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首页> 外文期刊>Acta astronautica >Mars final approach navigation using ground beacons and orbiters: An information propagation perspective
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Mars final approach navigation using ground beacons and orbiters: An information propagation perspective

机译:火星使用地面信标和轨道器的最后进近导航:信息传播的角度

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摘要

In this paper, the Mars final approach navigation is fulfilled using radiometric measurements from ground-based beacons and orbiters. In the navigation system, the beacons are fixed on the surface of the Mars and orbiters can be phased to cooperate with the probe. The trajectory of the Mars probe and the true anomalies of the orbiters are the design variables that should be optimized. The propagation process of the Fisher information in dynamical system is clarified, and the Fisher information matrix (FIM) at the final time contains the whole information accumulated. from the measurements. The system's observability is optimized through maximizing the eigenvalues of the information matrix. Furthermore, the optimal geometrical configurations with three and four measurements are analytically solved for the first time. In simulations, an unscented Kalman filter (UKF) is applied to examine the navigation performance in different scenarios in which three and four measurements are applied. The results show that the position and velocity estimation accuracy can reach 10 m and 0.01 m/s respectively. The Fisher information increases the most when the geometrical configuration is in the vicinity of the optimal configuration.
机译:在本文中,使用来自地面信标和轨道器的辐射测量数据来完成火星最终进近导航。在导航系统中,信标固定在火星表面,并且轨道器可以定相以与探测器配合。火星探测器的轨迹和轨道器的真实异常是应该优化的设计变量。阐明了费舍尔信息在动力系统中的传播过程,最后的费舍尔信息矩阵(FIM)包含了累积的全部信息。从测量。通过最大化信息矩阵的特征值来优化系统的可观察性。此外,首次解析了具有三个和四个测量值的最佳几何构型。在模拟中,应用无味卡尔曼滤波器(UKF)来检查在应用了三个和四个测量值的不同情况下的导航性能。结果表明,位置和速度估计精度分别达到10 m和0.01 m / s。当几何构型在最佳构型附近时,Fisher信息增加最多。

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