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Chapter 46 Experiment and Validation System for X-ray Pulsar-Based Navigation

机译:第46章基于X射线脉冲星的导航实验与验证系统

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Due to the huge costs, space flight experiment cannot be realized in the preliminary step of X-ray pulsar based navigation (XPNAV) research. So, a kind of XPNAV experiment and validation system is designed in this paper. This system is composed of two parts: the simulation of the pulsar signals and the calculation of navigation parameters. In the first part, the time at which X-ray photon arrive the solar system barycentre is modelled by non-homogeneous Poisson process, then the output pulse of X-ray detector while the observation of pulsars can be simulated by time transformation. In the second part, navigation information included in the pulsar signals which are simulated in the first part can be reached using the Delta-Correction method. This system can simulate four pulsar signals and the process of XPNAV at photo level. This system has the advantage of low costs and high simulation accuracy, and provides a reference for the design of prototype for space flight experiments.
机译:由于成本高昂,无法在基于X射线脉冲星的导航(XPNAV)研究的初步步骤中实现太空飞行实验。因此,本文设计了一种XPNAV实验与验证系统。该系统由两部分组成:脉冲星信号的模拟和导航参数的计算。第一部分通过非均匀泊松过程对X射线光子到达太阳系统重心的时间进行建模,然后通过时间变换模拟X射线探测器的输出脉冲,同时对脉冲星的观测进行模拟。在第二部分中,可以使用Delta-Correction方法获得在第一部分中模拟的脉冲星信号中包含的导航信息。该系统可以在光水平上模拟四个脉冲星信号和XPNAV的过程。该系统具有成本低,仿真精度高的优点,为航天实验样机的设计提供了参考。

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