Algorithms of increasing the calculation accuracy for an aircraft's orientation angle

DOI10.1134/S1064230715050032zbMath1383.93074OpenAlexW2327955453MaRDI QIDQ1742442

V. S. Kulabukhov, V. V. Bulgakov, A. V. Stulovskii, O. N. Korsun, D. S. Timofeyev

Publication date: 11 April 2018

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

Full work available at URL: https://doi.org/10.1134/s1064230715050032

zbMATH Keywords

numerical integrationaircraft's orientation anglesPoisson's and quaternion equationsrandom errors of matrix elements

Mathematics Subject Classification ID

Application models in control theory (93C95) Stochastic systems in control theory (general) (93E03) Control/observation systems governed by ordinary differential equations (93C15)

Related Items (1)

Identification of aerodynamic coefficients of longitudinal movement and error estimates for onboard measurements of supercritical angles of attack

Cites Work

• Estimation of systematic errors of onboard measurement of angle of attack and sliding angle based on integration of data of satellite navigation system and identification of wind velocity
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