A robust control design approach for altitude control and trajectory tracking of a quadrotor

• Datum: 2021
• Hauptverfasser: Gulshan, Z. A., Ali, M. Z. H., Shah, M. S., Nouman, D., Anwar, M., Ullah, M. F.
• Format: Artikel
• Sprache: English
• Veröffentlicht: National Technical University "Kharkiv Polytechnic Institute" and Аnatolii Pidhornyi Institute of Power Machines and Systems of NAS of Ukraine 2021
• Schlagworte: six degree of freedom quadrotor; unmanned aerial vehicle; attitude regulation; nonlinear system; robust control; H∞ controller
• Online Zugang: http://eie.khpi.edu.ua/article/view/242489
• Назва журналу: Electrical Engineering & Electromechanics

Introduction. Unmanned aerial vehicles as quadcopters, twin rotors, fixed-wing crafts, and helicopters are being used in many applications these days. Control approaches applied on the quadrotor after decoupling the model or separate altitude control and trajectory tracking have been reported in the...