Now showing items 1-2 of 2

    • 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) ...
    • PID based controller design for attitude stabilization of Quad-rotor 

      Muhammad Hassan, Tanveer; Hazry, Desa, Assoc. Prof. Dr.; Syed Faiz, Ahmed, Dr.; Muhammad Kamran, Joyo; Faizan, A Warsi; Zuradzman, Mohamad Razlan, Dr.; Wan Khairunizam, Wan Ahmad, Dr.; Abadal-Salam, T. Hussain (American-Eurasian Network for Scientific Information (AENSI), 2014)
      This article presents a PID based control approach for stabilizing the attitude of quad-rotor UAV during flying. To solve the stability problem of quad-rotor UAV, some suitable and easy feedback control algorithm can be ...