executed on a computer, the computer executes the method.
In conclusion, the method for clearing the firing opportunity conflict of the dual-ship vertically-launched first-launched aircraft-based missile provided by the invention can provide convenience for clearing the firing opportunity conflict of the dual-ship vertically-launched first-launched aircraft-based missile, eliminate the potential safety hazard of the dual-ship vertically-launched first-launched aircraft-based missile and ensure the safety of the dual-ship vertically-launched first-launched aircraft-based missile, and has the characteristics of simplicity and convenience, and the timing and the target sequence of the dual-ship vertically-launched first-launched aircraft-based missile can be determined.
The above-mentioned embodiments only express several embodiments of the present application, and the description thereof is more specific and detailed, but not construed as limiting the scope of the present application. It should be noted that, for a person skilled in the art, several variations and modifications can be made without departing from the concept of the present application, which falls within the scope of protection of the present application. Therefore, the protection scope of the present patent shall be subject to the appended claims.
Claims (3)
1. A shooting opportunity conflict resolution method for a dual-ship vertical-launching first-ship air-borne missile comprises the following steps:
s1, determining a horizontal plane shooting area of each single-ship vertical launching aircraft-based missile, wherein the horizontal plane shooting area of the single-ship vertical launching aircraft-based missile is determined through a horizontal plane shooting area of the single-ship vertical launching aircraft-based missile;
s2, comparing the distance value between the two ships with a remote boundary value of a horizontal plane launching area of the two-ship vertically-launched naval missile, wherein the remote boundary value of the horizontal plane launching area of the two-ship vertically-launched naval missile comprises a remote boundary value of a horizontal plane launching area of a first single-ship vertically-launched naval missile and a remote boundary value of a horizontal plane launching area of a second single-ship vertically-launched naval missile;
and S3, adjusting the shooting time of the first ship air-borne missile vertically launched by the two single ships based on the set digestion mechanism.
2. The method according to claim 1, wherein the resolution mechanism is composed of resolution schemes corresponding to a plurality of comparison results, and the comparison results refer to the magnitude relation between the relative position relation of the horizontal plane shooting areas of the dual-ship vertical launching aircraft-based missile, namely the dual-ship distance value, and the far boundary value of the horizontal plane launching area of the first single-ship vertical launching aircraft-based missile and the far boundary value of the horizontal plane launching area of the second single-ship vertical launching aircraft-based missile.
3. The method of claim 2, wherein the resolution mechanism comprises:
if the distance values between the two ships are larger than the far-limit value of the horizontal plane launching area of the first single-ship vertically-launched aircraft missile and the far-limit value of the horizontal plane launching area of the second single-ship vertically-launched aircraft missile; judging whether the incoming air target is located in a curved surface of an overlapping area of a horizontal plane launching area of a first single-ship vertical launching aircraft-borne missile and a horizontal plane launching area of a second single-ship vertical launching aircraft-borne missile, and enabling a later-launched single-ship vertical launching aircraft-borne missile to firstly shoot the target in the curved surface after a certain delay time, wherein the delay time is the sum of the average time required by the earlier-launched single-ship vertical launching aircraft-borne missile to reach the remote boundary value of the horizontal plane launching area of the corresponding vertical launching aircraft-borne missile and the weapon operational response time corresponding to the later-launched single-ship vertical launching aircraft-borne missile; if the distance values between the two ships are smaller than the far-limit value of the horizontal plane launching area of the first single-ship vertically-launched aircraft missile and the far-limit value of the horizontal plane launching area of the second single-ship vertically-launched aircraft missile, enabling the later-launched single-ship vertically-launched aircraft missile to firstly shoot the curved surface inner target after the delay time; if the distance value between the two ships is between the far-limit value of the horizontal plane launching area of the first single-ship vertical launching aircraft-borne missile and the far-limit value of the horizontal plane launching area of the second single-ship vertical launching aircraft-borne missile, judging whether an approaching aerial target is not located in a first area curved surface, and enabling a later-launched single-ship vertical launching aircraft-borne missile to firstly shoot the target in the curved surface after the delay time, wherein the first area curved surface is a curved surface area formed by a plurality of intersection points, and the intersection points comprise: the system comprises a first single-ship launching point, a second single-ship launching point, a directional line segment and an extension line, wherein the directional line segment is formed by the first single-ship launching point and takes the first single-ship launching point as a starting point, and the second single-ship launching point as an end point.
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