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HPC GPS BASED AUTONOMOUS NAVIGATION SYSTEM FOR FUTURE GENERATIONS OF SATELLITES

机译:基于HPC和GPS的自主导航系统,用于后代卫星

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This paper elaborates on the development of a space born autonomous navigation system utilising the advanced Global Positioning System (GPS) and High Performance Computing (HPC) technology for future generations of satellite systems. GPS is a device integrated into the satellite system to sense spacecraft trajectory and attitude, measure the relative distance between space vehicles, deliver precise time synchronisation to spacecraft electronics, and sound the atmosphere. However, the advances in GPS technology are not sychronised with the current capability of a standard spacecraft system to handle all the measurements and provide on-board processing capacity to use these measurements for autonomous navigation. Current spacecraft systems provide very limited on-board computing capability, and therefore these satellites rely on other devices to provide information about the spacecraft position such as star cameras and some times require ground processing of data to give instructions on appropriate positions of the satellite. HPC systems consist of reconfigurable logic circuits added to a conventional processor to generate a powerful system for handling intensive computing tasks. Reconfigurable Computing Technology (RCT) using Field Programmable Gate Arrays (FPGAs) represents a flexible computing platform where both the hardware and the software can be programmed on an application by application basis. This emerging technology is very promising for a lot of applications, especially satellite systems. This paper investigates the deployment of HPC in the context of real-time reactive computer system on-board the spacecraft in conjunction with the GPS to implement the autonomous navigation system. In particular, the paper introduces the use of a reconfigurable computer for position and velocity computations of the spacecraft efficiently, with a focus on cost-effective implementation of precise orbit determination and control algorithms on FPGAs. Experimental testbeds for this research are also presented.
机译:在利用先进的全球定位系统(GPS)和高性能计算(HPC)技术,卫星系统的后代出生的空间自主导航系统的发展本文阐述。 GPS是集成到卫星系统,以读出航天器轨道和姿态的装置,测量空间飞行器之间的相对距离,对航天器电子产品上提供精确的时间同步,并且声音大气。然而,在GPS技术的进步不是一个标准的航天器系统来处理所有的测量,并提供板载使用这些测量结果用于自主导航处理能力的电流能力sychronised。当前航天器系统提供的车载计算能力非常有限,因此,这些卫星依靠其它设备提供有关航天器的位置,例如星相机和一些时间要求数据的地面处理,得到对卫星的适当的位置的指示信息。 HPC系统由加入到常规的处理器,以产生用于处理密集的计算任务的强大系统可重新配置逻辑电路。可重构计算技术使用现场可编程门阵列(FPGA)(RCT)表示的柔性的计算平台,其中的硬件和软件可以在由应用程序的基础的应用程序进行编程。这种新兴的技术是非常有前途的很多应用,特别是卫星系统。本文研究了HPC的实时反应的计算机系统的机载与GPS相结合的航天器实现自主导航系统的情况下部署。特别地,文中介绍了使用用于有效地航天器的位置和速度计算的可重新配置的计算机的,重点放在对FPGA的精确轨道确定和控制算法成本效益的实施。本研究的实验测试平台,还提出。

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