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The research of satellite attitude determination algorithm based on federal filter

机译:基于联邦滤波的卫星姿态确定算法研究

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In order to obtain satellite attitude with better precision and reliability by using a multi-sensor satellite attitude determination system with uncertain model error, federated filter structure is adopted. The subfilter of federated filter is an improved Nonlinear filter, which is suitable for estimation of nonlinear system with uncertain model error by combining the Predictive filter and second-order divided Difference Filter (NPDF). The proposed method estimate model error and system state estimation by fusion multi-sensor information. The simulation results show that the federated filter with feedback, compared with no feedback, obtained better precision that is similar with that of centralized filter. 5 kinds of information-sharing methods are compared, Frobenius norm of estimated error variance matrix algorithm and variance matrix eigenvalue trace algorithm obtained relatively better estimation precision.
机译:为了通过使用具有不确定模型误差的多传感器卫星姿态确定系统获得具有更好的精度和可靠性的卫星姿态,采用联合滤波器结构。联合滤波器的子滤波器是一种改进的非线性滤波器,其适用于通过组合预测滤波器和二阶划分差滤波器(NPDF)来估计具有不确定模型误差的非线性系统。所提出的方法估算模型误差和融合多传感器信息的系统状态估计。仿真结果表明,具有反馈的联邦滤波器与无反馈相比,获得了与集中滤波器类似的更好的精度。比较了5种信息共享方法,估计误差方差矩阵算法的Frobenius规范算法和方差矩阵特征曲率算法获得了相对较好的估计精度。

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