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Autonomous Navigation of Mars Probes by Single X-ray Pulsar Measurement and Optical Data of Viewing Martian Moons

机译:X射线脉冲星测量和火星月球光学数据对火星探测器的自主导航

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摘要

In order to achieve high accuracy of autonomous navigation for Mars probes, an integrated navigation method using X-ray pulsar measurement and optical data of viewing Martian moons is proposed. For single X-ray pulsar measurement on board a Mars probe, navigation accuracy is low due to its poor observability. On the other hand, Phobos and Deimos, two natural moons of Mars, are important optical navigation information sources available for Mars missions. However, the Martian moons ephemeris bias and the differences between barycentre and centre of brightness of Martian moons will result in low navigation accuracy. The method of integrated navigation using X-ray pulsar measurement and optical data of viewing Martian moons can overcome the defect and achieve accurate navigation. Two sequential orbit determination algorithms, Extended Kalman Filter (EKF) and Unscented Kalman Filter (UKF), are compared. The simulation results show this method can obtain high autonomous navigation accuracy during the phase of a probe orbiting Mars.
机译:为了实现火星探测器自主导航的高精度,提出了一种结合X射线脉冲星测量和火星观测光学数据的综合导航方法。对于火星探测器上的单个X射线脉冲星测量,由于其可观察性差,导航精度低。另一方面,火星的两个自然卫星火卫一和火卫二是可用于火星任务的重要光学导航信息源。但是,火星卫星的星历表偏差以及火星卫星的重心和亮度中心之间的差异将导致导航精度降低。利用X射线脉冲星测量和观测火星卫星的光学数据的组合导航方法可以克服这一缺陷,实现精确的导航。比较了两个顺序轨道确定算法,扩展卡尔曼滤波器(EKF)和无味卡尔曼滤波器(UKF)。仿真结果表明,该方法在火星轨道探测阶段具有较高的自主导航精度。

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