The principal minor test for semidefinite matrices
The principal minor test for semidefinite matrices
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半定矩阵的主要次要检验
DOI：
10.2514/3.20077
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发表时间：
1986
影响因子：
2.6
通讯作者：
J. Prussing
中科院分区：
文献类型：
--
作者：
J. Prussing
给出了所有状态变量的初始条件，而仅指定了最终高度和航迹角。准线性化方案是接下来通过线性化状态/eostate系统沿着与标称轨迹的横截性条件。在VAX 117750串行机上编写了计算机代码，以评估准线性化-积分矩阵算法。图1给出了在下列边界条件下助推-滑翔导弹弹道问题的数值研究结果。
The initial conditions on all the state variables are given, while only the final altitude and flight path angle are specified. The quasi-linearization scheme is next set up by linearizing the state/eostate system along with the transversality condition about nominal trajectories. A computer code was written on a VAX 117750 serial machine to evaluate the quasi-linearization-integrating matrix algorithm. Figure 1 gives the results of this numerical study for the boost-glide missile trajectory problem for the following boundary conditions.