A General Euler Angle Error Model of Strapdown Inertial Navigation Systems
AbstractAttitude error models play an important role in analyzing the characteristics of navigation error propagation for the design and operation of strapdown inertial navigation systems (SINS). However, the majority of existing attitude error models focus on misalignment, rather than Euler angle errors. Misalignment cannot directly describe attitude error propagation, which is an indirect measurement. To solve the problem, a general Euler angle error model of SINS is proposed. Based on Euler angle error propagation analysis, relative Euler angle errors, and convected Euler angle errors are introduced to compose the general Euler angle error model. Simulation experiments are carried out to verify the proposed model. View Full-Text
Scifeed alert for new publicationsNever miss any articles matching your research from any publisher
- Get alerts for new papers matching your research
- Find out the new papers from selected authors
- Updated daily for 49'000+ journals and 6000+ publishers
- Define your Scifeed now
Li, J.; Dang, P.; Li, Y.; Gu, B. A General Euler Angle Error Model of Strapdown Inertial Navigation Systems. Appl. Sci. 2018, 8, 74.
Li J, Dang P, Li Y, Gu B. A General Euler Angle Error Model of Strapdown Inertial Navigation Systems. Applied Sciences. 2018; 8(1):74.Chicago/Turabian Style
Li, Jianli; Dang, Pengfei; Li, Yiqi; Gu, Bin. 2018. "A General Euler Angle Error Model of Strapdown Inertial Navigation Systems." Appl. Sci. 8, no. 1: 74.
Note that from the first issue of 2016, MDPI journals use article numbers instead of page numbers. See further details here.