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Pulsar Navigation Profile Folding and Measurement Based on Loop Tracking

机译:基于回路跟踪的脉冲星导航剖面折叠与测量

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Pulsar navigation is a possible measurement of spacecraft navigation autonomous navigation, and profile folding and measure is one of the core technologies of it, whose performance determines the capability of the final navigation result. Current profile folding measures are commonly based on the presumption that the time of photon arrival can be transformed to the solar system barycentre and the presumption that folding profile is exactitude. However, on the real navigation scene, since the position and the velocity of the spacecraft are not exactly acquir-able, folding profile would bring deformation and therefore cause the phase measure error. In order to solve this problem, this paper introduces the loop tracking to the pulsar navigation profile folding and measurement processing. By lock the difference between measure phase and predict phase, the period feedback can be realized to rise the accuracy of the pulsar phase measurement. The result shows that this method could improve the profile folding and phase measure result, and suits for dynamic pulsar navigation.
机译:脉冲星导航是航天器导航自主导航的一种可能度量,轮廓折叠和度量是其核心技术之一,其性能决定了最终导航结果的能力。当前的轮廓折叠措施通常基于以下假设:光子到达的时间可以转换为太阳系重心,并且该折叠轮廓是精确的。但是,在真实的导航场景中,由于无法精确获取航天器的位置和速度,因此折叠轮廓会带来变形,从而导致相位测量误差。为了解决这个问题,本文将循环跟踪引入脉冲星导航轮廓的折叠和测量处理中。通过锁定测量相位和预测相位之间的差异,可以实现周期反馈,从而提高脉冲星相位测量的准确性。结果表明,该方法可以改善轮廓线折叠和相位测量结果,适合动态脉冲星导航。

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