基于数字图像处理的半自动瞄准线法反坦克导弹控制系统的设计与实现

Muhammad Hanifudin Al Fadli, D. Gunawan, R. O. Bura, Larasmoyo Nugroho
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引用次数: 0

摘要

反坦克导弹(ATGM)系统在现代战场上具有非常重要的作用。这一体系在许多现代冲突中证明了其有效性,如叙利亚内战和纳戈尔诺-卡拉巴赫战争。ATGM系统有一个非常简单的电子和机制,但它有非常高的准确度和精度。在ATGM中使用的控制方法之一是SACLOS方法。这种方法通过探测放置在导弹尾部的红外灯来跟踪导弹位置。跟踪系统发送控制信号给导弹,作为导弹飞行时位置修正的结果。本研究的红外跟踪系统采用改进的OV5647相机,增加了940 nm窄带通滤波器。有3个相机,放大倍率为1倍,8倍和16倍,使用3个树莓派板访问。红外灯的X、y坐标数据通过无线遥测发送到机身。Atmega328微控制器处理x和y坐标数据输入成比例控制。该研究成果是一种带有红外跟踪仪的反坦克导弹控制系统原型,该红外跟踪仪能够以90.11 FPS的跟踪速度跟踪一系列88个红外led,最远可跟踪997.16米。利用YUV色彩空间亮度进行图像处理的阈值参数范围为240-255。控制参数Kp=7用于风洞试验,风速为20m /s,能够引导机体运动到望远镜的准星。
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DESIGN AND IMPLEMENTATION OF ANTI-TANK GUIDED-MISSILE (ATGM) CONTROL SYSTEM USING SEMI-AUTOMATIC COMMAND LINE OF SIGHT (SACLOS) METHOD BASED ON DIGITAL IMAGE PROCESSING
The Anti-Tank Guided-Missile (ATGM) system has a very important role in the modern battlefield. This system proved its effectiveness in many modern conflicts such as the Syrian Civil War and Nagorno-Karabakh War. The ATGM system has a very simple electronic and mechanism but it has a very high level of accuracy and precision. One of the control methods used in ATGM is SACLOS method. This method tracks missile position by detecting an infrared lamp that is placed on the missile tail. The tracking system sends control signals to the missile as a result of the correction of the missile position when flying. The infrared tracking system in this research was made using a modified OV5647 camera with the addition of a 940 nm narrow bandpass filter. There are 3 cameras with 1x, 8x, and 16x magnifications which are accessed using 3 Raspberry Pi boards. X and y coordinate data of the infrared lamp is sent to the airframe using wireless telemetry. Atmega328 microcontroller process x and y coordinate data into input proportional control. The result of this research is the prototype of an anti-tank missile control system with an infrared tracking instrument capable track a series of 88 infrared LEDs as far as 997.16 meters with a tracking speed of 90.11 FPS. The threshold parameters of image processing using luminance of YUV color space has a range of 240-255. The control parameter Kp=7 is used in wind tunnel testing with airspeed 20 m/s capable of directing airframe motion to the telescope's crosshairs.
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