CN116164586A - Assembly for accurate shooting calibration of target range - Google Patents
Assembly for accurate shooting calibration of target range Download PDFInfo
- Publication number
- CN116164586A CN116164586A CN202211567725.XA CN202211567725A CN116164586A CN 116164586 A CN116164586 A CN 116164586A CN 202211567725 A CN202211567725 A CN 202211567725A CN 116164586 A CN116164586 A CN 116164586A
- Authority
- CN
- China
- Prior art keywords
- shooting
- positioning
- orientation
- connecting rods
- parallel
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41G—WEAPON SIGHTS; AIMING
- F41G1/00—Sighting devices
- F41G1/54—Devices for testing or checking ; Tools for adjustment of sights
Landscapes
- Physics & Mathematics (AREA)
- Optics & Photonics (AREA)
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
Description
技术领域technical field
本发明属于导弹发射技术领域,具体涉及一种用于靶场精确射向标定的组件。The invention belongs to the technical field of missile launching, and in particular relates to a component used for precise shooting calibration in a shooting range.
背景技术Background technique
射向标定用于确定导弹/火箭弹发射的初始方位角,对其精度要求很高。对于惯性制导导弹/火箭弹,初始射向实际测量值与理论射向之间的误差直接影响导弹/火箭弹命中精度。目前常用的射向标定方法主要有直瞄式和双经纬仪射向标定方法。Shooting calibration is used to determine the initial azimuth angle of missile/rocket launch, which requires high accuracy. For inertial guided missiles/rockets, the error between the actual measured value of the initial shooting direction and the theoretical shooting direction directly affects the hit accuracy of the missile/rocket. At present, the commonly used calibration methods mainly include direct-pointing and double-theodolite calibration methods.
1.直瞄式射向标定方法1. Direct aiming calibration method
通过人眼直瞄或借助炮瞄镜的方法对射向进行标定,操作简便,易于上手,但精度相对较差,且易受天气影响,当借助炮瞄镜进行标定时,对人员操作水平要求较高。Calibrate the shooting direction by direct sighting with the human eye or with the help of the gun sight, which is easy to operate and easy to use, but the accuracy is relatively poor and is easily affected by the weather. higher.
2.双经纬仪射向标定方法2. Double theodolite calibration method
通过双经纬仪检测发射装置射向与空间已知基准方向的夹角,与理论射向进行对比,对发射装置射向进行标定。该方法精度相对较高,但操作麻烦,标定时间长,对人员操作要求高,对于地面基准射向精度要求高,易受天气影响。The angle between the launching device's shooting direction and the known reference direction in space is detected by the double theodolite, and compared with the theoretical shooting direction, the shooting device's shooting direction is calibrated. The accuracy of this method is relatively high, but the operation is cumbersome, the calibration time is long, the requirements for personnel operation are high, the accuracy of ground reference shooting is high, and it is easily affected by the weather.
发明内容Contents of the invention
(一)要解决的技术问题(1) Technical problems to be solved
本发明要解决的技术问题是:如何快速简便精确的对发射装置射向进行标定。The technical problem to be solved by the present invention is: how to quickly, easily and accurately calibrate the shooting direction of the transmitting device.
(二)技术方案(2) Technical solutions
为了解决上述技术问题,本发明提供一种用于靶场精确射向标定的组件,所述组件包括:定位定向装置1、转接装置2及定向接口3;In order to solve the above-mentioned technical problems, the present invention provides a component for accurate shooting calibration in the shooting range, the component includes: a positioning and
所述定位定向装置1固定在转接装置2上;The positioning and
所述固定安装有定位定向装置1的转接装置2通过定向接口3安装在发射装置上;The
通过所述定向接口3与发射装置上对应接口的匹配设置,确保定位定向装置1的寻北射向与发射装置的射向保持平行。Through the matching setting of the
所述通过所述定向接口3与发射装置上对应接口的匹配设置,确保定位定向装置1的寻北射向,表示:使得定位定向装置1的三个姿态轴与发射装置的姿态轴平行,其中方位轴与发射装置射向平行。The matching setting of the
其中,所述转接装置2的结构包括:四根立柱,四根连接杆;Wherein, the structure of the
所述四根立柱相互平行设置,形成矩形方框的外围竖直结构,四根立柱各自的下端部,相邻两两之间通过所述四根连接杆连接;由此所述四根连接杆,形成为两对平行的连接杆。The four uprights are arranged parallel to each other to form a peripheral vertical structure of a rectangular box, and the respective lower ends of the four uprights are connected between adjacent two by the four connecting rods; thus the four connecting rods , formed as two pairs of parallel connecting rods.
其中,所述两对平行的连接杆中,其中一对平行的连接杆上,分别设有两个连接孔,两个连接杆上共计4个连接孔,所述定位定向装置1的四个角通过所述4个连接孔,固定安装在转接装置2上。Wherein, among the two pairs of parallel connecting rods, two connecting holes are respectively provided on the pair of parallel connecting rods, and there are 4 connecting holes in total on the two connecting rods. The four corners of the positioning and
其中,所述两对平行的连接杆中,其中一对平行的连接杆上安装定位定向装置1,另一对平行的连接杆与该安装定位定向装置1的一对连接杆相互垂直。Among the two pairs of parallel connecting rods, the positioning and
其中,建立坐标系,定义所述立柱的延伸方向为Z轴,垂直于Z轴的平面为X-Y平面,将所述固定安装定位定向装置1的一对平行的连接杆的延伸方向定义为X轴,则另一对平行的连接杆的延伸方向则为Y轴。Wherein, a coordinate system is established, the extension direction of the column is defined as the Z axis, the plane perpendicular to the Z axis is the X-Y plane, and the extension direction of a pair of parallel connecting rods of the fixed installation positioning and
其中,所述X轴方向即为所述定位定向装置1的寻北射向。Wherein, the X-axis direction is the north-seeking direction of the positioning and
其中,在将所述固定安装有定位定向装置1的转接装置2通过定向接口3安装在发射装置上,并通过所述定向接口3确保定位定向装置1的寻北射向与发射装置的射向保持平行之后,Wherein, the
所述定位定向装置1上电寻北,寻北结束后,即可实时输出当前发射装置北向角信息。The positioning and
其中,分析计算当前发射装置的射向与理论射向之间的差值,调整发射装置射向至理论射向位置。Wherein, analyzing and calculating the difference between the shooting direction of the current launching device and the theoretical shooting direction, and adjusting the shooting direction of the launching device to the theoretical shooting position.
其中,该组件不受天气影响,精度高,可以实时输出当前射向信息,且对人员要求不高,不受人员操作误差的影响。Among them, this component is not affected by the weather, has high precision, can output current shooting information in real time, and has low requirements for personnel, and is not affected by personnel operation errors.
(三)有益效果(3) Beneficial effects
与现有技术相比较,本发明与现有技术相比较,本发明的有益技术效果:操作简单,不受天气影响,对人员操作水平要求低,精度高且可实时输出射向信息。Compared with the prior art, the present invention has the beneficial technical effects: simple operation, not affected by the weather, low requirements on personnel operation level, high precision and real-time output of shooting information.
该方法简单、可靠,具有很大的推广应用空间。The method is simple, reliable, and has great potential for popularization and application.
该方法已在相关项目上应用,定位定向装置方位定位精度优于1mil,加工转接装置定向接口跨距为500mm,定向接口与发射装置发射导轨之间间隙为0.5mm,转接装置与发射装置之间定向误差不大于1mil,定位定向装置与转接装置之间定向误差靠机械加工精度保证,误差可忽略不计,进而保证了整个测试系统的精度,采用此方法已成功为10余发导弹/火箭弹精确标定射向,标定速度快,效率高,人为误差小,发射后通过对测试数据进行判读,射向标定精度较高,满足制导控制要求。This method has been applied in related projects. The azimuth positioning accuracy of the positioning and directional device is better than 1mil. The span of the directional interface of the processing transfer device is 500mm. The gap between the directional interface and the launching rail of the launching device is 0.5mm. The orientation error between them is not more than 1mil. The orientation error between the positioning and orientation device and the adapter device is guaranteed by the machining accuracy, and the error is negligible, thereby ensuring the accuracy of the entire test system. This method has been successfully used for more than 10 rounds of missiles/ The rocket is accurately calibrated, with fast calibration speed, high efficiency, and small human error. After the launch, the test data is interpreted, and the accuracy of the calibration is high, which meets the guidance and control requirements.
附图说明Description of drawings
图1为定位定向装置与转接装置配合示意图;Figure 1 is a schematic diagram of the cooperation between the positioning and orientation device and the adapter device;
图2为某发射装置采用本发明所述组件进行射向标定的示意图。Fig. 2 is a schematic diagram of a launch device using the components described in the present invention to perform calibration.
具体实施方式Detailed ways
为使本发明的目的、内容和优点更加清楚,下面结合附图和实施例,对本发明的具体实施方式作进一步详细描述。In order to make the purpose, content and advantages of the present invention clearer, the specific implementation manners of the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments.
为了解决上述技术问题,本发明提供一种用于靶场精确射向标定的组件,所述组件包括:定位定向装置1、转接装置2及定向接口3;In order to solve the above-mentioned technical problems, the present invention provides a component for accurate shooting calibration in the shooting range, the component includes: a positioning and
所述定位定向装置1固定在转接装置2上;The positioning and
所述固定安装有定位定向装置1的转接装置2通过定向接口3安装在发射装置上;The
通过所述定向接口3与发射装置上对应接口的匹配设置,确保定位定向装置1的寻北射向与发射装置的射向保持平行。Through the matching setting of the
所述通过所述定向接口3与发射装置上对应接口的匹配设置,确保定位定向装置1的寻北射向,表示:使得定位定向装置1的三个姿态轴与发射装置的姿态轴平行,其中方位轴与发射装置射向平行。The matching setting of the
其中,所述转接装置2的结构包括:四根立柱,四根连接杆;Wherein, the structure of the
所述四根立柱相互平行设置,形成矩形方框的外围竖直结构,四根立柱各自的下端部,相邻两两之间通过所述四根连接杆连接;由此所述四根连接杆,形成为两对平行的连接杆。The four uprights are arranged parallel to each other to form a peripheral vertical structure of a rectangular box, and the respective lower ends of the four uprights are connected between adjacent two by the four connecting rods; thus the four connecting rods , formed as two pairs of parallel connecting rods.
其中,所述两对平行的连接杆中,其中一对平行的连接杆上,分别设有两个连接孔,两个连接杆上共计4个连接孔,所述定位定向装置1的四个角通过所述4个连接孔,固定安装在转接装置2上。Wherein, among the two pairs of parallel connecting rods, two connecting holes are respectively provided on the pair of parallel connecting rods, and there are 4 connecting holes in total on the two connecting rods. The four corners of the positioning and
其中,所述两对平行的连接杆中,其中一对平行的连接杆上安装定位定向装置1,另一对平行的连接杆与该安装定位定向装置1的一对连接杆相互垂直。Among the two pairs of parallel connecting rods, the positioning and
其中,建立坐标系,定义所述立柱的延伸方向为Z轴,垂直于Z轴的平面为X-Y平面,将所述固定安装定位定向装置1的一对平行的连接杆的延伸方向定义为X轴,则另一对平行的连接杆的延伸方向则为Y轴。Wherein, a coordinate system is established, the extension direction of the column is defined as the Z axis, the plane perpendicular to the Z axis is the X-Y plane, and the extension direction of a pair of parallel connecting rods of the fixed installation positioning and
其中,所述X轴方向即为所述定位定向装置1的寻北射向。Wherein, the X-axis direction is the north-seeking direction of the positioning and
其中,在将所述固定安装有定位定向装置1的转接装置2通过定向接口3安装在发射装置上,并通过所述定向接口3确保定位定向装置1的寻北射向与发射装置的射向保持平行之后,Wherein, the
所述定位定向装置1上电寻北,寻北结束后,即可实时输出当前发射装置北向角信息。The positioning and
其中,分析计算当前发射装置的射向与理论射向之间的差值,调整发射装置射向至理论射向位置。Wherein, analyzing and calculating the difference between the shooting direction of the current launching device and the theoretical shooting direction, and adjusting the shooting direction of the launching device to the theoretical shooting position.
其中,该组件不受天气影响,精度高,可以实时输出当前射向信息,且对人员要求不高,不受人员操作误差的影响,Among them, the component is not affected by the weather, has high precision, can output current shooting information in real time, and has low requirements for personnel, and is not affected by personnel operation errors.
实施例1Example 1
本发明含有定位定向装置1和转接装置2,其中转接装置2用于固定安装定位定向装置1,同时还可以通过定向接口3将转接装置2和定位定向装置1固定于发射装置上,具体步骤如下:The present invention includes a positioning and
1)设计加工转接装置2用于固定安装定位定向装置1,且保证转接装置2的X轴方向与定位定向装置1的射向保持平行;1) Design and process the
2)将转接装置2连同定位定向装置1安装在发射装置上,同时通过定向接口3确保定位定向装置1射向与发射装置射向保持平行;2) Install the
3)定位定向装置1上电寻北,寻北结束后,即可实时输出当前发射装置北向角等信息;3) The positioning and
4)分析计算当前射向与理论射向之间的差值,调整发射装置射向至理论射向位置。4) Analyze and calculate the difference between the current shooting direction and the theoretical shooting direction, and adjust the launching device to shoot to the theoretical shooting position.
以上所述仅是本发明的优选实施方式,应当指出,对于本技术领域的普通技术人员来说,在不脱离本发明技术原理的前提下,还可以做出若干改进和变形,这些改进和变形也应视为本发明的保护范围。The above is only a preferred embodiment of the present invention, it should be pointed out that for those of ordinary skill in the art, without departing from the technical principle of the present invention, some improvements and modifications can also be made. It should also be regarded as the protection scope of the present invention.
Claims (10)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202211567725.XA CN116164586A (en) | 2022-12-07 | 2022-12-07 | Assembly for accurate shooting calibration of target range |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202211567725.XA CN116164586A (en) | 2022-12-07 | 2022-12-07 | Assembly for accurate shooting calibration of target range |
Publications (1)
Publication Number | Publication Date |
---|---|
CN116164586A true CN116164586A (en) | 2023-05-26 |
Family
ID=86412145
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN202211567725.XA Pending CN116164586A (en) | 2022-12-07 | 2022-12-07 | Assembly for accurate shooting calibration of target range |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN116164586A (en) |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4093154A (en) * | 1953-02-19 | 1978-06-06 | Walter G. Finch | Target seeking gyro for a missile |
CN101162142A (en) * | 2007-11-27 | 2008-04-16 | 北京航空航天大学 | Positioning mechanism for two-position north-seeker |
WO2017026956A2 (en) * | 2015-08-13 | 2017-02-16 | Aselsan Elektronik Sanayi Ve Ticaret Anonim Sirketi | An artillery surveying device |
CN114111753A (en) * | 2021-12-27 | 2022-03-01 | 中国人民解放军61540部队 | A fiber optic gyroscope north finder |
-
2022
- 2022-12-07 CN CN202211567725.XA patent/CN116164586A/en active Pending
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4093154A (en) * | 1953-02-19 | 1978-06-06 | Walter G. Finch | Target seeking gyro for a missile |
CN101162142A (en) * | 2007-11-27 | 2008-04-16 | 北京航空航天大学 | Positioning mechanism for two-position north-seeker |
WO2017026956A2 (en) * | 2015-08-13 | 2017-02-16 | Aselsan Elektronik Sanayi Ve Ticaret Anonim Sirketi | An artillery surveying device |
CN114111753A (en) * | 2021-12-27 | 2022-03-01 | 中国人民解放军61540部队 | A fiber optic gyroscope north finder |
Non-Patent Citations (1)
Title |
---|
李从善;高峰端;乔彦峰;: "同一基座式非陀螺寻北瞄准方案研究", 仪器仪表学报, no. 1, 12 October 2006 (2006-10-12), pages 32 - 33 * |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN111044994B (en) | Optical axis calibration device and method for airborne laser range finder of airplane | |
CN109373833B (en) | Combined measurement method suitable for initial attitude and speed of spinning projectile | |
CN112698580B (en) | Semi-physical simulation system and simulation method suitable for infrared accurate guided bomb | |
CN104089529B (en) | Use the method and apparatus that fibre optic gyroscope is calibrated fighter plane armament systems | |
CN103868528B (en) | Measuring method for attitude measuring precision of shooting range optical measuring equipment | |
CN107478450A (en) | A kind of tracking accuracy detecting system with dynamic simulation target simulation function | |
CN113865432A (en) | Self-propelled artillery barrel orientation detection method | |
CN111060141A (en) | Aircraft axial calibration device and method based on inertial navigation and optical measurement | |
CN108008368A (en) | A kind of object localization method based on echo Doppler Information revision angle error | |
CN111141282B (en) | Positioning and aiming control method and device based on Loongson processor and aiming computer | |
CN104535053A (en) | Gun adjustment precision detection system based on satellite positioning | |
CN110285708B (en) | A rapid detection method for north-seeking accuracy of self-propelled artillery positioning and orientation system | |
CN105675323B (en) | A kind of ground test method of satellite structure heat endurance | |
CN113790739B (en) | Space attitude calibration device and calibration method for aircraft gun | |
CN104833268B (en) | Small caliber piece dynamic tracking accuracy detecting device | |
CN111551072A (en) | Method for leading out axis of gun barrel | |
CN112414209B (en) | Projectile coordinate testing method and device for acquiring cannon jump angle | |
CN101858712B (en) | A Digital Calibration Method for Aircraft Cannon Applied to Aircraft Assembly | |
CN112162239B (en) | Impact point positioning method based on horizontal gate array | |
CN116164586A (en) | Assembly for accurate shooting calibration of target range | |
CN203928892U (en) | The equipment that uses fibre optic gyroscope to calibrate fighter plane armament systems | |
CN112464457A (en) | Jumping angle calculation method and device based on artillery initial segment coordinates | |
CN110109164B (en) | Vehicle-mounted azimuth angle transfer alignment device and method | |
CN115685778A (en) | Radar-seeking aircraft miss distance estimation method based on radio frequency semi-physical simulation | |
CN109764752B (en) | Rapid initial alignment method for reducing machining precision requirement of individual-soldier guided rocket |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PB01 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination |