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

DOI10.1134/S1064230718030048zbMath1398.93345OpenAlexW2809116347WikidataQ129622360 ScholiaQ129622360MaRDI QIDQ1792406

A. V. Kanyshev, V. N. Ovcharenko, O. N. Korsun, A. V. Stulovskii

Publication date: 11 October 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/s1064230718030048

zbMATH Keywords

error estimatesaerodynamic coefficientslongitudinal movementsupercritical angles of attack

Mathematics Subject Classification ID

Application models in control theory (93C95) Estimation and detection in stochastic control theory (93E10) General aerodynamics and subsonic flows (76G25) Identification in stochastic control theory (93E12)

Related Items (2)

Identification of nonstationary aerodynamic characteristics of an aircraft based on flight data ⋮ Direct method for forming the optimal open loop control of aerial vehicles

Cites Work

• Unnamed Item
• Mathematical description of nonstationary aerodynamic characteristics of a passenger aircraft model in longitudinal motion at large angles of attack
• Algorithms of increasing the calculation accuracy for an aircraft's orientation angle
• Knowledge-based ant colony optimization method to design fuzzy proportional integral derivative controllers
• Unsteady aerodynamics modeling for flight dynamics application

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