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制导系统工具误差的自适应估计
引用本文:张金槐. 制导系统工具误差的自适应估计[J]. 航天控制, 1991, 0(Z1)
作者姓名:张金槐
作者单位:国防科技大学
摘    要:本文研完惯性制导系统工具误差的自适应估计问题。运用自适应技术,这是解决制导精度鉴定问题的一个新的尝试,文中对仪表的误差模型给出了动态补偿,并给出了误差系数的递推估计。对模型中随机量的统计特性应用了自适应技术,并对岭回归引入了自适应估计,对滤波过程中模型的辨识及估值中偏倚的补偿,进行了讨论。

关 键 词:线性模型参数估计  岭估计  自适应估计  模型辨识

ADAPTIVE ESTIMATION OF THE INSTRUMENTAL ERROR TO THE GUIDANCE SYSTEM
Zhang Jin-Huai National University of Defense Technology. ADAPTIVE ESTIMATION OF THE INSTRUMENTAL ERROR TO THE GUIDANCE SYSTEM[J]. Aerospace Control, 1991, 0(Z1)
Authors:Zhang Jin-Huai National University of Defense Technology
Affiliation:Zhang Jin-Huai National University of Defense Technology
Abstract:This paper studies the problems of adaptive estimation of the instrumental error to the guidance system. In the first, we establish the dynamic compensation model of the instrumental error and give recursive estimators of the error coefficients. When the statistical characteristics of the random error are unknown, we suggest to apply the adaptive estimation method and using this method to construct ridge estimation of the parameters. In the same time, the identification of the model and the compensation for the biased estimator are discussed.
Keywords:Parameter estimation Linear model Ridge estimation Adaptive estimation Model identification.
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