Numerical solution and dispersion analysis for airborne rocket trajectory are studied.
本文研究航空火箭(简称航箭)弹道的数值解法和散布分析。
Several works have been done in automatic QT dispersion analysis, but most of them were vulnerable, susceptive to noises and baseline wandering.
已有的几种QT间期的自动测量方法都在时域进行，易受噪声和基线漂移影响。
To reach this goal, convergence analysis, extrapolation, von Neumann stability analysis, and dispersion analysis are introduced and used frequently throughout the book.
为了达到这个目标，会集分析，外推力，冯·诺伊曼稳定性分析和散布分析被介绍并且经常在整个书使用。
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