,

H Mohammadkarimi1, S Mozafari2, M H Alizadeh2

  • 1Department of Aerospace Engineering, Amirkabir University of Technology, Tehran, Iran. h.mohammadkarimi@aut.ac.ir.

Scientific reports
|July 9, 2024
PubMed
概括

本研究提出了一种新的SINS (Strapdown惯性导航系统) 调整方法,可以显著加快偏差误差计算速度. 在20秒内达到高精度,超过了需要10分钟的传统方法.

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