Design and simulation of a hybrid PD-ANFIS controller for attitude tracking control of a quadrotor UAV

DOI10.1007/S13369-017-2586-ZzbMath1390.93552OpenAlexW2742293939MaRDI QIDQ1640535

Shahida Khatoon, Ibraheem Nasiruddin, Mohammed Hasan Shahid

Publication date: 14 June 2018

Published in: Arabian Journal for Science and Engineering (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s13369-017-2586-z

zbMATH Keywords

PIDhybrid controllerquadrotorUAVrotorcraftANFIS

Mathematics Subject Classification ID

Frequency-response methods in control theory (93C80) Control of mechanical systems (70Q05)

Related Items (1)

Robust trajectory tracking control for a quadrotor subject to disturbances and model uncertainties

Cites Work

• Backstepping approach for controlling a quadrotor using Lagrange form dynamics
• An integral predictive/nonlinear \(\mathcal H_{\infty}\) control structure for a quadrotor helicopter
• Attitude stabilization control of a quadrotor UAV by using backstepping approach
• Robust block second order sliding mode control for a quadrotor
• Backstepping sliding mode controller improved with fuzzy logic: Application to the quadrotor helicopter
• High‐order sliding‐mode observer for a quadrotor UAV

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