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    • NMPC-PID based control structure design for avoiding uncertainties in attitude and altitude tracking control of quad-rotor (UAV) 

      M. Hassan, Tanveer; Hazry, Desa, Assoc. Prof. Dr.; Syed Faiz, Ahmed; M. Kamran, Joyo; Faizan. A., Warsi; Kamarudin, Hussin, Brig. Jen. Dato' Prof. Dr.; Zuradzman, Mohamad Razlan, Dr.; Wan Khairunizam, Wan Ahmad, Dr.; Shahriman, Abu Bakar, Dr. (IEEE Conference Publications, 2014-03)
      The extensive consideration in this research article is to utilize the advantages of two most popular control techniques which are Non-Linear Model Predictive Control (NMPC) and Proportional Integral and Derivative (PID) ...