CN104535053A - Gun adjustment precision detection system based on satellite positioning - Google Patents
Gun adjustment precision detection system based on satellite positioning Download PDFInfo
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Abstract
本发明公开了一种基于卫星定位的调炮精度检测系统,涉及火炮技术领域;包括卫星、炮膛轴线标定仪及其夹具、定位定向主机、零相位天线和外接显控器;所述炮膛轴线标定仪包括激光发射端和激光接收端,所述激光发射端和激光接收端分别通过夹具固定在火炮身管的两端,所述激光发射端和激光接收端的顶端分别固定有零相位天线;所述外接显控器与定位定向主机连接;两零相位天线与定位定向主机有线或无线连接。本发明结构简单,操作方便,大大提高了测试效率,节省了人力和测试时间,调炮精度测试精确;用途广泛,特别适用高炮的调炮精度检查。
The invention discloses a gun adjustment accuracy detection system based on satellite positioning, which relates to the technical field of guns; including a satellite, a gun bore axis calibration instrument and its fixture, a positioning and orientation host, a zero-phase antenna and an external display controller; the gun bore axis calibration The instrument includes a laser emitting end and a laser receiving end, the laser emitting end and the laser receiving end are respectively fixed on the two ends of the artillery barrel by a clamp, and the tops of the laser emitting end and the laser receiving end are respectively fixed with a zero-phase antenna; The external display controller is connected to the positioning and directional host; the two zero-phase antennas are wired or wirelessly connected to the positioning and directional host. The invention has the advantages of simple structure, convenient operation, greatly improved test efficiency, saving manpower and test time, accurate test of gun adjustment accuracy, wide application, and is especially suitable for inspection of gun adjustment accuracy of anti-aircraft guns.
Description
技术领域 technical field
本发明涉及火炮技术领域。 The invention relates to the technical field of artillery.
背景技术 Background technique
调炮精度是调炮完成后火炮身管实际指向与输入诸元决定的期望指向之间的差值。它反映的是当火控系统发出高低、方位目标值后,火炮随动系统将火力轴线调转到指定位置后与理论值之间的误差。目前,在地炮、自行火炮和火箭炮的调炮精度检查中主要采用双经纬仪空间交会法、图像识别法、角位移传感器法和全站仪法等方法。但是在高炮测量中,由于高炮可以360度旋转,当身管旋转角度大于90度时,高炮图像识别法、角位移传感器法和全站仪法等方法由于不能定位炮口的标记点,因此不能实现高炮调炮精度检测。双经纬仪交汇法虽然能够实现一定范围的调炮精度的检测,但是这种方法需要两台经纬仪,测试时需要首先确定两标记点,再进行两经纬仪的布站,其所需测试设备多、测试项目多、所需人员多、人为因素大;并且,当高炮身管转动较大角度时,为找准标记点,经常需要调整经纬仪的位置,增大了测试难度,延长了测试周期;且在测试时还会出现炮塔挡住定位点的情况,即使调整经纬仪的位置也无法进行测量。因而,采用双经纬仪交汇法,其试验周期长,检查条件苛刻,人为因素大,难以反映真正的精度指标要求。 The gun adjustment accuracy is the difference between the actual orientation of the gun barrel and the expected orientation determined by the input parameters after the gun adjustment is completed. It reflects the error between the theoretical value after the fire control system sends out the height and azimuth target values, and the artillery follow-up system transfers the firepower axis to the designated position. At present, methods such as double theodolite space intersection method, image recognition method, angular displacement sensor method and total station method are mainly used in the gun adjustment accuracy inspection of ground artillery, self-propelled artillery and rocket launcher. However, in the measurement of anti-aircraft guns, since the anti-aircraft guns can rotate 360 degrees, when the barrel rotation angle is greater than 90 degrees, methods such as image recognition methods, angular displacement sensor methods, and total station methods cannot locate the marking points of the muzzle. , so the accuracy detection of anti-aircraft gun adjustment cannot be realized. Although the double theodolite intersection method can achieve a certain range of gun adjustment accuracy detection, this method requires two theodolites. During the test, it is necessary to first determine the two marking points, and then carry out the two theodolites. There are many projects, many personnel are required, and human factors are large; and, when the antiaircraft gun barrel rotates at a large angle, in order to find the marking point, it is often necessary to adjust the position of the theodolite, which increases the difficulty of the test and prolongs the test cycle; and During the test, the turret blocked the positioning point, even if the position of the theodolite was adjusted, it could not be measured. Therefore, the use of double theodolite intersection method has long test period, harsh inspection conditions, large human factors, and it is difficult to reflect the real accuracy index requirements.
发明内容 Contents of the invention
本发明所要解决的技术问题是提供一种基于卫星定位的调炮精度检测系统,结构简单,操作方便,大大提高了测试效率,节省了人力和测试时间,调炮精度测试精确;用途广泛,特别适用高炮的调炮精度检查。 The technical problem to be solved by the present invention is to provide a detection system for gun adjustment accuracy based on satellite positioning. It is suitable for checking the adjustment accuracy of anti-aircraft guns.
为解决上述技术问题,本发明所采取的技术方案是: In order to solve the problems of the technologies described above, the technical solution adopted in the present invention is:
一种基于卫星定位的调炮精度检测系统,包括卫星、炮膛轴线标定仪及其夹具、定位定向主机、零相位天线和外接显控器;所述炮膛轴线标定仪包括激光发射端和激光接收端,所述激光发射端和激光接收端分别通过夹具固定在火炮身管的两端,所述激光发射端和激光接收端的顶端分别固定有零相位天线;所述外接显控器与定位定向主机连接;两零相位天线与定位定向主机有线或无线连接; A gun adjustment accuracy detection system based on satellite positioning, including a satellite, a gun bore axis calibration instrument and its fixture, a positioning and orientation host, a zero-phase antenna, and an external display controller; the gun bore axis calibration instrument includes a laser emitting end and a laser receiving end , the laser emitting end and the laser receiving end are respectively fixed on the two ends of the gun barrel by clamps, and the tops of the laser emitting end and the laser receiving end are respectively fixed with a zero-phase antenna; the external display controller is connected to the positioning and directional host ; The two zero-phase antennas are wired or wirelessly connected to the positioning and directional host;
调炮前,调节炮膛轴线标定仪以使激光发射端上设有的激光发射器发射的激光线与激光接收端上设有的十字靶板对准,实现两零相位天线与炮膛轴线的一致性标定;启动定位定向主机,两零相位天线接收卫星的定位信号,并将定位信号传输到定位定向主机; Before adjusting the gun, adjust the bore axis calibration instrument so that the laser line emitted by the laser emitter on the laser emitting end is aligned with the cross target plate on the laser receiving end to achieve the consistency between the two zero-phase antennas and the bore axis Calibration; start the positioning and orientation host, the two zero-phase antennas receive the positioning signal of the satellite, and transmit the positioning signal to the positioning and orientation host;
调炮时,两零相位天线同时接收多个卫星的定位信号;调炮后,定位定向主机对载波信号的相位信号进行处理,得到方位与高低两个方向的调炮角度,根据手动或电动目标值,计算出调炮精度,并将调炮精度结果值发送到外接显控器进行显示。 When adjusting the gun, the two zero-phase antennas receive the positioning signals of multiple satellites at the same time; after the gun is adjusted, the positioning and directional host processes the phase signal of the carrier signal to obtain the angle of the gun in the azimuth and high and low directions. According to the manual or electric target value, calculate the gun adjustment accuracy, and send the gun adjustment accuracy result value to an external monitor for display.
进一步的技术方案,所述的激光发射端包括激光发射器、第一支杆和第一调节钮,所述激光发射器固定于第一支杆的一侧面,所述第一调节钮位于第一支杆上;所述激光接收端包括十字靶板、第二支杆和第二调节钮,十字靶板固定于第二支杆的顶端,第二调节钮位于第二支杆上。 In a further technical solution, the laser emitting end includes a laser emitter, a first pole and a first adjustment button, the laser emitter is fixed on one side of the first pole, and the first adjustment knob is located on the first on the pole; the laser receiving end includes a cross target board, a second pole and a second adjustment button, the cross target board is fixed on the top of the second pole, and the second adjustment knob is located on the second pole.
进一步的技术方案,所述的卫星为北斗卫星,所述的定位定向主机包括北斗RNSS射频模块和处理模块,所述北斗RNSS射频模块用于接收北斗卫星的RNSS射频信号,并将信号发送给处理模块进行处理;所述零相位天线为北斗二号零电气相位中心天线。 In a further technical solution, the satellite is a Beidou satellite, and the positioning and orientation host includes a Beidou RNSS radio frequency module and a processing module, and the Beidou RNSS radio frequency module is used to receive the Beidou satellite's RNSS radio frequency signal, and send the signal to the processing module module for processing; the zero-phase antenna is the Beidou-2 zero-electric phase central antenna.
采用上述技术方案所产生的有益效果在于:本发明结构简单,操作方便,大大提高了测试效率,节省了人力和测试时间,调炮精度测试精确;用途广泛,特别适用高炮的调炮精度检查;基于北斗RNSS的载波相位定位原理,定位数据准确,能够提高测试结果的准确性;设有的炮膛轴线标定仪能够精确校准两个天线的相对位置,进一步提高测试结果的准确性;设有的定位定向主机和外接显控器能够对测试数据进行运算与显示,无需人为计算,自动化程度高,节省了人力和测试时间,提高了测试效率。 The beneficial effects produced by adopting the above-mentioned technical solution are: the present invention has simple structure, convenient operation, greatly improves the test efficiency, saves manpower and test time, and the accuracy test of gun adjustment is accurate; it is widely used, and is especially suitable for checking the accuracy of gun adjustment of anti-aircraft guns ;Based on the carrier phase positioning principle of Beidou RNSS, the positioning data is accurate, which can improve the accuracy of the test results; the equipped gun bore axis calibration instrument can accurately calibrate the relative position of the two antennas, and further improve the accuracy of the test results; The positioning and directional host and the external display controller can calculate and display the test data without manual calculation. The degree of automation is high, which saves manpower and test time and improves test efficiency.
附图说明 Description of drawings
图1是本发明结构示意图; Fig. 1 is a structural representation of the present invention;
图2是本发明激光发射端结构示意图; Fig. 2 is a structural schematic diagram of the laser emitting end of the present invention;
图3是本发明激光接收端结构示意图; Fig. 3 is a schematic diagram of the structure of the laser receiving end of the present invention;
在附图中:1、定位定向主机,2、卫星,3、炮膛轴线标定仪,4、零相位天线,5、夹具,6、火炮身管,7、外接显控器,8、十字靶板,9、第一支杆,10、第一调节钮,11、激光发射器,12、定位轴,13、第二调节钮,14、第二支杆。 In the attached drawings: 1. Positioning and orientation host, 2. Satellite, 3. Gun bore axis calibration instrument, 4. Zero-phase antenna, 5. Fixture, 6. Gun barrel, 7. External display controller, 8. Cross target board , 9, the first pole, 10, the first adjustment button, 11, the laser transmitter, 12, the positioning shaft, 13, the second adjustment button, 14, the second pole.
具体实施方式 Detailed ways
下面结合附图和具体实施方式对本发明作进一步详细的说明。 The present invention will be further described in detail below in conjunction with the accompanying drawings and specific embodiments.
如图1所示,基于卫星定位的调炮精度检测系统,包括卫星2、炮膛轴线标定仪3及其夹具5、定位定向主机1、零相位天线4和外接显控器7。炮膛轴线标定仪3包括激光发射端和激光接收端,激光发射端和激光接收端分别通过夹具5固定在火炮身管6的两端。如图2所示,的激光发射端包括激光发射器11、第一支杆9和第一调节钮10。激光发射器11固定于第一支杆9的一侧面,第一支杆9包括连接在一起的上下两个支杆,第一调节钮10位于第一支杆9上,用于调节上下两个支杆,实现第一支杆9的高度可调。零相位天线4位于上部支杆的顶端,激光发射器11通过侧干固定在第一支杆9的一侧面。第一支杆9与定位轴12固定连接,定位轴12固定于火炮身管6上。如图3所示,激光接收端包括十字靶板8、第二支杆14和第二调节钮13,十字靶板8固定于第二支杆14的顶端。第二调节钮13位于第二支杆14上,用于调节第二支杆14的高度,另一个零相位天线4固定在十字靶板8的顶端。外接显控器7与定位定向主机1连接;两零相位天线4与定位定向主机1有线或无线连接。的卫星2为北斗卫星,的定位定向主机1包括北斗RNSS射频模块和处理模块,北斗RNSS射频模块用于接收北斗卫星的RNSS射频信号,并将信号发送给处理模块进行处理;零相位天线4为北斗二号零电气相位中心天线。 As shown in Figure 1, the gun adjustment accuracy detection system based on satellite positioning includes a satellite 2, a gun bore axis calibration instrument 3 and its fixture 5, a positioning and orientation host 1, a zero-phase antenna 4, and an external display controller 7 . The gun bore axis calibration instrument 3 includes a laser emitting end and a laser receiving end, and the laser emitting end and the laser receiving end are respectively fixed on both ends of the gun barrel 6 by a clamp 5 . As shown in FIG. 2 , the laser emitting end includes a laser emitter 11 , a first support rod 9 and a first adjustment button 10 . The laser transmitter 11 is fixed on one side of the first pole 9. The first pole 9 includes two upper and lower poles connected together. The first adjustment button 10 is located on the first pole 9 for adjusting the upper and lower poles. The pole realizes the adjustable height of the first pole 9. The zero-phase antenna 4 is located at the top of the upper pole, and the laser transmitter 11 is fixed on one side of the first pole 9 through a side stem. The first strut 9 is fixedly connected with the positioning shaft 12, and the positioning shaft 12 is fixed on the gun barrel 6. As shown in FIG. 3 , the laser receiving end includes a cross target board 8 , a second support rod 14 and a second adjustment button 13 , and the cross target board 8 is fixed on the top end of the second support rod 14 . The second adjustment knob 13 is located on the second pole 14 for adjusting the height of the second pole 14 , and another zero-phase antenna 4 is fixed on the top of the cross target plate 8 . The external display controller 7 is connected to the positioning and orientation host 1; the two zero-phase antennas 4 are wired or wirelessly connected to the positioning and orientation host 1. The satellite 2 is a Beidou satellite, and the positioning and orientation host 1 includes a Beidou RNSS radio frequency module and a processing module. The Beidou RNSS radio frequency module is used to receive the RNSS radio frequency signal of the Beidou satellite and send the signal to the processing module for processing; Beidou-2 zero electrical phase center antenna.
调炮前,调节炮膛轴线标定仪3以使激光发射端发射的激光线与激光接收端上十字靶板8上的十字对准,实现两零相位天线4与炮膛轴线的一致性标定;两零相位天线4接收卫星2的定位信号,并将定位信号传输到定位定向主机1。调炮时,两零相位天线4同时接收多个卫星2的定位信号;调炮后,定位定向主机1对载波信号的相位信号进行处理,得到方位与高低两个方向的调炮角度,根据手动或电动目标值,计算出调炮精度,并将调炮精度结果值发送到外接显控器7进行显示。 Before adjusting the gun, adjust the gun bore axis calibration instrument 3 so that the laser line emitted by the laser emitting end is aligned with the cross on the cross target plate 8 on the laser receiving end, so as to realize the consistency calibration of the two-zero phase antenna 4 and the gun bore axis; The phase antenna 4 receives the positioning signal from the satellite 2 and transmits the positioning signal to the positioning and orientation host 1 . When adjusting the gun, two zero-phase antennas 4 receive the positioning signals of multiple satellites 2 at the same time; Or the motorized target value, calculate the gun adjustment accuracy, and send the gun adjustment accuracy result value to the external display controller 7 for display.
本发明的检测原理是:两个零相位天线4接收北斗卫星定位系统的信号,经过对载波信号相位信号的处理,得到两个零相位天线4连接线的定向角度,然后解析为火炮身管6的方位角度和高低角度,在定位定向主机1上进行显示。测试时,首先将炮膛轴线标定仪3用夹具5固定在火炮身管6的两端,调节炮膛轴线标定仪3使得激光发射光路与接收装置的十字靶板8对准,进而实现两零相位天线连线与炮膛轴线的一致性标定。然后开启定位定向主机1,检测调炮前火炮身管6的位置信息,通过火控系统或者手动调节,将火炮身管6指向理想的未来点,再检测火炮身管6的实际指向,实际指向与期望指向之间的差值即为调炮精度指标。 The detection principle of the present invention is: two zero-phase antennas 4 receive the signal of Beidou satellite positioning system, through the processing to carrier signal phase signal, obtain the directional angle of two zero-phase antenna 4 connection lines, then resolve into gun barrel 6 The azimuth angle and height angle are displayed on the positioning and orientation host 1. During the test, first fix the bore axis calibration instrument 3 on both ends of the gun barrel 6 with clamps 5, adjust the bore axis calibration instrument 3 so that the laser emission optical path is aligned with the cross target plate 8 of the receiving device, and then realize two zero-phase antennas Consistency calibration between the connection line and the axis of the bore. Then turn on the positioning and orientation main engine 1, detect the position information of the artillery barrel 6 before adjusting the gun, and point the artillery barrel 6 to the ideal future point through the fire control system or manual adjustment, and then detect the actual pointing of the artillery barrel 6, the actual pointing The difference between the expected pointing and the gun adjustment accuracy index.
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| CN105180713A (en) * | 2015-08-18 | 2015-12-23 | 中国人民解放军军械工程学院 | Artillery body tube measuring device based on Beidou radio navigation satellite system (RNSS) |
| CN105651169A (en) * | 2016-01-13 | 2016-06-08 | 袁建虎 | Precision detection method of mine laying and sweeping and obstacle breaching equipment direction finder based on total station |
| CN106094781A (en) * | 2015-12-26 | 2016-11-09 | 中国人民解放军军械工程学院 | Detection device and detection method for rocket gun electric transmission performance |
| CN110285708A (en) * | 2019-05-28 | 2019-09-27 | 中国人民解放军陆军工程大学 | Rapid detection method for north-seeking precision of self-propelled gun positioning and orienting system |
| CN110686565A (en) * | 2019-09-25 | 2020-01-14 | 西安昆仑工业(集团)有限责任公司 | Zero position and true north calibration device and calibration method for vehicle-mounted 30 mm artillery system |
| CN113701562A (en) * | 2021-08-27 | 2021-11-26 | 中国人民解放军32181部队 | Gun adjustment precision detection system and detection method thereof |
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| CN101010563A (en) * | 2004-07-13 | 2007-08-01 | 天宝导航有限公司 | Combination laser system and global navigation satellite system |
| US8104186B2 (en) * | 2007-05-07 | 2012-01-31 | Michael Raschella | Method and system for projecting an aiming X-shaped mark on a target |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN105180713A (en) * | 2015-08-18 | 2015-12-23 | 中国人民解放军军械工程学院 | Artillery body tube measuring device based on Beidou radio navigation satellite system (RNSS) |
| CN106094781A (en) * | 2015-12-26 | 2016-11-09 | 中国人民解放军军械工程学院 | Detection device and detection method for rocket gun electric transmission performance |
| CN105651169A (en) * | 2016-01-13 | 2016-06-08 | 袁建虎 | Precision detection method of mine laying and sweeping and obstacle breaching equipment direction finder based on total station |
| CN110285708A (en) * | 2019-05-28 | 2019-09-27 | 中国人民解放军陆军工程大学 | Rapid detection method for north-seeking precision of self-propelled gun positioning and orienting system |
| CN110285708B (en) * | 2019-05-28 | 2021-07-27 | 中国人民解放军陆军工程大学 | A rapid detection method for north-seeking accuracy of self-propelled artillery positioning and orientation system |
| CN110686565A (en) * | 2019-09-25 | 2020-01-14 | 西安昆仑工业(集团)有限责任公司 | Zero position and true north calibration device and calibration method for vehicle-mounted 30 mm artillery system |
| CN113701562A (en) * | 2021-08-27 | 2021-11-26 | 中国人民解放军32181部队 | Gun adjustment precision detection system and detection method thereof |
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