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HPC GPS BASED AUTONOMOUSNAVIGATION SYSTEM FOR FUTUREGENERATIONS OF SATELLITES

机译:基于HPC和GPS的自主 r n卫星导航系统 r n卫星的生成

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This paper elaborates on the development of a space bornrnautonomous navigation system utilising the advancedrnGlobal Positioning System (GPS) and High PerformancernComputing (HPC) technology for future generations ofrnsatellite systems.rnGPS is a device integrated into the satellite system tornsense spacecraft trajectory and attitude, measure thernrelative distance between space vehicles, deliver preciserntime synchronisation to spacecraft electronics, and soundrnthe atmosphere. However, the advances in GPSrntechnology are not sychronised with the current capabilityrnof a standard spacecraft system to handle all thernmeasurements and provide on-board processing capacityrnto use these measurements for autonomous navigation.rnCurrent spacecraft systems provide very limited on-boardrncomputing capability, and therefore these satellites rely onrnother devices to provide information about the spacecraftrnposition such as star cameras and some times requirernground processing of data to give instructions onrnappropriate positions of the satellite.rnHPC systems consist of reconfigurable logic circuitsrnadded to a conventional processor to generate a powerfulrnsystem for handling intensive computing tasks.Reconfigurable Computing Technology (RCT) usingrnField Programmable Gate Arrays (FPGAs) represents arnflexible computing platform where both the hardware andrnthe software can be programmed on an application byrnapplication basis. This emerging technology is veryrnpromising for a lot of applications, especially satelliternsystems.rnThis paper investigates the deployment of HPC in therncontext of real-time reactive computer system on-boardrnthe spacecraft in conjunction with the GPS to implementrnthe autonomous navigation system. In particular, thernpaper introduces the use of a reconfigurable computer forrnposition and velocity computations of the spacecraftrnefficiently, with a focus on cost-effective implementationrnof precise orbit determination and control algorithms onrnFPGAs. Experimental testbeds for this research are alsornpresented.
机译:本文阐述了利用先进的全球定位系统(GPS)和高性能rnComputing(HPC)技术为下一代卫星系统开发的天生自主导航系统的方法。航天器之间的距离,为航天器电子设备提供精确的时间同步,并为大气层提供声音。但是,GPS技术的进步并没有与标准航天器系统的当前能力保持同步,以处理所有的测量并提供机载处理能力以将这些测量值用于自主导航。当前的航天器系统提供了非常有限的机载计算能力,因此这些卫星HPC系统依赖于其他设备来提供有关航天器位置的信息,例如星空摄像机,有时还需要对数据进行地面处理,以在卫星的适当位置上给出指令.rn HPC系统由可重新配置的逻辑电路组成,该逻辑电路被添加到常规处理器中以生成用于处理密集计算任务的强大系统。使用现场可编程门阵列(FPGA)的可重构计算技术(RCT)代表了一种灵活的计算平台,在该平台上,可以根据应用程序对硬件和软件进行编程。这项新兴技术对于许多应用特别是卫星系统来说是非常有前途的。本文研究了航天器上实时反应计算机系统结合GPS在HPC中的部署,以实现自主导航系统。特别是,本文介绍了可重配置计算机对航天器的定位和速度计算的使用效率,重点是FPGA上精确轨道确定和控制算法的经济有效实施。还提供了用于该研究的实验性试验台。

著录项

  • 来源
  • 会议地点 Long Beach CA(US);Long Beach CA(US);Long Beach CA(US)
  • 作者单位

    Cooperative Research Centre for Satellite SystemsrnSchool of Electrical and Electronic Systems EngineeringrnQueensland University of TechnologyrnGPO Box 2434, Brisbane, QLD 4001, AUSTRALIA;

    Cooperative Research Centre for Satellite SystemsrnSchool of Electrical and Electronic Systems EngineeringrnQueensland University of TechnologyrnGPO Box 2434, Brisbane, QLD 4001, AUSTRALIA;

    Cooperative Research Centre for Satellite SystemsrnSchool of Electrical and Electronic Systems EngineeringrnQueensland University of TechnologyrnGPO Box 2434, Brisbane, QLD 4001, AUSTRALIA;

  • 会议组织
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 无线电导航 ;
  • 关键词

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