A quaternion-based method for SINS/SAR integrated navigation system

IEEE Transactions on Aerospace and Electronic Systems

Volumn 48, Issue 1, 2012, Pages 514-524

  Zhong, Yongmin ^a   Gao, Shesheng ^b   Li, Wei ^b  

^a RMIT UNIVERSITY   (Australia)

^b NORTHWESTERN POLYTECHNICAL UNIVERSITY   (China)

Author keywords

[No Author keywords available]

Indexed keywords

ERROR MODEL; INTEGRATED NAVIGATION SYSTEMS; MATRIX; NAVIGATION ERROR; NON-LINEAR ERROR; NON-LINEAR MODEL; OBSERVATION MODEL; OPTIMAL DATA; PARTICLE FILTERING; POSITIONING PRECISION; SINS/SAR INTEGRATED; STRAP-DOWN INERTIAL NAVIGATION SYSTEMS;

DATA FUSION; INERTIAL NAVIGATION SYSTEMS;

NAVIGATION;

EID: 84862954768     PISSN: 00189251     EISSN: None     Source Type: Journal    
DOI: 10.1109/TAES.2012.6129652     Document Type: Article

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