CN110645831A - Auxiliary sighting device for improving hitting precision of ground missile - Google Patents
Auxiliary sighting device for improving hitting precision of ground missile Download PDFInfo
- Publication number
- CN110645831A CN110645831A CN201911150702.7A CN201911150702A CN110645831A CN 110645831 A CN110645831 A CN 110645831A CN 201911150702 A CN201911150702 A CN 201911150702A CN 110645831 A CN110645831 A CN 110645831A
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- auxiliary
- oil liquid
- cavity
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- improving
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
- F41F1/00—Launching apparatus for projecting projectiles or missiles from barrels, e.g. cannons; Harpoon guns
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41G—WEAPON SIGHTS; AIMING
- F41G1/00—Sighting devices
- F41G1/06—Rearsights
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41G—WEAPON SIGHTS; AIMING
- F41G1/00—Sighting devices
- F41G1/46—Sighting devices for particular applications
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Optics & Photonics (AREA)
- Lighting Device Outwards From Vehicle And Optical Signal (AREA)
Abstract
The invention discloses an auxiliary sighting device for improving the precision of ground-oriented missile striking, which comprises a base, wherein the left end and the right end of the base are symmetrically provided with balance supports, each balance support comprises a rib plate hinged on the end surface of the base, an oil liquid cavity arranged in the rib plate, an adjusting rod connected to the inner wall of the lower end of the oil liquid cavity in a sliding manner, and a hose communicated and connected between the oil liquid cavities, the invention adopts the relation of dynamic oil liquid balance to arrange left and right symmetrical support parts, firstly ensures the horizontal precision of a signal sighting device, improves the precision of a struck target, simultaneously adopts a light refraction mode to focus circularly distributed auxiliary light rays and main light rays to be emitted out from the same emission tube in parallel, enhances the light rays to clearly guide signals, arranges equipment on an arc-shaped track and carries out rotation control in a gear meshing mode to accurately change the sighting angle, realize the semi-automatic guiding striking aiming with high precision.
Description
Technical Field
The invention relates to the technical field of weapon sights, in particular to an auxiliary sight for improving the hitting precision of a ground missile.
Background
In the information digital war era, the communication and automatic control technology is utilized to strike the long-distance target with gunfire, and the method is a conventional combat means. The guidance system comprises active homing guidance, semi-active homing guidance and passive homing guidance, wherein the semi-active homing guidance depends on energy irradiated on a target, and the missile receives energy reflected by the target to carry out fire striking.
Conventional pilot sights are single infrared emitters. Because impurities in the outside air can refract light, reflected signals are not strong enough, the precision of the missile attacking target is influenced, and the handheld launching sighting device has insufficient guiding precision. The present invention sets forth a device that solves the above problems.
Disclosure of Invention
The technical problem is as follows:
conventional pilot sights are single infrared emitters. Impurities in the outside air can refract light, so that the reflected signal is not strong enough, and the precision of the missile attacking the target is influenced.
In order to solve the problems, the embodiment designs an auxiliary sighting device for improving the hitting precision of the ground missile, and the auxiliary sighting device for improving the hitting precision of the ground missile comprises a base, wherein balance supports are symmetrically arranged at the left end and the right end of the base, each balance support comprises a rib plate hinged to the end surface of the base, an oil liquid cavity arranged in each rib plate, an adjusting rod connected to the inner wall of the lower end of each oil liquid cavity in a sliding manner, and a hose communicated with the oil liquid cavities, oil liquid in the oil liquid cavity at the extrusion side is conveyed to the other side through the hose to push the adjusting rod at the other side to keep the base horizontal, a transmission cavity is arranged in the base, an arc-shaped track is arranged at the upper end of the transmission cavity, an arc-shaped track is connected in the arc-shaped track in a sliding manner, a gathering box is arranged at the upper end of the arc-shaped rack, and a refraction cavity is, the inner wall of the upper end of the refraction cavity is provided with a transmitting tube in a through way, the lower end of the transmitting tube is provided with a transmitting device, the transmitting device comprises an integrated board fixed at the lower end of the transmitting tube, a main lamp fixed at the upper end of the integrated board and positioned in the transmitting tube, eight auxiliary lamps arranged on the integrated board in an annular array, eight rotating grooves arranged on the integrated board in the annular array and a light screen rotationally connected in the rotating grooves, the light screen rotationally shields and changes light rays, so that the light rays of the auxiliary lamps are coincided with the light rays of the main lamp and are emitted from the transmitting tube, a lifting disc is slidably connected in the refraction cavity, a starting assembly is arranged in the lifting disc and comprises eight push rods arranged on the lifting disc and in the annular array, the light screen is pushed by the push rods to rotate, and a steering device is arranged, the steering device comprises a telescopic shaft which is rotatably connected in the transmission cavity and a reversing gear which is arranged on the telescopic shaft and is meshed and connected with the lower end of the arc-shaped rack, and the arc-shaped rack slides to change the orientation of the gathering box through the meshing rotation of the reversing gear and the arc-shaped rack.
Preferably, the push rod has a length decreasing in a one-sided direction.
Preferably, the lower end of the integrated plate is provided with eight switches in an annular array, and each switch independently controls a single auxiliary lamp.
The balance support further comprises a supporting leg hinged to the lower end of the adjusting rod, and a resistance spring is connected between the adjusting rod and the inner wall of the lower end of the oil cavity.
The transmitting device further comprises a steering mirror arranged on the side end face of the light screen close to the symmetrical center, a torque spring is connected between the light screen and the rotating groove, eight fold line holes capable of receiving light rays are arranged in the transmitting tube in a penetrating mode, a gathering ring arranged at the upper end of each fold line hole is arranged in the transmitting tube, and the inclined plane inclination angle of the steering mirror is the same as the inclination angle of the end face of the inner ring of the gathering ring.
Wherein, the start-up subassembly still include sliding connection in on the lifter plate and eight of annular array link up the post, link up post and self homonymy push rod length proportion is invariable, be equipped with the ascending holding tank of opening in linking up the post, holding tank sliding connection have with the pressing plate of switch butt, press the pressing plate lower extreme with be connected with compression spring between the holding tank lower extreme inner wall, the holding tank upper end is equipped with the ring that resets, the ring with be connected with reset spring between the lifter plate, refraction intracavity rotate be connected with the screw rod of lifter plate threaded connection, screw rod lower extreme power is connected with embedded in motor in refraction chamber bottom inner wall, the motor with the auxiliary lamp with electric power is connected between the main lamp.
The steering device further comprises a knob arranged on the telescopic shaft and located on the outer side of the rear end of the transmission cavity, a synchronous plate located in the front end of the knob is arranged on the telescopic shaft, a sliding rod is connected to the inner wall of the rear end of the transmission cavity in a sliding mode, a friction block capable of being abutted to the reversing gear is arranged on the sliding rod, and the rear end of the sliding rod is fixedly connected with the synchronous plate.
The invention has the beneficial effects that: according to the invention, bilateral symmetrical supporting parts are arranged in a relation of dynamic oil balance, the horizontal accuracy of the signal aiming device is firstly ensured, the accuracy of a target to be struck is improved, meanwhile, the light rays of the auxiliary lamp and the main lamp which are distributed in an annular manner are gathered and emitted out from the same emission tube in parallel in a light ray refraction mode, the clear guide signal of the light ray bundle is enhanced, the equipment is arranged on an arc-shaped track and is rotationally controlled in a gear meshing mode, the aiming angle is accurately changed, and the high-precision semi-automatic guide striking aiming is realized.
Drawings
For ease of illustration, the invention is described in detail by the following specific examples and figures.
FIG. 1 is a schematic overall structure diagram of an auxiliary sighting device for improving the hitting precision of a ground missile according to the invention;
FIG. 2 is a schematic view of the structure in the direction "A-A" of FIG. 1;
FIG. 3 is a schematic view of the structure in the direction "B-B" of FIG. 1;
FIG. 4 is a schematic view of the interior structure of the adapter column of FIG. 1.
Detailed Description
The invention will now be described in detail with reference to fig. 1-4, for ease of description, the orientations described below will now be defined as follows: the up, down, left, right, and front-back directions described below correspond to the up, down, left, right, and front-back directions in the projection relationship of fig. 1 itself.
The invention relates to an auxiliary sighting device for improving the hitting precision of a ground missile, which is mainly applied to the aiming process of improving the guidance of semi-active homing, and the invention is further explained by combining the attached drawings of the invention:
the invention relates to an auxiliary sighting device for improving the hitting precision of a ground missile, which comprises a base 31, wherein balance supports 901 are symmetrically arranged at the left end and the right end of the base 31, each balance support 901 comprises a rib plate 35 hinged to the end surface of the base 31, an oil cavity 36 arranged in the rib plate 35, an adjusting rod 38 connected to the inner wall of the lower end of the oil cavity 36 in a sliding manner, and a hose 40 communicated and connected between the oil cavities 36, wherein oil in the oil cavity 36 at the extruded side is delivered to the other side through the hose 40 to push the adjusting rod 38 at the other side to keep the base 31 horizontal, a transmission cavity 32 is arranged in the base 31, an arc-shaped track 32 is arranged at the upper end of the transmission cavity 32, an arc-shaped rack 29 is connected in the arc-shaped track 27 in a sliding manner, a gathering box 11 is arranged at the upper end of the arc-shaped rack 29, a refraction cavity 12 is arranged in the gathering, the inner wall of the upper end of the refraction cavity 12 is provided with a transmitting tube 18 in a penetrating manner, the lower end of the transmitting tube 18 is provided with a transmitting device 902, the transmitting device 902 comprises an integration plate 22 fixed at the lower end of the transmitting tube 18, a main lamp 20 fixed at the upper end of the integration plate 22 and positioned in the transmitting tube 18, eight auxiliary lamps 21 arranged on the integration plate 22 in an annular array manner, eight rotary grooves 14 arranged on the integration plate 22 in an annular array manner, and a light shielding plate 19 rotatably connected in the rotary grooves 14, the light shielding plate 19 rotates to shield and change light rays, so that the light rays of the auxiliary lamps 21 are overlapped with the light rays of the main lamp 20 and emitted from the transmitting tube 18, the refraction cavity 12 is connected with a lifting disc 25 in a sliding manner, a starting assembly 903 is arranged in the lifting disc 25, the starting assembly 903 comprises eight push rods 23 arranged on the lifting disc 25 and in an annular array manner, and the light shielding, the steering device 904 is arranged in the transmission cavity 32 and comprises an expansion shaft 33 rotatably connected in the transmission cavity 32 and a reversing gear 34 arranged on the expansion shaft 33 and meshed with the lower end of the arc-shaped rack 29, and the arc-shaped rack 29 slides to change the orientation of the gathering box 11 through the meshing rotation of the reversing gear 34 and the arc-shaped rack 29.
Advantageously, the length of the push rod 23 decreases in the unilateral direction, which ensures that a time difference between the front and the rear starting is generated.
Advantageously, the lower end of the integrated board 22 is provided with eight switches 26 in an annular array, and each switch 26 independently controls a single secondary lamp 21, so that orderly and gradually enhanced light generation and signal enhancement are ensured.
According to an embodiment, the following detailed description is provided for the balance bracket 901, the balance bracket 901 further includes a support leg 39 hinged to the lower end of the adjusting rod 38, a resistance spring 37 is connected between the adjusting rod 38 and the inner wall of the lower end of the oil liquid chamber 36, and the adjusting rod 38 is slidably reset by the elastic force of the resistance spring 37 when the device is not required to be fixedly disengaged from the ground.
According to an embodiment, the transmitting device 902 is described in detail below, the transmitting device 902 further includes a steering mirror 13 disposed on an end surface of the light shielding plate 19 close to the symmetric center, a torque spring 47 is connected between the light shielding plate 19 and the rotating groove 14, eight fold holes 17 capable of receiving light rays are penetratingly disposed in the transmitting tube 18, a gathering ring 16 located at an upper end of the fold hole 17 is disposed in the transmitting tube 18, an inclined plane inclination angle of the steering mirror 13 is the same as an inner ring end surface inclination angle of the gathering ring 16, so that the relationship of the sub-lamp 21 is guaranteed, after the steering mirror 13 and the gathering ring 16 are refracted, to be parallel to the light rays of the main lamp 20 and to be emitted from the transmitting tube 18.
According to an embodiment, the starting assembly 903 is described in detail below, the starting assembly 903 further includes eight connecting posts 46 connected to the lifting plate 25 in an annular array, the length ratio of the connecting posts 46 to the push rod 23 on the same side of the starting assembly is constant, an accommodating groove 43 with an upward opening is formed in each connecting post 46, a pressing plate 44 connected to the switch 26 in a sliding manner is connected to the accommodating groove 43, a compression spring 45 is connected between the lower end of the pressing plate 44 and the inner wall of the lower end of the accommodating groove 43, a return ring 41 is arranged at the upper end of the accommodating groove 43, a return spring 42 is connected between the return ring 41 and the lifting plate 25, a screw 24 connected to the lifting plate 25 in a threaded manner is rotatably connected to the refraction cavity 12, a motor 30 embedded in the inner wall of the bottom end of the refraction cavity 12 is connected to the lower end of the screw 24 in a power manner, and the motor 30 is electrically connected to the auxiliary lamp 21 and the, the lengths of the connecting columns 46 are different, and a time difference exists between the front and the back, the switch 26 is pressed to light the auxiliary lamp 21, so that the guide signal is enhanced step by step.
According to an embodiment, the following detailed description is provided for a steering device 904, the steering device 904 further includes a knob 48 disposed on the telescopic shaft 33 and located outside the rear end of the transmission cavity 32, a synchronizing plate 49 located in the front end of the knob 48 is disposed on the telescopic shaft 33, a sliding rod 50 is slidably connected to the inner wall of the rear end of the transmission cavity 32, a friction block 51 capable of abutting against the reversing gear 34 is disposed on the sliding rod 50, the rear end of the sliding rod 50 is fixedly connected to the synchronizing plate 49, and the synchronizing plate 49 pushes the friction block 51 to disengage from the abutment against the reversing gear 34 through the sliding rod 50, so that the reversing gear 34 is rotated to adjust the orientation of the device while unlocking the device.
The following detailed description of the steps of using the auxiliary sight for improving the accuracy of hitting a ground missile in the present disclosure with reference to fig. 1 to 4:
initially, the oil amount in the oil chamber 36 is the same, so that the resistance spring 37 does not elastically deform when the adjusting rod 38 is placed, the light screen 19 is unfolded outwards, the lifting disc 25 is located at the lowest end of the refraction chamber 12, and the longest push rod 23 and the longest connecting column 46 are respectively abutted against the light screen 19 and the switch 26 on the side.
When the device is placed, the supporting feet 39 are placed on a fixed horizontal plane, if the horizontal plane has a height difference, the supporting feet 39 at a high position push the oil in the oil chamber 36 at a high position to pass through the hose 40 to reach the supporting feet 39 at a low position through the adjusting rod 38 at the high position, and at the moment, the oil in the oil chamber 36 at the low position increases to push the adjusting rod 38 at the low position to move downwards, so that the supporting feet 39 are positioned on the same horizontal plane, and the accuracy of a guide target is guaranteed;
when a single set of aiming light is emitted, the motor 30 is started, the main lamp 20 is lightened through electric power, and a guide signal is emitted from the emission tube 18 to a target;
when the guide signal is required to be enhanced, the motor 30 is started to rotate through the screw rod 24 and the screw thread of the lifting disk 25 to enable the lifting disk 25 to move upwards, the auxiliary lamp 21 at the changed side is turned on through the abutting of the pressing plate 44 and the switch 26, the push rod 23 pushes the shading plate 19 at the side to turn over, so that the light of the turned-on auxiliary lamp 21 enters the transmitting tube 18 from the broken line hole 17 through the refraction of the steering mirror 13, the light emitted by the auxiliary lamp 21 is parallel to the light of the main lamp 20 through the refraction of the gathering ring 16 and is emitted from the upper end of the transmitting tube 18 to carry out target striking guide, and in the subsequent process of moving upwards the lifting disk 25, the remaining auxiliary lamps 21 are turned on one by one through the same steps to enhance the light, the guide signal is clear, the switch 26 at the turned-on auxiliary lamp 21 side slides into the accommodating groove 43, and the pressing plate 44 is pushed to extrude the compression spring 45 for self-adaptive adjustment, and penguins are accommodated, the reset ring 41 is abutted with the integrated board 22 and moves downwards relative to the lifting disc 25 to press the reset spring 42;
when the irradiation angle needs to be changed, the synchronous plate 49 is manually pushed to move forwards, the friction block 51 is separated from the butting connection with the reversing gear 34 through the main lamp 20, the reversing gear 34 is rotated through the telescopic shaft 33 through the manual rotating knob 48, the reversing gear 34 rotates the arc-shaped rack 29 through meshing, the arc-shaped rack 29 slides in the arc-shaped track 27 to change the orientation of the gathering box 11, and the light angle emitted by the emitting tube 18 is changed.
The invention has the beneficial effects that: according to the invention, bilateral symmetrical supporting parts are arranged in a relation of dynamic oil balance, the horizontal accuracy of the signal aiming device is firstly ensured, the accuracy of a target to be struck is improved, meanwhile, the light rays of the auxiliary lamp and the main lamp which are distributed in an annular manner are gathered and emitted out from the same emission tube in parallel in a light ray refraction mode, the clear guide signal of the light ray bundle is enhanced, the equipment is arranged on an arc-shaped track and is rotationally controlled in a gear meshing mode, the aiming angle is accurately changed, and the high-precision semi-automatic guide striking aiming is realized.
In the above manner, a person skilled in the art can make various changes depending on the operation mode within the scope of the present invention.
Claims (7)
1. The utility model provides an improve supplementary sight to ground guided missile hitting precision, includes the base, its characterized in that: the left end and the right end of the base are symmetrically provided with balance brackets;
the balance support comprises a rib plate hinged to the end face of the base, an oil liquid cavity arranged in the rib plate, an adjusting rod connected to the inner wall of the lower end of the oil liquid cavity in a sliding mode, and a hose communicated and connected between the oil liquid cavities, oil liquid in the oil liquid cavity on the extruded side is conveyed to the other side through the hose and used for pushing the adjusting rod on the other side to keep the base horizontal, a transmission cavity is arranged in the base, an arc-shaped rail is arranged at the upper end of the transmission cavity, an arc-shaped rail is connected in the arc-shaped rail in a sliding mode, a gathering box is arranged at the upper end of the arc-shaped rack, a refraction cavity is arranged in the gathering box, and a transmitting pipe is arranged on the inner wall;
the lower end of the transmitting tube is provided with a transmitting device, the transmitting device comprises an integrated board fixed at the lower end of the transmitting tube, a main lamp fixed at the upper end of the integrated board and positioned in the transmitting tube, eight auxiliary lamps arranged on the integrated board in an annular array, eight rotating grooves arranged on the integrated board in an annular array and a light shielding plate rotationally connected in the rotating grooves, the light shielding plate rotationally shields and changes light rays, so that the light rays of the auxiliary lamps are coincided with the light rays of the main lamp and are emitted out of the transmitting tube, and a lifting disc is slidably connected in the refraction cavity;
be equipped with the starting assembly in the lifter plate, the starting assembly including set up in eight push rods of just annular array on the lifter plate, through the push rod promotes the light screen rotates, be equipped with in the transmission intracavity and turn to the device, turn to the device including rotate connect in telescopic shaft in the transmission intracavity, set up in on the telescopic shaft and with the switching-over gear that the meshing of arc rack lower extreme is connected, through switching-over gear with the meshing of arc rack rotates, makes the arc rack slides and changes gather together the case orientation.
2. An auxiliary sight for improving the accuracy of the attack of a ground missile as claimed in claim 1, wherein: the length of the push rod decreases progressively in the unilateral direction.
3. An auxiliary sight for improving the accuracy of the attack of a ground missile as claimed in claim 1, wherein: eight switches are arranged on the annular array at the lower end of the integrated board, and each switch independently controls a single auxiliary lamp.
4. An auxiliary sight for improving the accuracy of the attack of a ground missile as claimed in claim 1, wherein: the balance support further comprises a supporting leg hinged to the lower end of the adjusting rod, and a resistance spring is connected between the adjusting rod and the inner wall of the lower end of the oil cavity.
5. An auxiliary sight for improving the accuracy of the attack of a ground missile as claimed in claim 1, wherein: the transmitting device further comprises a steering mirror arranged on the side end face of the light screen close to the symmetrical center, a torque spring is connected between the light screen and the rotating groove, eight fold line holes capable of receiving light rays are arranged in the transmitting tube in a penetrating mode, a gathering ring located at the upper end of each fold line hole is arranged in the transmitting tube, and the inclined plane inclination angle of the steering mirror is the same as the end face inclination angle of the inner ring of the gathering ring.
6. An auxiliary sight for improving the accuracy of the attack of a ground missile as claimed in claim 3, wherein: the start-up subassembly still include sliding connection in on the lifter plate and eight of annular array link up the post, link up post and self homonymy push rod length proportion is invariable, be equipped with the ascending holding tank of opening in linking up the post, sliding connection have in the holding tank with the press platen of switch butt, press platen lower extreme with be connected with compression spring between the holding tank lower extreme inner wall, the holding tank upper end is equipped with the ring that resets, the ring with be connected with reset spring between the lifter plate, the refraction intracavity rotate be connected with the screw rod of lifter plate thread connection, screw rod lower extreme power is connected with embedded in motor in refraction chamber bottom inner wall, the motor with the auxiliary lamp with electric power is connected between the main lamp.
7. An auxiliary sight for improving the accuracy of the attack of a ground missile as claimed in claim 1, wherein: the steering device further comprises a knob arranged on the telescopic shaft and located on the outer side of the rear end of the transmission cavity, a synchronous plate located in the front end of the knob is arranged on the telescopic shaft, a sliding rod is connected to the inner wall of the rear end of the transmission cavity in a sliding mode, a friction block capable of being abutted to the reversing gear is arranged on the sliding rod, and the rear end of the sliding rod is fixedly connected with the synchronous plate.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201911150702.7A CN110645831B (en) | 2019-11-21 | 2019-11-21 | Auxiliary sighting device for improving hitting precision of ground missile |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201911150702.7A CN110645831B (en) | 2019-11-21 | 2019-11-21 | Auxiliary sighting device for improving hitting precision of ground missile |
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| Publication Number | Publication Date |
|---|---|
| CN110645831A true CN110645831A (en) | 2020-01-03 |
| CN110645831B CN110645831B (en) | 2020-09-18 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201911150702.7A Expired - Fee Related CN110645831B (en) | 2019-11-21 | 2019-11-21 | Auxiliary sighting device for improving hitting precision of ground missile |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112504011A (en) * | 2020-12-24 | 2021-03-16 | 中国人民解放军空军工程大学 | Ground-to-air missile weapon system killer area calculation model system |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2107880C1 (en) * | 1995-02-23 | 1998-03-27 | Конструкторское бюро приборостроения | Scanning device of beam guidance system |
| US5992292A (en) * | 1993-03-05 | 1999-11-30 | Stn Atlas Elektronic Gmbh | Fire control device for, in particular, transportable air defense systems |
| CN206479091U (en) * | 2017-01-20 | 2017-09-08 | 中国航天科工集团上海浦东开发中心 | A kind of portable a variety of MISSILE LAUNCHING hunting gears |
| CN109556459A (en) * | 2019-01-22 | 2019-04-02 | 中国人民解放军陆军工程大学 | Rocket gun inertial navigation north-seeking precision detection system and method |
-
2019
- 2019-11-21 CN CN201911150702.7A patent/CN110645831B/en not_active Expired - Fee Related
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5992292A (en) * | 1993-03-05 | 1999-11-30 | Stn Atlas Elektronic Gmbh | Fire control device for, in particular, transportable air defense systems |
| RU2107880C1 (en) * | 1995-02-23 | 1998-03-27 | Конструкторское бюро приборостроения | Scanning device of beam guidance system |
| CN206479091U (en) * | 2017-01-20 | 2017-09-08 | 中国航天科工集团上海浦东开发中心 | A kind of portable a variety of MISSILE LAUNCHING hunting gears |
| CN109556459A (en) * | 2019-01-22 | 2019-04-02 | 中国人民解放军陆军工程大学 | Rocket gun inertial navigation north-seeking precision detection system and method |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112504011A (en) * | 2020-12-24 | 2021-03-16 | 中国人民解放军空军工程大学 | Ground-to-air missile weapon system killer area calculation model system |
| CN112504011B (en) * | 2020-12-24 | 2022-10-14 | 中国人民解放军空军工程大学 | Ground-to-air missile weapon system killing area calculation model system |
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| CN110645831B (en) | 2020-09-18 |
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Effective date of registration: 20200803 Address after: Room 1701, 17 / F, building 2, Xizi international Ginza, Nanyuan street, Yuhang District, Hangzhou City, Zhejiang Province Applicant after: HANGZHOU BAIZE FANGZHOU TECHNOLOGY Co.,Ltd. Address before: No. 10, Xingang street, Zhongxin Town, Zengcheng District, Guangzhou City, Guangdong Province Applicant before: Guangzhou Haoxiang Optical Instrument Co.,Ltd. |
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