Robust Gyro-free Attitude Estimation for a Small Fixed-wing Unmanned Aerial Vehicle

DOI10.1002/asjc.507zbMath1303.93169OpenAlexW1737954324MaRDI QIDQ2937895

Sreenatha Gopalarao Anavatti, Abhijit G. Kallapur, Ian R. Petersen

Publication date: 13 January 2015

Published in: Asian Journal of Control (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1002/asjc.507

zbMATH Keywords

unmanned aerial vehiclesattitude estimationnorm-bound uncertaintyrobust extended Kalman filterdeterministic filteringgyroscopic failure

Mathematics Subject Classification ID

Filtering in stochastic control theory (93E11) Estimation and detection in stochastic control theory (93E10) Automated systems (robots, etc.) in control theory (93C85) Control/observation systems governed by ordinary differential equations (93C15)

Related Items (2)

Monocular Camera based Trajectory Tracking of 3-DOF Helicopter ⋮ Multiple Model Adaptive Estimator for Nonlinear System with Unknown Disturbance

Uses Software

• Aerosim

Cites Work

• Robust Kalman filtering for signals and systems with large uncertainties.
• Nonlinear attitude and gyroscope's bias estimation for a VTOL UAV
• A Discrete-Time Robust Extended Kalman Filter for Uncertain Systems With Sum Quadratic Constraints

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