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本文叙述最大似然法识别导弹稳定性和操纵性导数原理,推导了最大似然函数,应用Gauss方法进行非线性迭代,求出了导弹的稳定性和操纵性导数。
This paper describes the maximum likelihood method to identify the missile stability and maneuvering derivative principle, derives the maximum likelihood function, and applies the Gauss method for nonlinear iteration to obtain the missile stability and maneuvering derivative.