Parameter identification method for SINS initial alignment under inertial frame

DOI10.1155/2016/5301242zbMath1400.70035OpenAlexW2510074741WikidataQ59131544 ScholiaQ59131544MaRDI QIDQ1793282

Xiaosong Guo, Haijian Xue, Zhaofa Zhou

Publication date: 12 October 2018

Published in: Mathematical Problems in Engineering (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1155/2016/5301242

Mathematics Subject Classification ID

System identification (93B30) Control of mechanical systems (70Q05)

Cites Work

• In-flight alignment of a strapdown inertial navigation system of an unmanned aerial vehicle
• Initial self-alignment for marine rotary SINS using novel adaptive Kalman filter
• A new form of the extended Kalman filter for parameter estimation in linear systems with correlated noise

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