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High Accuracy State and Parameter estimation of GEO-Stationary Satellites Using Jet Transport Based Nonlinear Filtering Algorithm

机译:基于喷射传输的非线性滤波算法的地理静止卫星的高精度状态和参数估计

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We consider the problem of state and parameter estimation for geostationary spacecraft in an accurate and efficient way. For this purpose we implement a Jet Transport Taylor technique in two coordinate representations, analyzing the impact of using different orders in the computations. Then, under the assumption of a Gaussian distribution, we evaluate the mean vectors and covariance matrices corresponding to estimated states and parameters. These are incorporated into a high order Kalman filter where the estimates are updated sequentially. The performances on the orbit determination and parameter estimation are discussed by a series of numerical simulations which are compared with a classical implementation of the filter.
机译:我们以准确有效的方式考虑地静止航天器的状态和参数估计问题。为此目的,我们在两个坐标表示中实施喷射运输泰勒技术,分析在计算中使用不同订单的影响。然后,在高斯分布的假设下,我们评估对应于估计状态和参数的均值向量和协方差矩阵。这些被纳入高阶卡尔曼滤波器,其中估计是顺序更新的。通过与滤波器的经典实现进行比较的一系列数值模拟讨论了轨道确定和参数估计的性能。

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