Application of the taguchi quality method to design navigation constants that are robust to target maneuvers

Chien Chun Kung, Feng Lung Chiang, Ciann Dong Yang

研究成果: Article同行評審

摘要

The object of this paper is to present a quality control approach to design the navigation constants for missile guidance law that are robust for target's maneuverability and missile's performance. Target's maneuvers and missile's time constants are considered to be noise factors and Taguchi Quality Method (TQM) is used to conduct matrix experiments and determine the robust navigation constants. From the simulation results for three kinds of guidance laws, we find that robust navigation constants have a greater ability to enhance the interception of targets that are performing uncertain maneuvers with less interception time and smaller miss distances in the hitting phase.

原文English
頁(從 - 到)231-246
頁數16
期刊Transactions of the Canadian Society for Mechanical Engineering
37
發行號2
DOIs
出版狀態Published - 2013

All Science Journal Classification (ASJC) codes

  • 機械工業

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