Maximal admissible mode decision delay in terminal guidance

Shengwen XIANG, Tiancheng LI, Wei CHEN, Hongqi FAN, Qiang FU

科研成果: 期刊稿件文章同行评审

1 引用 (Scopus)

摘要

Mode decision-maker is a critical component in the logic-based Integrated Estimation and Guidance (IEG) system. For the best possible estimation and guidance performance, the mode decision delay of the mode decision-maker should be limited to a range as small as possible. This paper presents a numerical method for computing the maximal admissible mode decision delay that varies with time-to-go. Particular attention has been paid to highly maneuvering target interception in terminal guidance. The results of this research offer useful guidelines for the design of the mode decision-maker in IEG systems.

源语言英语
页(从-至)1959-1966
页数8
期刊Chinese Journal of Aeronautics
32
8
DOI
出版状态已出版 - 8月 2019
已对外发布

指纹

探究 'Maximal admissible mode decision delay in terminal guidance' 的科研主题。它们共同构成独一无二的指纹。

引用此