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Nonlinear attitude and gyroscope's bias estimation for a VTOL UAV

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Publication:3442669
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DOI10.1080/00207720601110798zbMath1117.93049OpenAlexW2146922149MaRDI QIDQ3442669

Philippe Souères, Jean-Michel Pflimlin, Tarek Hamel

Publication date: 18 May 2007

Published in: International Journal of Systems Science (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1080/00207720601110798


zbMATH Keywords

observersunmanned air vehiclesspecial orthogonal group \((SO(3))\)


Mathematics Subject Classification ID

Application models in control theory (93C95) Observability (93B07) Algebraic methods (93B25)


Related Items (4)

Attitude observers for accelerated vehicles without accelerometer measurements ⋮ Robust Gyro-free Attitude Estimation for a Small Fixed-wing Unmanned Aerial Vehicle ⋮ Nonlinear speed estimation of a GPS-free UAV ⋮ Robust attitude tracking control of small-scale unmanned helicopter




Cites Work

  • A globally convergent angular velocity observer for rigid body motion




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