在卫星的状态估计过程中应用推广的序列估计算法，借助数值积分方法积分状态向量和协方差矩阵。

For the estimation of satellite state, the extended sequential estimation algorithm was applied. The numerical method was used to integrate state vector and error covariance matrix.

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针对结构隐式极限状态函数的可靠性分析，提出了一种支持向量机分类迭代算法。

For reliability analysis of structure with implicit limit state function, an iterative algorithm was presented on the basis of support vector classification machine.

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采用一种稍加修改的强跟踪滤波算法估计降阶状态向量，然后利用降阶状态向量估计非线性状态函数。

A slightly modified strong tracking filtering algorithm is used to estimate the reduced-order state vector, which is then used to estimate the nonlinear state function.

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