Modern CAD technique to design Gyrocompass for UAVs and robot, ships, Aircrafts navigation systems

Q4 Computer Science
M. Zaghloul
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引用次数: 1

Abstract

This paper concerns the practical design and implementation of gyrocompass required for operation of all installed navigation equipments on robot, aircrafts, ships, also for UAVs. Most navigation systems today use some type of compass to determine heading direction. Using the Earth Os magnetic field, electronic compasses based on magneto-resistive (MR) sensors can electrically resolve better than 0.1 degree rotation and accuracy from 1 to 2 degree. Most of installed equipment on aircrafts, ships, and spaceship are form of computer-based navigation information system that complies with International regulations. These equipments can be Global position System (GPS), Radar, speed, direction, electronic chart display, height finder for aircrafts and spaceship, echo sounder for ships etc. In our design, Compass Module was utilized with Honeywell's HMC5883L 3-Axis Magnetometer, I2C, 2.7-6.5V, TTL-USB and microcontroller 16F877. For programming of the microcontroller, software PIC Basic pro was used, a window based Software. We are trying to use a cheap and good resolution within a small size Using Anisotropic Magneto resistive (AMR) technology that provides advantages over other magnetic sensor technologies. These anisotropic, directional sensors feature precision in-axis sensitivity and linearity. These sensors’ solid-state construction with very low cross-axis sensitivity is designed to measure both the direction and the magnitude of Earth’s magnetic fields, from milli-gauss to 8 gauss. The complete designed system has three outputs, the first one is USB port friendly user interface, the other two outputs are control logic state outputs. We used the designed gyro output to interface with Radar display so the targets direction can be measured in true mode instead of relative mode; as well, our designed module was employed in car protection in driver safety.
现代CAD技术设计的陀螺罗盘为无人机和机器人,船舶,飞机导航系统
本文研究了机器人、飞机、船舶以及无人机上安装的所有导航设备所需的陀螺罗盘的实际设计与实现。今天大多数导航系统使用某种类型的指南针来确定航向。利用地球磁场,基于磁阻(MR)传感器的电子罗盘可以电分辨优于0.1度的旋转,精度在1到2度之间。飞机、船舶和宇宙飞船上安装的大部分设备都是符合国际规则的计算机导航信息系统。这些设备可以是全球定位系统(GPS),雷达,速度,方向,电子海图显示,飞机和宇宙飞船的测高仪,船舶的回声测深仪等。Compass Module采用Honeywell的HMC5883L三轴磁强计,I2C, 2.7-6.5V, TTL-USB,单片机16F877。单片机的编程采用基于窗口的软件PIC Basic pro。我们正在尝试使用各向异性磁阻(AMR)技术在小尺寸内使用廉价和良好的分辨率,该技术比其他磁传感器技术具有优势。这些各向异性定向传感器具有高精度的轴内灵敏度和线性度。这些传感器的固态结构具有非常低的交叉轴灵敏度,旨在测量地球磁场的方向和大小,从毫高斯到8高斯。完整设计的系统有三个输出,一个是USB接口友好的用户界面,另外两个是控制逻辑状态输出。利用设计好的陀螺输出与雷达显示器接口,实现了以真实模式代替相对模式测量目标方向;并将所设计的模块应用于驾驶员安全的汽车保护中。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
International Journal of Computer Science and Applications
International Journal of Computer Science and Applications Computer Science-Computer Science Applications
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期刊介绍: IJCSA is an international forum for scientists and engineers involved in computer science and its applications to publish high quality and refereed papers. Papers reporting original research and innovative applications from all parts of the world are welcome. Papers for publication in the IJCSA are selected through rigorous peer review to ensure originality, timeliness, relevance, and readability.
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