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Kinematics, design, programming and control of a robotic platform for satellite tracking and other applications.

机译:用于卫星跟踪和其他应用的机器人平台的运动学,设计,编程和控制。

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摘要

In order to avoid the keyhole problems associated with present antenna mounting systems and to meet the requirements of acquisition and tracking for high gain and narrow beamwidth antennas, a novel antenna mount system is developed. The antenna is mounted on a microprocessor controlled robotic platform with six degrees of freedom. The mechanism is based on the principles of Stewart platform, which employes six variable length actuators constrained between a fixed base and a movable platform. This antenna mount is especially suitable for high gain antennas using high frequency band widths for marine satellite communications. The kinematics and geometry of the parallel link mechanism has been studied in detail. The kinematic analysis for the parallel manipulator consists of developing a set of kinematic equations for the six linear actuators in terms of the "world coordinates" (Ф,θ,α,x,y,z). These kinematic equations are then solved for the "machine coordinates'" (L1 ,L2,L3,L4,L5,L6), which are the six actuator lengths. A computer simulation has been done to model the motion of the platform. The simulation has simplified the task of examining various mechanism configurations, the range of motion and the mechanism mechanical constraints. A six motor controller board based on the motion controller microprocessors has been developed. Limited unipolar pulse width modulated servo drives are used to drive the permanent magnet DC motors of the linear actuators. A desktop computer is used as the host processor to generate the command data. The motion control microprocessors generate the velocity and acceleration profiles and drive the six axes simultaneously. The main control programme residing in the host processor schedules the overall operation. The orbital satellite bearings are calculated on a minicomputer and downloaded to the control desktop computer. A prototype antenna mount based on the descriptions above was designed, constructed and tested for tracking a high pass and low pass of an orbiting weather satellite, (the NOAA-7). A microwave antenna mounted on the platform was found to be capable of tracking an orbital satellite throughout the visible hemisphere, although the reception tracking has not been inplemented. This antenna mount offers a light weight, structurally strong and fast dynamic response tracking system for land and marine applications. This parallel robotic mechanism has potential for further applications such as a prepackaged portable communications system which can be deployed rapidly at remote construction sites or during civil defence emergencies. In addition it may be employed as a stabilized platform which can be used for marine VTOL aircraft recovery during rough weather. The application of this antenna mount in a low cost marine satellite communications system is emphasized since the fast dynamic response of the system will eliminate the need for an expensive stabilized platform.
机译:为了避免与当前天线安装系统相关的钥匙孔问题并满足对高增益和窄波束宽度天线的获取和跟踪的要求,开发了一种新颖的天线安装系统。天线安装在具有六个自由度的微处理器控制的机器人平台上。该机构基于Stewart平台的原理,该平台采用了六个固定在固定基座和可移动平台之间的可变长度致动器。这种天线安装座特别适用于使用高带宽的高增益天线进行船用卫星通信。对平行连杆机构的运动学和几何形状进行了详细研究。并联机械手的运动学分析包括根据“世界坐标”(Ф,θ,α,x,y,z)为六个线性执行器开发一组运动学方程。然后针对六个执行器长度的“机器坐标”(L1,L2,L3,L4,L5,L6)求解这些运动学方程。已经完成了计算机仿真,以对平台的运动进行建模。该模拟简化了检查各种机构配置,运动范围和机构机械约束的任务。已经开发了基于运动控制器微处理器的六个电机控制器板。有限的单极脉宽调制伺服驱动器用于驱动线性执行器的永磁直流电动机。台式计算机用作主机处理器以生成命令数据。运动控制微处理器生成速度和加速度曲线,并同时驱动六个轴。驻留在主机处理器中的主控制程序会调度整个操作。在小型计算机上计算轨道卫星方位,然后将其下载到控制台式计算机。设计,制造和测试了基于上述描述的原型天线支架,用于跟踪轨道气象卫星(NOAA-7)的高通和低通。发现还没有安装在平台上的微波天线能够跟踪整个可见半球的轨道卫星。这种天线安装座为陆地和海洋应用提供了重量轻,结构坚固和快速的动态响应跟踪系统。这种并行机器人机制具有进一步应用的潜力,例如预包装的便携式通信系统,可以在远程施工现场或民防紧急情况下快速部署。另外,它可用作稳定平台,可用于恶劣天气期间海上VTOL飞机的恢复。由于该系统的快速动态响应将消除对昂贵的稳定平台的需求,因此强调了该天线支架在低成本海洋卫星通信系统中的应用。

著录项

  • 作者

    Afzulpurkar N. V.;

  • 作者单位
  • 年度 1990
  • 总页数
  • 原文格式 PDF
  • 正文语种 en
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