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In-flight alignment of a strapdown inertial navigation system of an unmanned aerial vehicle

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Publication:394073
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DOI10.1134/S1064230712060147zbMath1279.93081OpenAlexW2089727549MaRDI QIDQ394073

K. K. Veremeenko, V. M. Savel'ev

Publication date: 24 January 2014

Published in: Journal of Computer and Systems Sciences International (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1134/s1064230712060147


zbMATH Keywords

carrier aircraftinitial alignment systemstrapdown inertial navigation systemunmanned aerial vehicle


Mathematics Subject Classification ID

Application models in control theory (93C95) Variable mass, rockets (70P05)


Related Items (4)

Nonlinear stochastic evaluation of the orientation parameters of a strapdown inertial navigation system of a space vehicle during prelaunch preparation ⋮ Aerodrome vehicle integrated control system using computer vision ⋮ In-flight self-alignment method aided by geomagnetism for moving basement of guided munitions ⋮ Parameter identification method for SINS initial alignment under inertial frame







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