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- W2016128293 abstract "This paper presents a robust adaptive ℋ <sub xmlns:mml=http://www.w3.org/1998/Math/MathML xmlns:xlink=http://www.w3.org/1999/xlink>∞</sub> strategy to solve the attitude of the quad-rotor helicopter control problems with actuator failures and external disturbances. The dynamic motion equations are obtained by the Euler formalism. Based on the linear time-invariant state-space equations of the quad-rotor, a state feedback robust adaptive ℋ <sub xmlns:mml=http://www.w3.org/1998/Math/MathML xmlns:xlink=http://www.w3.org/1999/xlink>∞</sub> tracking controller is proposed to track the given attitude angles with actuator faults. The controller gain consists of two parts: one part is the fixed gain which is obtained based on LMIs (linear Matrix inequalities), the other one is the time-varying gain which is adjusted on-line by the designed adaptive laws. Simulations based on a 3D Hover System of Quanser, are presented to verify the control strategy in the SIMULINK/MATLAB environment." @default.
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- W2016128293 date "2014-07-01" @default.
- W2016128293 modified "2023-10-16" @default.
- W2016128293 title "Fault tolerant tracking control for quad-rotor helicopter via robust adaptive technique" @default.
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- W2016128293 doi "https://doi.org/10.1109/chicc.2014.6895471" @default.
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