Research on the Necessity of Lie Group Strapdown Inertial Integrated Navigation Error Model Based on...
Research on the Necessity of Lie Group Strapdown Inertial Integrated Navigation Error Model Based on Euler Angle
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Basel: MDPI AG
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English
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Basel: MDPI AG
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In response to the lack of specific demonstration and analysis of the research on the necessity of the Lie group strapdown inertial integrated navigation error model based on the Euler angle, two common integrated navigation systems, strapdown inertial navigation system/global navigation satellite system (SINS/GNSS) and strapdown inertial navigatio...
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Research on the Necessity of Lie Group Strapdown Inertial Integrated Navigation Error Model Based on Euler Angle
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TN_cdi_doaj_primary_oai_doaj_org_article_d2f16e96e50443a28c6b9210282ed757
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https://devfeature-collection.sl.nsw.gov.au/record/TN_cdi_doaj_primary_oai_doaj_org_article_d2f16e96e50443a28c6b9210282ed757
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ISSN
1424-8220
E-ISSN
1424-8220
DOI
10.3390/s22207742