JPH07190693A - Passive guiding apparatus - Google Patents

Abstract

PURPOSE:To launch a missile, to accurately guide the missile without irradiating with a radio wave even after the missile is launched and to hit an antiaircraft target by calculating a prediction hitting point without irradiating directly the target with the wave. CONSTITUTION:Two angle information are integrated by a surface ship 1 having a missile guiding unit 2 which has a ship-board passive electromagnetic wave detector 3 and a missile launcher 7 and a missile 12 having a passive electromagnetic detector 15 to guide the missile 12. Thus, the angle information of two different mobile targets are continuously analyzed without directly irradiating with a radio wave, a prediction hitting point is calculated, the missile 12 is guided to hit an antiaircraft target 20 by the missile 12.

Description

Detailed Description of the Invention

[0001]

BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a passive guidance system for attacking an anti-aircraft target with a missile without directly emitting radio waves from the surface ship to the anti-aircraft target.

[0002]

2. Description of the Related Art FIG. 22 is a conceptual diagram of an operation of a conventional missile attack against an air target, and FIG. 23 is a system configuration diagram of a conventional missile guidance system. 22 and 23
In the figure, 1 is a surface ship, 3 is a passive electromagnetic wave detection device on board, 7 is a missile launcher, 12 is a missile, 20 is an air target, 21 is an electromagnetic wave radiated from an air target, 10
4 is a shooting command device, 105 is a guided radio wave emitting device, 106
Is an induction wave emitted from the induction wave emission device 105, 1
Reference numeral 07 is a missile launch signal transmitted from the shooting command device to the missile launching device, and 108 is a control signal transmitted from the shooting commanding device to the guided radio wave launching device.

Next, the operation will be described. 22 and 23, the conventional method detects the electromagnetic wave 21 radiated from the anti-aircraft target 20 by the onboard passive electromagnetic wave detection device 3 of the surface ship 1, and inputs the result thereof by the shooting command device 104 to transmit the radio wave. The missile launching device 7 launches the missile 12 while the missile launching device 7 outputs a missile launch signal based on the result of calculating the predicted hit point by calculating the predicted hit point. Device 1
Guided radio wave emitting device 10 by control signal 108 from 04.
5 to control the guided wave 1 from the guided wave emitting device 105.
06 is emitted to irradiate the anti-air target 20, and the missile 12 emitted from the missile launching device 7 continuously receives the reflected wave to hit the anti-air target 20 to be shot down.

[0004]

Since the conventional missile guidance system is constructed as described above, in order to calculate the predicted hit point for launching and guiding the missile, direct radio waves are transmitted to the anti-aircraft target. In order to guide the missile accurately and shoot down the anti-aircraft target, it is necessary to continuously irradiate the radio wave, exposing the position of the surface ship to the other party. There was a problem.

The present invention has been made in order to solve the above-mentioned problems, and it is possible to calculate a predicted hit point and to launch a missile without directly radiating radio waves to an anti-air target, and at the same time, to launch a missile. The aim is to obtain a passive guidance device that can accurately guide the missile and shoot down the anti-aircraft target without radio wave irradiation.

[0006]

A passive induction device according to the present invention is equipped with a shipboard passive electromagnetic wave detection device on a surface ship, and the passive electromagnetic wave detection device changes the angle information based on the detection result and the relative distance outside the ship. By combining with the angle information based on the result detected by the device, the predicted hit point is calculated without directly irradiating the anti-aircraft target with radio waves, the missile is launched, and the anti-aircraft target is not continuously radiated with radio waves. By transmitting the predicted hit point instruction information to the missile that has been launched via, the missile is accurately guided to shoot down the anti-aircraft target. Furthermore, the passive guidance device of the present invention includes a hit point calculation device, a surface ship, or a missile, or a carrier-based helicopter,
Alternatively, it is mounted on an unmanned aerial vehicle, a discard type radio wave detection device, or a cannonball type radio wave detection device.

[0007]

The passive guidance device according to the present invention calculates the predicted hit point based on the angle information detected by the passive electromagnetic wave detection devices at two locations where the relative distances of the surface ship and the rest vary and the anti-aircraft target is calculated. Launch a missile and guide it accurately, without directly irradiating the
You can shoot down anti-aircraft targets with missiles.

[0008]

BEST MODE FOR CARRYING OUT THE INVENTION For the sake of convenience of explanation, a structure in which one of the passive electromagnetic wave detecting devices is provided in a missile guiding device of a surface ship will be described below. Example 1. FIG. 1 is a system configuration diagram of a passive guidance device showing an embodiment of the present invention, FIG. 2 is an operation conceptual diagram when a missile is launched from an anti-aircraft target from a surface ship according to the present invention, and FIG. It is a functional block diagram of the hit point calculation apparatus by this invention. In the figure, 1 is a surface ship, 2 is a missile guidance device equipped on the surface ship 1, 3 is a passive electromagnetic wave detection device for the missile guidance device 2, 4 is a missile tracking device, 5 is a communication device on board, and 6 is a hit point. Calculation device, 7 is a missile launching device, 8 is angle information detected by the onboard passive electromagnetic wave detection device 3, and 9 is a missile tracking device 4.
Position information of the missile 12 which was measured by 10; angle information from the missile 12 obtained via the onboard communication device 5;
Is predicted hit point instruction information from the hit point calculation device 6, 12 is a missile, 13 is a communication device of the missile 12, 14 is a steering device of the missile 12, 15 is a passive electromagnetic wave detection device of the missile 12, 16 is communication of the missile 12. Angle information from the device 13, 17 is predicted hit point instruction information from the onboard communication device 5, 18 is predicted hit point instruction information input from the communication device 13 of the missile 12 to the steering device 14, and 19 is a passive electromagnetic wave of the missile 12. Angle information detected by the detection device 15, 20 is an air target, 21 is an electromagnetic wave radiated from the air target, 109 is angle information input processing, 110 is position information input processing, 111 is starting point coordinate setting processing, and 112 is angle synthesis processing. , 113 is an intersection point coordinate calculation process, 114 is a predicted hit point calculation process, and 115 is a predicted hit point instruction information output process.

Next, the operation will be described. From the missile launcher 7 of the surface ship 1 to the passive electromagnetic wave detector 3 on board
Missile 12 launched by angle information 8 detected by
Is the angle information 8 of the onboard passive electromagnetic wave detection device 3 and the angle information 1 of the passive electromagnetic wave detection device 15 of the missile 12.
0 and the position information 9 of the missile 12 of the missile tracking device 4, the hit point calculation device 6 calculates and the onboard communication device 5
The anti-aircraft target 20 according to the hit point instruction information 17 transmitted via
It is possible to be guided without hitting the radio wave directly to, hit, and shoot down the anti-air target 20.

Next, the present invention will be described with reference to FIGS. The onboard passive electromagnetic wave detection device 3 of the missile guidance device 2 equipped on the surface ship 1 detects the electromagnetic wave 21 radiated from the anti-aircraft target 20, and outputs the result as the angle information 8 to the hit point calculation device 6 and the missile launcher 7. introduce.
The missile launcher 7 detects the missile 1 based on the angle information 8.
Fire a 2. The passive electromagnetic wave detection device 15 of the launched missile 12 detects the electromagnetic wave 21 radiated from the anti-air target 20 while flying, and transmits the result as angle information 19 to the communication device 13 of the missile 12, and the communication device 1
3 is angle information 1 from the missile 12 to the onboard communication device 5.
Send as 6. The onboard communication device 5 transmits the angle information 10 from the missile 12 to the hit point calculation device 6. The missile tracking device 4 tracks and measures the missile 12 in flight, continuously measures the position of the missile 12, and transmits the result to the hit point calculation device 6 as position information 9 of the missile 12. The hit point calculation device 6 is based on the inputted two pieces of angle information 8 and 10 and the position information 9 of the missile 12,
The position of the anti-air target 20 is continuously measured, the predicted hit point of the missile 12 for the anti-air target 20 is calculated from the result, and the predicted hit point instruction information 11 is transmitted to the onboard communication device 5. The onboard communication device 5 is the communication device 1 of the missile 12.
3, the predicted hit point instruction information 17 is transmitted. The communication device 13 of the missile 12 transmits the predicted hit point instruction information 18 to the steering device 14, and the steering device 14 guides the missile 12 according to the predicted hit point instruction information 18. Next, the function of the hit point calculation device according to the present invention will be described with reference to FIG. The hit point calculation device 6 inputs the angle information 16 from the missile 12 as the angle information 10 from the onboard communication device 5 and the angle information 8 from the onboard passive electromagnetic wave detection device 3 (process 109). On the other hand, the position information 9 of the missile 12 is input from the missile tracking device 4 (Process 1
10). Next, the input position information 9 of the missile 12
In order to use it as the starting point of the angle information, it is set and registered as the starting point coordinates (process 111). The input angle information and the starting point coordinates thereof are combined for each sampling time (process 112). From the result, the intersection of the two pieces of angle information for each sampling time is calculated and registered as the intersection coordinates (process 113). From the time difference of the sampling times and the intersection coordinates for each sampling time, the future position of the anti-aircraft target 20 is calculated, the trajectory of the anti-aircraft target 20 is predicted for each sampling time, and based on the position and speed of the flying missile 12, Calculate the meeting point between the missile 12 and the air target 20,
It is registered as a predicted hit point (process 114). The result is output to the shipboard communication device 5 as the predicted hit point instruction information 11 for each sampling time (process 115). The onboard communication device 5 transmits the predicted hit point instruction information 17 to the missile 12.

As described above, two passive electromagnetic wave detecting devices that detect the electromagnetic waves radiated from the air target and change the relative distance, a tracking device that measures the relative distance between the two passive electromagnetic wave detecting devices, and a hit point calculation. Since the device calculates the future position of the anti-aircraft target from two pieces of angle information and position information, it is possible to guide the missile and shoot down the anti-aircraft target without directly irradiating the anti-aircraft target with radio waves. The electromagnetic waves include radio waves and light waves.

Example 2. FIG. 3 is a system configuration diagram of a passive induction device showing an embodiment of the present invention. In the figure,
22 is the hit point calculation device of the missile 12, 23 is the angle information from the surface ship 1, 24 is the position information of the own ship 1 converted by the onboard communication device 28 based on the tracking result 9 of the missile tracking device 4, 25 is the missile 12 Angle information from the ship 1 transmitted from the communication device 13, 26 is position information of the ship 1 transmitted from the communication device 13 of the missile 12, 27 is predicted hit point instruction information from the hit point calculation device 22 of the missile 12, Reference numeral 28 is an onboard communication device that also converts the position information 9. In FIG. 3, except that the missile 12 is equipped with a hit point calculation device 22, the operation principle is the same as in the first embodiment, and the electromagnetic wave 21 radiated from the anti-aircraft target 20 is the same.
And two passive electromagnetic wave detection devices 3 and 15 that detect the
Since the tracking device 4 for measuring the relative distances of 15 and 15 and the hit point calculation device 22 are used to calculate the future position of the anti-air target 20 from the two pieces of angle information 8 and 19 and the position information 9, the anti-air target 20 It is possible to shoot down the anti-aircraft target 20 with the missile 12 without directly irradiating the radio wave.

Embodiment 3. FIG. 4 is a system configuration diagram of a passive induction device showing an embodiment of the present invention. In the figure,
29 is a helicopter tracking device for the missile guidance device 2,
Reference numeral 30 is position information of the onboard helicopter 32, 31 is angle information from the onboard helicopter 32 transmitted from the onboard communication device 5, 32 is an onboard helicopter, and 33 is an onboard helicopter 32.
On-board communication device, 34 is an on-board passive electromagnetic wave detection device,
Reference numeral 35 is angle information detected by the onboard passive electromagnetic wave detection device 34, and 36 is angle information transmitted from the onboard helicopter 32 to the onboard communication device 5. In FIG. 4, the on-board passive electromagnetic wave detection device 34 is different in that it is mounted on the ship-mounted helicopter 32, and the operation principle is the same as in the first embodiment, that is, the electromagnetic wave 21 radiated from the air target 20 is detected and the relative distance is changed. Two changing passive electromagnetic wave detectors 3 and 34
Using the tracking device 29 that measures the relative distance between the two passive electromagnetic wave detection devices 3 and 34, and the hit point calculation device 6, the future position of the anti-aircraft target 20 is calculated from the two angle information 8 and 35 and the position information 30. I'm calculating it
It is possible to shoot down the anti-aircraft target 20 with the missile 12 without directly irradiating the radio wave.

Example 4. FIG. 5 is a system configuration diagram of a passive induction device showing an embodiment of the present invention. In the figure,
37 is the position information of the own ship 1 converted by the onboard communication device 28 based on the tracking result 30 of the onboard helicopter tracking device 29, 3
8 is angle information from the own ship 1 transmitted from the onboard communication device 33 of the onboard helicopter 32, and 39 is onboard helicopter 32.
Position information of own ship 1 transmitted from the onboard communication device 33 of
Reference numeral 40 is a hit point calculation device for the ship-mounted helicopter 32, 41 is predicted hit point instruction information from the hit point calculation device 40 of the ship-mounted helicopter 32, and 42 is predicted hit point instruction information from the onboard communication device 33. In FIG. 5, the on-board passive electromagnetic wave detection device 34 and the hit point calculation device 40 are the ship-mounted helicopter 3
2 is different in that it is equipped with an electromagnetic wave 21 which is radiated from the air target 20 as in the second and third embodiments.
And two passive electromagnetic wave detecting devices 3 and 34 that detect the
Since the tracking device 29 that measures the relative distance between the target and the target 34 and the hit point calculation device 40 are used to calculate the future position of the anti-air target 20 from the two pieces of angle information 8 and 35 and the position information 30, the anti-air target 20 It is possible to shoot down the anti-aircraft target 20 with the missile 12 without directly irradiating the radio wave.

Example 5. FIG. 6 is a system configuration diagram of a passive induction device showing an embodiment of the present invention. In the figure,
Reference numeral 43 denotes an onboard missile launching device for launching the missile 12 based on the angle information 35 of the onboard passive electromagnetic wave detection device 34 of the onboard helicopter 32. In FIG. 6, except that the onboard missile launcher 43 is mounted on the ship-mounted helicopter 32, the operation principle is the same as in the fourth embodiment, the electromagnetic wave 21 radiated from the air target 20 is detected, and the relative distance changes. Two passive electromagnetic wave detection devices 3 and 34
Using a tracking device 29 for measuring the relative distance between the two passive electromagnetic wave detection devices 3 and 34 and a hit point calculation device 40,
Since the future position of the anti-air target 20 is calculated from the two pieces of angle information 8 and 35 and the position information 30, the anti-air target 20 can be shot down by the missile 12 without directly irradiating the anti-air target 20 with a radio wave.

Example 6. FIG. 7 is a system configuration diagram of a passive induction device showing an embodiment of the present invention. In the figure,
44 is position information of the onboard helicopter 32 from the onboard communication device 28, 45 is angle information from the onboard communication device 33, 47
Is position information of the onboard helicopter 32 transmitted from the communication device 13 of the missile 12. In FIG. 7, except that the missile is equipped with a hit point calculation device 22, the operation principle is the same as that of the fifth embodiment, the electromagnetic wave 21 radiated from the anti-aircraft target 20 is detected, and the two relative distances change. Tracking device 2 for measuring the relative distance between passive electromagnetic wave detecting devices 3 and 34 and two passive electromagnetic wave detecting devices 3 and 34.
9, the tracking device 4 for measuring the position of the missile 12, and the hit point calculation device 22 are used to obtain two pieces of angle information 8 and 35.
Since the future position of the anti-air target 20 is calculated from the position information 9 and 30, the missile 12 can shoot down the anti-air target 20 without directly irradiating the anti-air target 20 with a radio wave.

Embodiment 7. FIG. 8 is a system configuration diagram of a passive induction device showing an embodiment of the present invention. In the figure,
The on-board missile launching device 43 is mounted on the onboard helicopter 32, and is the same as the third embodiment. In FIG. 8, the operation principle is the same as that of the third embodiment, the electromagnetic wave 21 radiated from the air target 20 is detected, and the two passive electromagnetic wave detecting apparatuses 3 and 34 whose relative distance is changed and the two passive electromagnetic wave detecting apparatuses 3 and 34 are changed. Tracking device 29 for measuring the relative distance of 34
Since the future position of the anti-air target 20 is calculated from the two angle information 8 and 35 and the position information 30 by using the hit point calculation device 6, the missile 12 is not directly irradiated to the anti-air target 20. Can shoot down the anti-aircraft target 20.

Example 8. FIG. 9 is a system configuration diagram of a passive induction device showing an embodiment of the present invention. In the figure,
48 is an unmanned air vehicle tracking device for the missile guidance device 2, 49
Is position information of the unmanned aerial vehicle 51, 50 is angle information from the unmanned aerial vehicle 51 transmitted from the onboard communication device 5, 51 is an unmanned aerial vehicle, 52 is an onboard communication device of the unmanned aerial vehicle 51, 53
Is a passive electromagnetic wave detection device for unmanned air vehicle 51, 54
Is angle information detected by the onboard passive electromagnetic wave detection device 53, and 55 is angle information transmitted from the unmanned air vehicle 51 to the onboard communication device 5. In FIG. 9, the carrier-based helicopter 3
2 replaces the unmanned aerial vehicle 51, and the operating principle is the same as that of the third embodiment. The passive electromagnetic wave detection devices 3 and 53 that detect the electromagnetic wave 21 radiated from the anti-aircraft target 20 and change the relative distance, and the two passive electromagnetic wave detection devices 3 and 53. Passive electromagnetic wave detection devices 3 and 5
Using the tracking device 48 that measures the relative distance of 3 and the hit point calculation device 6, two pieces of angle information 8 and 54 and position information 4
Since the future position of the anti-aircraft target 20 is calculated from 9, the missile 1 does not need to be directly irradiated to the anti-aircraft target 20.
2 can shoot down the anti-aircraft target 20.

Example 9. FIG. 10 is a system configuration diagram of a passive induction device showing an embodiment of the present invention. In the figure, 56 is the position information of the own ship 1 converted by the onboard communication device 28 based on the tracking result 49 of the unmanned air vehicle tracking device 48, 5
7 is the angle information from the ship 1 transmitted from the onboard communication device 52 of the unmanned aerial vehicle 51, 58 is the position information of the ship 1 transmitted from the onboard communication device 52 of the unmanned aerial vehicle 51, and 59 is the unmanned aerial vehicle 51 hit point calculator, 60 unmanned air vehicle 51
Predictive hit point instruction information from the hit point calculation device 59, 61
Is the predicted hit point instruction information from the onboard communication device 52.
In FIG. 10, the onboard helicopter 32 is an unmanned air vehicle 51.
In addition to the above, the operating principle is the same as that of the fourth embodiment, and the anti-aircraft target 2
The two passive electromagnetic wave detection devices 3 and 53 that detect the electromagnetic wave 21 radiated from 0 and change the relative distance, the tracking device 48 that measures the relative distance between the two passive electromagnetic wave detection devices 3 and 53, and the hit point calculation 2 using the device 59
From the angle information 8 and 54 and the position information 49, the air target 2
Since the future position of 0 is calculated, the anti-air target 20 can be shot down by the missile 12 without directly irradiating the anti-air target 20 with a radio wave.

Example 10. FIG. 11 is a system configuration diagram of a passive induction device showing an embodiment of the present invention. In the figure, reference numeral 62 is an on-board missile launching device that launches the missile 12 based on the angle information 54 of the on-board passive electromagnetic wave detection device 53 of the unmanned air vehicle 51. In FIG. 11, the ship-mounted helicopter 32 is replaced by an unmanned aerial vehicle 51, and the operating principle is the same as in the fifth embodiment. The passive electromagnetic wave detection device 3 detects the electromagnetic waves 21 radiated from the anti-aircraft target 20 and changes the relative distance. And 53, a tracking device 48 that measures the relative distance between the two passive electromagnetic wave detection devices 3 and 53, and a hit point calculation device 59, two pieces of angle information 8 and 54.
Since the future position of the anti-aircraft target 20 is calculated from the position information 49, the anti-aircraft target 20 can be shot down by the missile 12 without directly irradiating the anti-aircraft target 20 with a radio wave.

Embodiment 11. FIG. 12 is a system configuration diagram of a passive induction device showing an embodiment of the present invention. In the figure, 63 is position information of the unmanned aerial vehicle 51 from the onboard communication device 28, 64 is angle information from the onboard communication device 52, and 65.
Is angle information from the unmanned aerial vehicle 51 transmitted from the communication device 13 of the missile 12, and 66 is position information of the unmanned aerial vehicle 51 transmitted from the communication device 13 of the missile 12.
In FIG. 12, the carrier-based helicopter 32 is an unmanned air vehicle 51.
In addition to the above, the operation principle is the same as in the sixth embodiment, and the anti-aircraft target 2
0 of the electromagnetic wave 21 radiated from 0, the relative distance changes the two passive electromagnetic wave detection devices 3 and 53, the tracking device 48 that measures the relative distance between the two passive electromagnetic wave detection devices 3 and 53, and the missile 12. The tracking device 4 for measuring the position and the hit point calculation device 22 are used to detect the air target 20 from the two pieces of angle information 8 and 54 and the position information 9 and 49.
Since the future position of the anti-aircraft target 2 is calculated by the missile 12, the anti-aircraft target 20 is not directly irradiated with the radio wave.
You can shoot down 0.

Embodiment 12. FIG. 13 is a system configuration diagram of a passive induction device showing an embodiment of the present invention. In the figure, the onboard missile launching device 62 is mounted on the unmanned aerial vehicle 51, and is the same as the eighth embodiment. In FIG. 13, the operation principle is the same as that of the eighth embodiment. The passive electromagnetic wave detecting devices 3 and 53 that detect the electromagnetic wave 21 radiated from the air target 20 and change the relative distance, and the two passive electromagnetic wave detecting devices 3 and Tracking device 4 for measuring the relative distance of 53
8 and the hit point calculation device 6 are used to calculate the future position of the anti-aircraft target 20 from the two pieces of angle information 8 and 54 and the positional information 49, so the missile can be directly emitted to the anti-aircraft target 20. You can shoot down the anti-aircraft target 20 with 12.

Example 13. FIG. 14 is a system configuration diagram of a passive induction device showing an embodiment of the present invention. In the figure, 67 is a discard type radio detection device tracking device of the missile guidance device 2, 68 is position information of the discard type radio detection device 70, 6
Reference numeral 9 is angle information from the discard type radio wave detection device 70 transmitted from the shipboard communication device 5, 70 is a discard type radio wave detection device, 71
Is a communication device mounted on the discard type radio wave detection device 70, 72 is a passive electromagnetic wave detection device mounted on the discard type radio wave detection device 70, 7
3 is the angle information detected by the onboard passive electromagnetic wave detection device 72, and 74 is the discard type radio wave detection device 70 to the onboard communication device 5
It is the angle information transmitted to. In FIG. 14, the ship-based helicopter 32 is replaced with the discard type radio wave detection device 70, and the operation principle is the same as in the third embodiment, the electromagnetic wave 21 radiated from the anti-aircraft target 20 is detected, and two passive electromagnetic wave detections in which the relative distance is changed. A tracking device 6 for measuring the relative distance between the devices 3 and 72 and the two passive electromagnetic wave detection devices 3 and 72.
7 and the hit point calculation device 6 are used to calculate the future position of the anti-aircraft target 20 from the two pieces of angle information 8 and 73 and the position information 68, so the missile can be directly emitted to the anti-aircraft target 20. You can shoot down the anti-aircraft target 20 with 12.

Example 14 FIG. 15 is a system configuration diagram of a passive induction device showing an embodiment of the present invention. In the figure, 75 is the position information of the own ship 1 converted by the onboard communication device 28 based on the tracking result 68 of the discard type radio detection device tracking device 67, and 76 is the onboard communication device 7 of the discard type radio detection device 70.
1, the angle information from the ship 1 transmitted from the ship 1, 77 is the position information of the ship 1 transmitted from the on-board communication device 71 of the dumping type radio wave detection device 70, 78 is the hit point calculation device of the dumping type radio wave detection device 70, 79 Is the predicted hit point instruction information from the hit point calculation device 78 of the discard type radio detection device 70, and 80 is the predicted hit point instruction information from the onboard communication device 71. In FIG. 15, the ship-mounted helicopter 32 is replaced with the discard type radio wave detection device 70, and the operation principle is the same as that of the fourth embodiment.
Two passive electromagnetic wave detection devices 3 and 72 that detect the electromagnetic wave 21 radiated from the device and change the relative distance, a tracking device 67 that measures the relative distance between the two passive electromagnetic wave detection devices 3 and 72, and a hit point calculation device. 78 using the two pieces of angle information 8 and 73 and the position information 68.
Since the future position of the anti-aircraft target 2 is calculated by the missile 12, the anti-aircraft target 20 is not directly irradiated with the radio wave.
You can shoot down 0.

Example 15. FIG. 16 is a system configuration diagram of a passive induction device showing an embodiment of the present invention. In the figure, reference numeral 81 is a hit point calculation device having a table of shots, 82 is a gun, 83 is a bullet type radio wave detection device, 84 is a communication device mounted on the bullet type radio wave detection device 83, and 85 is a bullet type radio wave detection device 8
3 is the onboard passive electromagnetic wave detection device, 86 is angle information detected by the onboard passive electromagnetic wave detection device 85, 87 is angle information transmitted from the shell-type radio wave detection device 83 to the onboard communication device 5, and 88 is transmitted from the onboard communication device 5. It is angle information from the cannonball type radio detection device 83 that is generated. In FIG.
The ship-mounted helicopter 32 replaces the bullet-type radio wave detection device 83, and the position information of the bullet-type radio wave detection device 83 is determined from the surface of the table, and the principle of operation is the same as in the third embodiment.
Using the two passive electromagnetic wave detection devices 3 and 85 whose relative distance changes and the hit point calculation device 81 which calculates the relative distance between the two passive electromagnetic wave detection devices 3 and 85, Since the future position of the anti-aircraft target 20 is calculated from the two pieces of angle information 8 and 86,
The missile 12 can shoot down the anti-air target 20 without directly irradiating the anti-air target 20 with a radio wave.

Example 16. FIG. 17 is a system configuration diagram of a passive induction device showing an embodiment of the present invention. In the figure, 89 is predicted hit point instruction information from the bullet-type radio detection device 83 transmitted from the onboard communication device 5, and 90 is angle information from the own ship 1 transmitted from the on-board communication device 84 of the bullet-type radio detection device 83. , 91 is the hit point calculation device of the bullet-type radio detection device 83, 92 is the predicted hit point instruction information from the hit-point calculation device 91 of the bullet type radio detection device 83, and 93 is the predicted hit point instruction information from the onboard communication device 84. Is. In FIG. 17, the ship-mounted helicopter 32 is a bullet-type radio detection device 83.
Instead of determining the position information of the cannonball type radio wave detection device 83 by means of an emission table, the operation principle is the same as in the fourth embodiment, the electromagnetic wave 21 radiated from the air target 20 is detected, and two passive electromagnetic waves whose relative distance changes. The detection devices 3 and 85,
Since the future position of the anti-aircraft target 20 is calculated from the two angle information 8 and 86 by using the hit point calculation device 91 which calculates the relative distance between the two passive electromagnetic wave detection devices 3 and 85, the direct position to the anti-aircraft target 20 is calculated. The missile 12 can shoot down the anti-aircraft target 20 without radiating radio waves.

Example 17 FIG. 18 is a system configuration diagram of a passive induction device showing an embodiment of the present invention. In the figure, 94 is position information of the discard type radio detection device 70 from the onboard communication device 28, 95 is angle information from the onboard communication device 71, 96 is a discard type radio detection device 70 transmitted from the communication device 13 of the missile 12. And 97 is position information of the discard type radio wave detection device 70 transmitted from the communication device 13 of the missile 12. In FIG. 18, the helicopter 32 on board the ship is replaced with the radio wave detection device 70 of the discard type, and the missile launching device 7 is mounted on the surface ship, and the operating principle is the same as in the sixth embodiment.
And two passive electromagnetic wave detection devices 3 and 72 that detect the
Using the tracking device 67 for measuring the relative distance between the two and 72, the tracking device 4 for measuring the position of the missile 12, and the hit point calculation device 22, two pieces of angle information 8 and 73 and position information 9 are used.
Since the future position of the anti-aircraft target 20 is calculated from Nos. 68 and 68, it is possible to shoot down the anti-aircraft target 20 with the missile 12 without directly irradiating the anti-aircraft target 20 with a radio wave.

Example 18. FIG. 19 is a system configuration diagram of a passive induction device showing an embodiment of the present invention. In the figure, 98 is a bullet-type radio detection device tracking device of the missile guidance device 2, 99 is position information of the bullet-type radio detection device 83 tracked by the bullet-type radio detection device tracking device 98, and 100 is a shell from the onboard communication device 28. Information of the type radio wave detection device 83, 101 is angle information from the on-board communication device 84, 102
Is angle information from the bullet-type radio wave detection device 83 transmitted from the communication device 13 of the missile 12, and 103 is the missile 12
Bullet type radio wave detection device 83 transmitted from the communication device 13 of
It is the position information of. 19, the helicopter 3 on board
2 replaces the cannonball type radio detecting device 83, the missile launching device 7 and the gun 82 are mounted on the surface ship, and the operation principle is the same as in the sixth embodiment, the electromagnetic wave 21 radiated from the anti-aircraft target 20 is detected and the relative movement is performed. Two passive electromagnetic wave detection devices 3 and 85 whose distances change, a tracking device 98 that measures the relative distance between the two passive electromagnetic wave detection devices 3 and 85, a tracking device 4 that measures the position of the missile 12, and a hit point calculation. The device 22 is used to calculate the future position of the anti-aircraft target 20 from the two pieces of angle information 8 and 86 and the positional information 9 and 99.
The missile 12 can shoot down the anti-aircraft target 20.

Example 19 FIG. 20 is a system configuration diagram of a passive induction device showing an embodiment of the present invention. In the figure, the missile launcher 7 is equipped on the surface ship 1,
Same as Example 6. In FIG. 20, the operation principle is the same as that of the sixth embodiment.
1 and two passive electromagnetic wave detection devices 3 and 34 whose relative distance changes, a tracking device 29 that measures the relative distance between the two passive electromagnetic wave detection devices 3 and 34, and a tracking device that measures the position of the missile 12. 4 and the hit point calculation device 22 are used to calculate the future position of the anti-aircraft target 20 from the two angle information 8 and 35 and the positional information 9 and 30, so that the anti-aircraft target 20 can be directly irradiated with the radio wave. , The target 12 can be shot down by the missile 12.

Example 20. FIG. 21 is a system configuration diagram of a passive induction device showing an embodiment of the present invention. In the figure, the missile launcher 7 is equipped on the surface ship 1,
Same as Example 11. In FIG. 21, the operation principle is the same as that of the eleventh embodiment, the electromagnetic wave 21 radiated from the air target 20 is detected, and the two passive electromagnetic wave detection devices 3 and 53 whose relative distances change and the two passive electromagnetic wave detection devices 3 and A tracking device 48 for measuring the relative distance of 53,
The tracking device 4 for measuring the position of the missile 12 and the hit point calculation device 22 are used to calculate the future position of the anti-aircraft target 20 from the two angle information 8 and 54 and the positional information 9 and 49. It is possible to shoot down the anti-aircraft target 20 with the missile 12 without directly irradiating the 20 with radio waves.

[0031]

As described above, according to the present invention, it is possible to shoot down an anti-aircraft target using a missile based on only angle information without directly irradiating a radio wave to the anti-aircraft target, which was not possible by the conventional method. .

[Brief description of drawings]

FIG. 1 is a system configuration diagram showing a first embodiment of the present invention.

FIG. 2 is a system operation conceptual diagram according to the first embodiment of the present invention.

FIG. 3 is a system configuration diagram showing a second embodiment of the present invention.

FIG. 4 is a system configuration diagram showing a third embodiment of the present invention.

FIG. 5 is a system configuration diagram showing a fourth embodiment of the present invention.

FIG. 6 is a system configuration diagram showing a fifth embodiment of the present invention.

FIG. 7 is a system configuration diagram showing a sixth embodiment of the present invention.

FIG. 8 is a system configuration diagram showing a seventh embodiment of the present invention.

FIG. 9 is a system configuration diagram showing an eighth embodiment of the present invention.

FIG. 10 is a system configuration diagram showing a ninth embodiment of the present invention.

FIG. 11 is a system configuration diagram showing an embodiment 10 of the present invention.

FIG. 12 is a system configuration diagram showing an eleventh embodiment of the present invention.

FIG. 13 is a system configuration diagram showing an embodiment 12 of the present invention.

FIG. 14 is a system configuration diagram showing a thirteenth embodiment of the present invention.

FIG. 15 is a system configuration diagram showing a fourteenth embodiment of the present invention.

FIG. 16 is a system configuration diagram showing a fifteenth embodiment of the present invention.

FIG. 17 is a system configuration diagram showing Embodiment 16 of the present invention.

FIG. 18 is a system configuration diagram showing a seventeenth embodiment of the present invention.

FIG. 19 is a system configuration diagram showing an eighteenth embodiment of the present invention.

FIG. 20 is a system configuration diagram showing Embodiment 19 of the present invention.

FIG. 21 is a system configuration diagram showing Embodiment 20 of the present invention.

FIG. 22 is an operational concept diagram of a missile attack on an air-to-air target by a conventional method.

FIG. 23 is a system configuration diagram of a missile guidance system according to a conventional method.

FIG. 24 is a functional configuration diagram of a hit point calculation device according to the present invention.

[Explanation of symbols]

1 surface ship 2 missile guidance device equipped on surface ship 3 missile guidance device onboard passive electromagnetic wave detection device 4 missile tracking device 5 onboard communication device 6 hit point calculation device 7 missile launcher 8 angle detected by onboard passive electromagnetic wave detection device Information 9 Missile position information measured by the missile tracking device 10 Angle information from the missile obtained via the onboard communication device 11 Predicted hit point instruction information from the hit point calculation device 12 Missile 13 Missile communication device 14 Missile steering device 15 Missile Passive Electromagnetic Wave Detecting Device 16 Angle Information from Missile Communication Device 17 Predicted Hit Point Indication Information from Shipboard Communication Device 18 Predicted Hit Point Indication Information Input from Missile Communication Device to Steering Device 19 Missile Passive Electromagnetic Wave Detection Angle information detected by the device 20 Anti-aircraft Standard 21 Electromagnetic waves radiated from anti-aircraft target 22 Missile hit point calculator 23 Angle information from surface ship 24 Position information of own ship converted by the onboard communication device based on the tracking result of the missile tracking device 25 Transmitted from the missile communication device Angle information from own ship 26 Angle information of own ship transmitted from communication device of missile 27 Predicted hit point instruction information from hit point calculation device of missile 28 Onboard communication device that performs conversion of position information 29 Missile guidance device Onboard helicopter tracking device 30 Position information of onboard helicopter 31 Angle information from onboard helicopter transmitted from onboard communication device 32 Onboard helicopter 33 Onboard communication device of onboard helicopter 34 Onboard passive electromagnetic wave detection device 35 Onboard passive electromagnetic wave detection device Detected angle information 36 From ship-mounted helicopter to ship Angle information transmitted to the onboard communication device 37 Position information of the own ship converted by the onboard communication device based on the tracking result of the onboard helicopter tracking device 38 Angle information from the own ship transmitted from the onboard communication device of the onboard helicopter 39 Information of the onboard helicopter Position information of own ship transmitted from onboard communication device 40 Hit point calculation device for onboard helicopter 41 Predicted hit point instruction information from onboard helicopter hit point calculation device 42 Predicted hit point instruction information from onboard communication device 43 Onboard helicopter Missile launcher that launches a missile based on the angle information of the on-board passive electromagnetic wave detection device 44 Position information of the onboard helicopter from the onboard communication device 45 Angle information from the onboard communication device 46 Transmitted from the missile communication device Angle information from carrier-based helicopter 47 Carrier-based helicopter transmitted from missile communication device Copter position information 48 Missile guidance device unmanned air vehicle tracking device 49 Unmanned air vehicle position information 50 Angle information from unmanned air vehicle transmitted from onboard communication device 51 Unmanned air vehicle 52 On-board communication device of unmanned air vehicle 53 Passive electromagnetic wave detection device for unmanned air vehicle 54 Angle information detected by passive electromagnetic wave detection device on board 55 Angle information transmitted from unmanned air vehicle to onboard communication device 56 Onboard communication device based on tracking result of unmanned air vehicle tracking device Position information of own ship converted by 57 57 Angle information from own ship transmitted from onboard communication device of unmanned air vehicle 58 Position information of own ship transmitted from onboard communication device of unmanned air vehicle 59 Calculation of hit point of unmanned air vehicle Device 60 Predicted hit point instruction information from the unmanned air vehicle's hit point calculation device 61 Predicted hit point instruction information from the onboard communication device 62 Unmanned air vehicle Onboard missile launcher that launches missiles based on angle information from passive electromagnetic wave detection device 63 Position information of unmanned air vehicle from onboard communication device 64 Angle information from onboard communication device 65 Transmitted from missile communication device Angle information from unmanned aerial vehicle 66 Position information of unmanned aerial vehicle transmitted from missile communication device 67 Discard type radio wave detector tracking device of missile guidance device 68 Position information of discard type radio wave detector 69 Transmitted from onboard communication device Angle information from a dump-type radio wave detector 70 Drop-type radio wave detector 71 Communication device equipped with a dump-type radio wave detector 72 Passive electromagnetic wave detector 73 equipped with a dump-type radio wave detector 73 Angle information detected by a passive electromagnetic wave detector 74 Angle information transmitted from the discard type radio wave detection device to the onboard communication device 75 The dump type radio wave detection device Position information of own ship converted by the onboard communication device based on the tracking result of the tracking device. 76 Angle information from own ship transmitted from the communication device mounted on the discard type radio wave detection device 77. Transmitted from communication device mounted on the discard type radio wave detection device. Position information of own ship 78 Hit point calculation device of dumping type radio wave detection device 79 Predicted hit point instruction information from hit point calculation device of dumping type radio wave detection device 80 Predicted hit point instruction information from on-board communication device 81 Includes a hit point calculator 82 Gun 83 Bullet-type radio detection device 84 Communication device equipped with a bullet-type radio detection device 85 Passive electromagnetic wave detection device 86 with a bullet-type radio detection device 86 Angle information detected by a mounted passive electromagnetic detection device 87 Bullet-type radio wave detection device Angle information transmitted from the detection device to the onboard communication device 88 Angle from the bullet-type radio detection device transmitted from the onboard communication device Report 89 Predictive hit point instruction information from the bullet-type radio wave detection device transmitted from the onboard communication device 90 Angle information from the own ship transmitted from the on-board communication device of the bullet-type radio wave detection device 91 Calculation of the hit point of the bullet-type radio wave detection device Device 92 Predicted hit point instruction information from the hit point calculation device of the bullet-type radio wave detection device 93 Predicted hit point instruction information from the onboard communication device 94 Position information of the discard type radio wave detection device from the onboard communication device 95 From the onboard communication device Angle information 96 Angle information from a drop-type radio wave detection device transmitted from a missile communication device 97 Position information of a drop-type radio wave detection device transmitted from a missile communication device 98 Missile guidance device bullet-type radio wave detection device tracking device 99 Bullet-type radio detection device Position information of the bullet-type radio detection device tracked by the tracking device 100 Bullet-type radio detection device from onboard communication device Position information 101 Position information from onboard communication device 102 Angle information from bullet-type radio detection device transmitted from missile communication device 103 Position information of bullet-type radio detection device transmitted from missile communication device 104 Conventional Shooting command device 105 Conventional guided radio wave emitting device 106 Guided radio wave emitted from the guided radio wave emitting device 107 Missile launch signal transmitted from the shooting commanding device to the missile launching device 108 Control transmitted from the shooting conducting device to the guided radio wave emitting device Signal 109 Angle information input processing 110 Position information input processing 111 Start point coordinate setting processing 112 Angle combination processing 113 Intersection coordinate calculation processing 114 Predicted hit point calculation processing 115 Predicted hit point instruction information output processing

Claims (20)

[Claims] 1. An onboard passive electromagnetic wave detection device for detecting electromagnetic waves radiated from an anti-aircraft target, which is mounted on a surface ship.
A missile launcher that inputs angle information from the onboard passive electromagnetic wave detection device to launch a missile, a missile tracking device that tracks the launched missile, receives angle information from the missile, and transmits predicted hit point instruction information to the missile Communication device, inputting angle information from the onboard passive electromagnetic wave detection device, missile position information from the missile tracking device, angle information from the missile from the onboard communication device to calculate the predicted hit point, and the result is onboard the ship. A missile guidance device having a hit point calculation device for transmitting to a missile via a communication device, and a communication device for receiving predicted hit point instruction information from the onboard communication device and transmitting angle information detected by the missile to the onboard communication device , A steering device for inputting predicted hit point instruction information from the communication device to fly a missile to an anti-air target, A missile having a passive electromagnetic wave detection device that detects an electromagnetic wave radiated from a target and transmits the result to a communication device, and has the two passive electromagnetic wave detection devices whose relative distances change. Passive guidance device. 2. An onboard passive electromagnetic wave detection device for detecting electromagnetic waves radiated from an anti-aircraft target, which is mounted on a surface ship.
Missile launcher that inputs angle information from the onboard passive electromagnetic wave detection device to launch a missile, missile tracking device that tracks the launched missile, input missile position information from the missile tracking device and convert it to own ship position information Then send the result to the missile, the missile guidance device having a ship communication device that inputs angle information from the shipboard passive electromagnetic wave detection device and sends it to the missile, and the angle information and the position information of the own ship from the shipboard communication device. A communication device for receiving, a passive electromagnetic wave detecting device for detecting an electromagnetic wave radiated from an air target, and angle information from the passive electromagnetic wave detecting device, the angle information from the onboard communication device and the position information of the own ship from the communication device. Enter the predicted hit point instruction information from the above-mentioned hit point calculation device to calculate the predicted hit point Composed of a missile having a steering device and of flying to-air target missiles, passive induction apparatus, characterized in that the relative distance has the above two passive electromagnetic wave detection device that varies. 3. A shipboard passive electromagnetic wave detection device, which is mounted on a surface ship and detects electromagnetic waves radiated from an anti-aircraft target,
The missile launcher that inputs angle information from the onboard passive electromagnetic wave detection device to launch a missile, the ship-mounted helicopter tracking device that tracks a ship-mounted helicopter, the angle information is received from the ship-mounted helicopter, and the predicted hit point indication information is transmitted to the missile. Calculate the predicted hit point by inputting the angle information from the onboard communication device, the onboard passive electromagnetic wave detection device, the position information of the onboard helicopter from the onboard helicopter tracking device, and the angle information from the onboard helicopter from the onboard communication device. And a missile guidance device having a hit point calculation device for transmitting the result to the missile via the onboard communication device and an electromagnetic wave radiated from an anti-aircraft target and transmitting the result to the onboard communication device. Passive electromagnetic wave detection device, angle information detected by the onboard passive electromagnetic wave detection device A ship-mounted helicopter having an on-board communication device for transmitting to a communication device, a communication device for receiving predicted hit point instruction information from the on-board communication device, and a steering device for inputting predicted hit point instruction information from the communication device to fly a missile to an anti-air target And a missile having, and having the above-mentioned two passive electromagnetic wave detecting devices whose relative distances change. 4. A shipboard passive electromagnetic wave detection device, which is installed in a surface ship and detects electromagnetic waves radiated from an anti-aircraft target,
Position information of own ship by inputting position information of the ship-mounted helicopter from the missile launcher that inputs angle information from the onboard passive electromagnetic wave detection device and launches a missile, the ship-mounted helicopter tracking device that tracks the ship-mounted helicopter, and the ship-mounted helicopter tracking device To the ship-based helicopter, the angle information from the ship-based helicopter and the angle information from the ship-based helicopter, and the angle information from the ship-based communication device. Position information is received, an onboard communication device that transmits predicted hit point indication information to the missile, an onboard passive electromagnetic wave detection device that detects an electromagnetic wave radiated from an air target, angle information from the onboard passive electromagnetic wave detection device, Input the angle information from the onboard communication device and the position information of the ship from the above onboard communication device to predict A ship-borne helicopter having a hit point calculation device for calculating points, a communication device for receiving predicted hit point instruction information from the onboard communication device, and steering for inputting predicted hit point instruction information from the communication device to fly a missile to an anti-aircraft target A passive induction device comprising the above-mentioned two passive electromagnetic wave detection devices that change in relative distance. 5. A shipboard passive electromagnetic wave detection device equipped on a surface ship to detect electromagnetic waves radiated from an anti-aircraft target,
An on-board helicopter tracking device that tracks the on-board helicopter, inputs the position information of the on-board helicopter from the above-mentioned on-board helicopter tracking device, converts it to the own ship's position information, sends the result to the on-board helicopter, and receives the angle information from the on-board passive electromagnetic wave detection device. A missile guidance device having an onboard communication device for inputting and transmitting to the onboard helicopter, an onboard communication device for receiving angle information and position information of the own ship from the onboard communication device, and transmitting predicted hit point instruction information to the missile, An on-board passive electromagnetic wave detection device that detects electromagnetic waves radiated from an anti-aircraft target, an on-board missile launcher that inputs angle information from the on-board passive electromagnetic wave detection device to launch a missile, and an angle from the on-board passive electromagnetic wave detection device Information is predicted from the onboard communication device by inputting the angle information from the onboard communication device and the position information of the own ship. A ship-borne helicopter having a hit point calculation device for calculating points, a communication device for receiving predicted hit point instruction information from the onboard communication device, and input of predicted hit point instruction information from the communication device to fly a missile to an anti-aircraft target. And a missile having a steering device, the passive guidance device having the two passive electromagnetic wave detection devices whose relative distances change. 6. A shipboard passive electromagnetic wave detection device, which is mounted on a surface ship and detects electromagnetic waves radiated from an anti-aircraft target,
A ship-mounted helicopter tracking device that tracks a ship-mounted helicopter, a missile tracking device that tracks a missile, input missile position information from the missile tracking device, convert it to the ship's position information, and send the result to the missile. A missile guidance device having an onboard communication device for inputting position information of the onboard helicopter from the device and transmitting it to the missile, and for inputting angle information from the onboard passive electromagnetic wave detection device and transmitting it to the missile, and radiation from an air target On-board passive electromagnetic wave detection device for detecting electromagnetic waves, on-board communication device for inputting angle information from the on-board passive electromagnetic wave detection device and transmitting it to the missile, and for inputting angle information from the on-board passive electromagnetic wave detection device to the missile An onboard helicopter having an onboard missile launcher for launching, angled from the onboard communication device Information, the position information of the ship and the position information of the ship-based helicopter, a communication device that receives the angle information from the onboard passive electromagnetic wave detection device from the onboard communication device, from the communication device, from the onboard passive electromagnetic wave detection device Angle information, angle information from the onboard communication device, position information of own ship and position information of ship-mounted helicopter are input to calculate the predicted hit point, the predicted hit point instruction information from the hit point calculation device. And a missile having a steering device for inputting and flying the missile to the air target,
A passive induction device comprising the above-mentioned two passive electromagnetic wave detection devices whose relative distance changes. 7. A shipboard passive electromagnetic wave detection device, which is mounted on a surface ship and detects electromagnetic waves radiated from an anti-aircraft target,
An on-board helicopter tracking device that tracks the on-board helicopter, an on-board communication device that receives angle information from the above-mentioned on-board helicopter and transmits predicted hit point indication information to a missile, and the above-mentioned on-board helicopter tracking device based on the above-mentioned on-board passive electromagnetic wave detection device. From the on-board helicopter position information from the on-board communication device, the angle information from the on-board helicopter is input to calculate the predicted hit point, and the result is transmitted to the missile via the on-board communication device. A missile guidance device and an on-board passive electromagnetic wave detection device that detects electromagnetic waves radiated from an anti-aircraft target and transmits the result to the on-board communication device, and angle information detected by the on-board passive electromagnetic wave detection device to the on-board communication device On-board communication device to transmit,
A ship-borne helicopter having a missile launching device that launches a missile by inputting angle information from the onboard passive electromagnetic wave detection device, a communication device that receives predicted hit point instruction information from the onboard communication device, and a predicted hit point instruction from the communication device A passive guidance device comprising: a missile having a steering device for inputting information and causing the missile to fly to an anti-air target; and the two passive electromagnetic wave detection devices having relative distances that change. 8. A shipboard passive electromagnetic wave detection device, which is mounted on a surface ship and detects electromagnetic waves radiated from an anti-aircraft target,
The missile launcher that inputs the angle information from the onboard passive electromagnetic wave detection device to launch the missile, the unmanned aerial vehicle tracking device that tracks the unmanned aerial vehicle, the angle information from the unmanned aerial vehicle, and receives the predicted hit point instruction information. Prediction by inputting angle information from the onboard communication device that transmits to the missile, the above-mentioned passive electromagnetic wave detection device on the ship, position information of the unmanned air vehicle from the unmanned air vehicle tracking device, and angle information from the unmanned air vehicle from the onboard communication device A missile guidance device having a hit point calculation device for calculating a hit point and transmitting the result to the missile via the onboard communication device, and an electromagnetic wave radiated from an anti-aircraft target is detected and the result is sent to the onboard communication device. There is an onboard passive electromagnetic wave detection device for transmitting, and an onboard communication device for transmitting the angle information detected by the onboard passive electromagnetic wave detection device to the onboard communication device. A missile having an unmanned air vehicle, a communication device that receives predicted hit point instruction information from the onboard communication device, and a steering device that inputs the predicted hit point instruction information from the communication device and causes the missile to fly to an anti-aircraft target. ,
A passive induction device comprising the above-mentioned two passive electromagnetic wave detection devices whose relative distance changes. 9. An onboard passive electromagnetic wave detection device for detecting an electromagnetic wave radiated from an anti-aircraft target, which is mounted on a surface ship.
Input the position information of the unmanned aerial vehicle from the unmanned aerial vehicle tracking device, the unmanned aerial vehicle tracking device that tracks the unmanned aerial vehicle, the missile launcher that inputs the angle information from the onboard passive electromagnetic wave detection device to launch the missile A missile guidance device having a shipboard communication device for converting the position information of the ship and transmitting the result to an unmanned air vehicle, and inputting angle information from the onboard passive electromagnetic wave detection device to the unmanned air vehicle.
An onboard communication device that receives angle information and own ship position information from the onboard communication device, and transmits predicted hit point indication information to the missile, onboard passive electromagnetic wave detection device that detects electromagnetic waves radiated from an air target, An unmanned aerial vehicle having a hit point calculation device for calculating a predicted hit point by inputting angle information from the upper passive electromagnetic wave detection device, angle information from the onboard communication device from the onboard communication device, and position information of the own ship, the above aircraft A missile having a communication device that receives predicted hit point instruction information from the upper communication device and a steering device that inputs the predicted hit point instruction information from the communication device and causes the missile to fly to an air-to-air target. 2. A passive induction device having the above-mentioned two passive electromagnetic wave detection devices. 10. A shipboard passive electromagnetic wave detection device equipped on a surface ship for detecting electromagnetic waves radiated from an anti-aircraft target, an unmanned air vehicle tracking device for tracking an unmanned air vehicle, and an unmanned air vehicle from the unmanned air vehicle tracking device. A missile having an onboard communication device that inputs position information, converts it to the position information of the own ship, transmits the result to an unmanned air vehicle, and inputs angle information from the above ship passive electromagnetic wave detection device and transmits to the unmanned air vehicle An onboard communication device that receives angle information and own ship position information from the onboard communication device and the above ship communication device, and transmits predicted hit point indication information to the missile, onboard passive electromagnetic wave detection that detects electromagnetic waves radiated from anti-aircraft targets Device, an on-board missile launcher that inputs angle information from the on-board passive electromagnetic wave detection device to launch a missile, and an angle from the on-board passive electromagnetic wave detection device An unmanned air vehicle that has a hit point calculation device that calculates the predicted hit point by inputting the angle information from the onboard communication device and the position information of the own ship from the above onboard communication device, the predicted hit point from the above onboard communication device The two passive electromagnetic waves, each of which has a communication device that receives instruction information and a steering device that inputs predicted hit point instruction information from the communication device and causes the missile to fly to an air-to-air target, the relative distance of which changes. A passive guidance device having a detection device. 11. A shipboard passive electromagnetic wave detection device equipped on a surface ship for detecting electromagnetic waves radiated from an anti-aircraft target, an unmanned air vehicle tracking device for tracking an unmanned air vehicle, a missile tracking device for tracking a missile, and the above missile tracking. The position information of the missile is input from the device and converted to the position information of the own ship, the result is sent to the missile, the position information of the unmanned aerial vehicle is input from the unmanned air vehicle tracking device and sent to the missile, and the onboard passive A missile guidance device having an onboard communication device for inputting angle information from an electromagnetic wave detection device and transmitting it to a missile, an onboard passive electromagnetic wave detection device for detecting an electromagnetic wave radiated from an anti-aircraft target, from the onboard passive electromagnetic wave detection device On-board communication device that inputs angle information and sends it to the missile, by inputting angle information from the on-board passive electromagnetic wave detection device An unmanned aerial vehicle having an on-board missile launcher for launching missiles, angle information from the onboard communication device, position information of own ship and position information of the unmanned aerial vehicle, from the onboard communication device to the onboard passive electromagnetic wave detection device. A communication device that receives angle information, from the communication device, the angle information from the onboard passive electromagnetic wave detection device, the angle information from the onboard communication device, the position information of the own ship, and the position information of the unmanned air vehicle are input. A missile having a hit point calculation device for calculating a predicted hit point and a steering device for inputting predicted hit point instruction information from the hit point calculation device to cause the missile to fly to an air-to-air target. A passive induction device having two passive electromagnetic wave detection devices. 12. A shipboard passive electromagnetic wave detection device for detecting an electromagnetic wave radiated from an anti-aircraft target, an unmanned air vehicle tracking device for tracking an unmanned air vehicle, and angle information received from the unmanned air vehicle for prediction. Onboard communication device that transmits hit point indication information to the missile, angle information from the onboard passive electromagnetic wave detection device, position information of the unmanned air vehicle from the unmanned air vehicle tracking device, angle from the unmanned air vehicle from the onboard communication device Enter the information to calculate the predicted hit point,
A missile guidance device having a hit point calculation device for transmitting the result to a missile via an onboard communication device, and an onboard passive electromagnetic wave detection device for detecting an electromagnetic wave radiated from an anti-aircraft target and transmitting the result to the onboard communication device An unmanned vehicle having an on-board communication device that transmits angle information detected by the on-board passive electromagnetic wave detection device to the on-board communication device, and a missile launcher that inputs angle information from the on-board passive electromagnetic wave detection device and launches a missile A missile having a flying object, a communication device that receives predicted hit point instruction information from the onboard communication device, and a steering device that inputs the predicted hit point instruction information from the communication device and causes the missile to fly to an anti-aircraft target, A passive induction device comprising the above-mentioned two passive electromagnetic wave detection devices whose relative distance changes. 13. A shipboard passive electromagnetic wave detection device equipped on a surface ship for detecting electromagnetic waves radiated from an anti-aircraft target, a missile launcher for inputting angle information from the shipboard passive electromagnetic wave detection device to launch a missile, and a discard type. Discard-type radio wave detection device tracking device for tracking radio wave detection device, on-board communication device that receives angle information from the above-mentioned dump-type radio wave detection device, and transmits predicted hit point instruction information to the missile, angle information from the on-board passive electromagnetic wave detection device , The position information of the discard type radio detection device from the discard type radio detection device tracking device, the angle information from the discard type radio detection device from the onboard communication device is input to calculate the predicted hit point, the result A missile guidance device having a hit point calculation device for transmitting the missile via the onboard communication device and an electromagnetic wave radiated from an anti-aircraft target are detected. A passive electromagnetic wave detection device that transmits the result to the onboard communication device, a dump type radio wave detection device having an onboard communication device that transmits the angle information detected by the onboard passive electromagnetic wave detection device to the onboard communication device, and is predicted from the onboard communication device A communication device for receiving the hit point instruction information,
A missile having a steering device for inputting predicted hit point instruction information from the communication device and causing the missile to fly to an air-to-air target, and having the two passive electromagnetic wave detection devices having relative distances changed. Passive guidance device. 14. A shipboard passive electromagnetic wave detection device equipped on a surface ship for detecting electromagnetic waves radiated from an anti-aircraft target, a missile launcher for inputting angle information from the shipboard passive electromagnetic wave detection device to launch a missile, and a discard type. Discard-type radio detection device tracking device for tracking radio detection device, inputting position information of the discard-type radio detection device from the above-mentioned discard-type radio detection device tracking device and converting it to position information of own ship, and the result is the above-mentioned discard-type radio detection device Missile guidance device having an onboard communication device that transmits to the device, inputs angle information from the onboard passive electromagnetic wave detection device and sends to the dumping type radio wave detection device, and angle information and own ship position information from the onboard communication device. Onboard communication device that receives information from the target and sends predicted hit point indication information to the missile, onboard passive electromagnetic that detects electromagnetic waves radiated from the air target Wave detection device, dumping having a hit point calculation device for calculating a predicted hit point by inputting angle information from the onboard passive electromagnetic wave detection device, angle information from the onboard communication device and onboard position information from the onboard communication device Type radio wave detection device, a communication device that receives predicted hit point instruction information from the on-board communication device, and a missile that has a steering device that inputs predicted hit point instruction information from the communication device and causes the missile to fly to an anti-aircraft target A passive induction device having the two passive electromagnetic wave detection devices whose relative distances change. 15. A shipboard passive electromagnetic wave detection device equipped on a surface ship for detecting electromagnetic waves radiated from an anti-aircraft target, a missile launching device for launching a missile by inputting predicted hit point instruction information from a hit point calculation device, and a cannonball Onboard communication device that receives angle information from a type radio wave detection device and transmits predicted hit point indication information to a missile, a gun that launches the cannonball type radio wave detection device, angle information from the onboard passive electromagnetic wave detection device, and onboard communication The angle information from the bullet-type radio detection device is input from the device, the predicted hit point is calculated together with the position information of the bullet-type radio detection device calculated from the table of the ammunition, and the result is passed via the onboard communication device. Missile guidance device that has a hit point calculation device that transmits it to the missile and electromagnetic waves radiated from an anti-aircraft target, and transmits the result to the onboard communication device Onboard passive electromagnetic wave detection device,
From the communication device, a bullet-type radio wave detection device having an onboard communication device for transmitting the angle information detected by the onboard passive electromagnetic wave detection device to the onboard communication device, a communication device for receiving predicted hit point instruction information from the onboard communication device, A passive guidance device comprising: a missile having a steering device for inputting predicted hit point instruction information and causing the missile to fly to an anti-air target, and the two passive electromagnetic wave detection devices having relative distances changed. . 16. A shipboard passive electromagnetic wave detection device equipped on a surface ship for detecting electromagnetic waves radiated from an anti-aircraft target, a missile launcher for inputting predicted hit point instruction information from a shipboard communication device to launch a missile, and a shell type. A missile guidance device having a gun for launching a radio wave detection device, a shipboard communication device for inputting angle information from the shipboard passive electromagnetic wave detection device and transmitting it to the shell-type radio wave detection device, and receiving angle information from the shipboard communication device However, the onboard communication device that transmits the predicted hit point instruction information to the missile and the onboard communication device, the onboard passive electromagnetic wave detection device that detects the electromagnetic waves radiated from the air target, the angle information from the onboard passive electromagnetic wave detection device, and the onboard communication. The angle information from the onboard communication device is input from the device, and it is the position information of the bullet-type radio detection device calculated from the table of the cannonball. From the communication device that receives the predicted hit point instruction information from the on-board communication device, the cannonball type radio wave detection device that has the hit point calculation device that calculates the predicted hit point together with the result of backward calculation of the position information of the ship A passive guidance device comprising: a missile having a steering device for inputting predicted hit point instruction information and causing the missile to fly to an anti-air target, and the two passive electromagnetic wave detection devices having relative distances changed. . 17. A ship-mounted passive electromagnetic wave detection device for detecting electromagnetic waves radiated from an anti-aircraft target, a dumping type radio wave detection device tracking device for tracking a dumping type radio wave detection device, and a missile tracking device for tracking a missile. , The missile launcher that inputs the angle information from the onboard passive electromagnetic wave detection device to launch the missile, input the missile position information from the missile tracking device and convert it to the own ship position information, and send the result to the missile, A missile having an onboard communication device that inputs position information of the dumping type radio wave detection device from the dumping type radio wave detection device tracking device and transmits it to the missile, and inputs angle information from the onboard passive electromagnetic wave detection device and transmits it to the missile Induction device and on-board passive electromagnetic wave detection device for detecting electromagnetic waves radiated from an air target A dumping type radio wave detection device having an on-board communication device for inputting angle information from an electromagnetic wave detection device and transmitting it to a missile, angle information from the onboard communication device, position information of own ship and position information of the dumping type radio wave detection device, A communication device that receives angle information from the onboard passive electromagnetic wave detection device from the onboard communication device, angle information from the onboard passive electromagnetic wave detection device from the communication device, angle information from the onboard communication device, and position information of the own ship And a hitting point calculation device for calculating the predicted hit point by inputting the position information of the dumping type radio wave detection device, and a steering device for inputting the predicted hit point instruction information from the hit point calculation device and causing the missile to fly to the anti-aircraft target. A passive induction device comprising the above-mentioned two passive electromagnetic wave detection devices that change in relative distance. 18. A shipboard passive electromagnetic wave detection device for detecting electromagnetic waves radiated from an anti-aircraft target, a cannonball type radio wave detection device tracking device for tracking a cannonball type radio wave detection device, and a missile tracking device for tracking a missile. , The missile launcher that inputs the angle information from the onboard passive electromagnetic wave detection device to launch the missile, input the missile position information from the missile tracking device and convert it to the own ship position information, and send the result to the missile, A missile having an on-board communication device that inputs position information of the bullet-type radio detection device from the above-mentioned bullet-type radio detection device tracking device and transmits it to the missile, and inputs angle information from the onboard passive electromagnetic wave detection device and transmits to the missile. Induction device and on-board passive electromagnetic wave detection device for detecting electromagnetic waves radiated from an air target A bullet-type radio wave detection device having an on-board communication device that inputs angle information from an electromagnetic wave detection device and transmits it to a missile, the on-board communication device carries angle information, own ship position information, and bullet-type radio wave detection device position information. A communication device that receives angle information from the onboard passive electromagnetic wave detection device from the communication device, angle information from the onboard passive electromagnetic wave detection device from the communication device, angle information from the onboard communication device, position information of the own ship, and shell type A missile having a hit point calculation device for inputting position information of a radio wave detection device and calculating a predicted hit point, and a steering device for inputting predicted hit point instruction information from the hit point calculation device to fly the missile to an anti-aircraft target. And a passive induction device having the above-mentioned two passive electromagnetic wave detection devices whose relative distance changes. 19. A shipboard passive electromagnetic wave detection device equipped on a surface ship for detecting electromagnetic waves radiated from an anti-aircraft target, a missile launcher for inputting angle information from the shipboard passive electromagnetic wave detection device to launch a missile, and a ship-based helicopter. The carrier-based helicopter tracking device that tracks the missile, the missile tracking device that tracks the missile, input the missile position information from the missile tracking device, convert it to the ship's position information, and send the result to the missile. A missile guidance device having an onboard communication device for inputting position information of the onboard helicopter and transmitting it to the missile, and inputting angle information from the onboard passive electromagnetic wave detection device and transmitting it to the missile, and electromagnetic waves radiated from the anti-aircraft target On-board passive electromagnetic wave detection device to detect, is it the on-board passive electromagnetic wave detection device? Ship-mounted helicopter having an on-board communication device for inputting angle information from the on-board communication device, and angle information, own ship position information and ship-mounted helicopter position information from the on-board communication device, and on-board passive electromagnetic waves from the on-board communication device A communication device that receives angle information from a detection device, from the communication device, the angle information from the onboard passive electromagnetic wave detection device, the angle information from the onboard communication device, the position information of the own ship, and the position information of the ship-based helicopter. A missile having a hit point calculation device for inputting and calculating a predicted hit point, and a steering device for inputting predicted hit point instruction information from the hit point calculation device and causing the missile to fly to an anti-aircraft target,
A passive induction device comprising the above-mentioned two passive electromagnetic wave detection devices whose relative distance changes. 20. A shipboard passive electromagnetic wave detection device equipped on a surface ship for detecting an electromagnetic wave radiated from an anti-aircraft target, a missile launcher for inputting angle information from the shipboard passive electromagnetic wave detection device to launch a missile, and an unmanned flight An unmanned aerial vehicle tracking device that tracks the body, a missile tracking device that tracks a missile, input missile position information from the above missile tracking device, convert it to own ship position information, and send the result to the missile, unmanned air vehicle tracking Radiation from an anti-aircraft target and a missile guidance device having an onboard communication device that inputs position information of an unmanned air vehicle from the device and transmits it to the missile, and inputs angle information from the onboard passive electromagnetic wave detection device and transmits it to the missile An on-board passive electromagnetic wave detection device that detects electromagnetic waves, and the angle information is input from the on-board passive electromagnetic wave detection device An unmanned air vehicle having an on-board communication device for transmitting to an aircraft, angle information from the above-mentioned on-board communication device, own ship position information and unmanned air vehicle position information, and an angle from the above-mentioned on-board communication device to the on-board passive electromagnetic wave detection device. Communication device that receives information, from the communication device, the angle information from the onboard passive electromagnetic wave detection device, the angle information from the onboard communication device, the position information of the own ship, and the position information of the unmanned aerial vehicle are predicted hits The hit point calculation device for calculating a point, and the missile having a steering device for inputting predicted hit point instruction information from the hit point calculation device and causing the missile to fly to an air-to-air target. The passive induction device having the passive electromagnetic wave detection device of.