Robust adaptive fault‐tolerant proportional‐derivative tracking control for six‐degrees of freedom unmanned aerial vehicles
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Publication:6180504
DOI10.1002/RNC.5778zbMath1529.93054MaRDI QIDQ6180504
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Publication date: 19 December 2023
Published in: International Journal of Robust and Nonlinear Control (Search for Journal in Brave)
Sensitivity (robustness) (93B35) Feedback control (93B52) Adaptive control/observation systems (93C40) Automated systems (robots, etc.) in control theory (93C85)
Cites Work
- Adaptive actuator failure compensation control of uncertain nonlinear systems with guaranteed transient performance
- Fault-tolerant finite time consensus for multiple uncertain nonlinear mechanical systems under single-way directed communication interactions and actuation failures
- An integral predictive/nonlinear \(\mathcal H_{\infty}\) control structure for a quadrotor helicopter
- Adaptive control with guaranteed transient and steady state tracking error bounds for strict feedback systems
- Time-varying feedback for regulation of normal-form nonlinear systems in \textit{prescribed} finite time
- Robust control for a quadrotor aircraft with small overshoot and high-precision position tracking performance
- Adaptive actuator failure compensation for nonlinear MIMO systems with an aircraft control application
- Robust adaptive fault estimation and fault tolerant control for quadrotor attitude systems
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