In this paper, the adjoint system theory is applied to the guidance accuracy assessment of the flying vehicle, and the covariance matrix of the impact point deviation is solved.
本文根据伴随系统理论，在某飞行器制导工具误差的精度评定中加以实际应用，求出落点偏差的协方差矩阵。
A new method based on the theory of adjoint systems to compute the controlling unstable equilibrium point is presented.
提出了一种基于伴随系统理论的电力系统主导不稳定平衡点的求解方法。
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