NMPC-PID based control structure design for avoiding uncertainties in attitude and altitude tracking control of quad-rotor (UAV)
Proceeding of the IEEE 10th International Colloquium on Signal Processing & its Applications (CSPA) 2014 at Kuala Lumpur, Malaysia on 7 Mac 2014 until 9 Mac 2014. Link to publisher's homepage at http://ezproxy.unimap.edu.my:2080/Xplore/dynhome.jsp?tag=1
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2014
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my.unimap-354152017-11-29T05:05:47Z 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. hassantanveer@live.com hazry@unimap.edu.my syedfaiz@unimap.edu.my sky_kamran12@hotmail.com f_warsi128@hotmail.com kamarudin@unimap.edu.my zuradzman@unimap.edu.my khairunizam@unimap.edu.my shahriman@unimap.edu.my Quad-rotor Attitude and altitude control Auto-tune PID Model predictive control (MPC) Proceeding of the IEEE 10th International Colloquium on Signal Processing & its Applications (CSPA) 2014 at Kuala Lumpur, Malaysia on 7 Mac 2014 until 9 Mac 2014. Link to publisher's homepage at http://ezproxy.unimap.edu.my:2080/Xplore/dynhome.jsp?tag=1 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) controller for better stabilizing of quad-rotor VAV under different noises and disturbance conditions. The idea is to satisfy the environmental and safety considerations and for that the study of noises and disturbance condition in VAV flight upon the performances of NMPC and PID respectively is being evaluated. Finally a new control method is developed by combing two techniques which can be able to handle different sort of uncertainties i.e. noises and external disturbances in quad-rotor type VAV systems. The simulation result proves that the proposed control structure technique works very well in altitude and attitude stabilization of quad-rotor under different perturbed and unperturbed conditions. 2014-06-12T06:52:33Z 2014-06-12T06:52:33Z 2014-03 Working Paper p. 117-122 978-1-4799-3090-6 http://ieeexplore.ieee.org/xpl/articleDetails.jsp?tp=&arnumber=6805732 http://dspace.unimap.edu.my:80/dspace/handle/123456789/35415 http://dx.doi.org/10.1109/CSPA.2014.6805732 en Proceeding of the IEEE 10th International Colloquium on Signal Processing & its Applications (CSPA), 2014; IEEE Conference Publications |
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| topic |
Quad-rotor Attitude and altitude control Auto-tune PID Model predictive control (MPC) |
| spellingShingle |
Quad-rotor Attitude and altitude control Auto-tune PID Model predictive control (MPC) 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. NMPC-PID based control structure design for avoiding uncertainties in attitude and altitude tracking control of quad-rotor (UAV) |
| description |
Proceeding of the IEEE 10th International Colloquium on Signal Processing & its Applications (CSPA) 2014 at Kuala Lumpur, Malaysia on 7 Mac 2014 until 9 Mac 2014. Link to publisher's homepage at http://ezproxy.unimap.edu.my:2080/Xplore/dynhome.jsp?tag=1 |
| author2 |
hassantanveer@live.com |
| author_facet |
hassantanveer@live.com 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. |
| format |
Working Paper |
| author |
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. |
| author_sort |
M. Hassan, Tanveer |
| title |
NMPC-PID based control structure design for avoiding uncertainties in attitude and altitude tracking control of quad-rotor (UAV) |
| title_short |
NMPC-PID based control structure design for avoiding uncertainties in attitude and altitude tracking control of quad-rotor (UAV) |
| title_full |
NMPC-PID based control structure design for avoiding uncertainties in attitude and altitude tracking control of quad-rotor (UAV) |
| title_fullStr |
NMPC-PID based control structure design for avoiding uncertainties in attitude and altitude tracking control of quad-rotor (UAV) |
| title_full_unstemmed |
NMPC-PID based control structure design for avoiding uncertainties in attitude and altitude tracking control of quad-rotor (UAV) |
| title_sort |
nmpc-pid based control structure design for avoiding uncertainties in attitude and altitude tracking control of quad-rotor (uav) |
| publisher |
IEEE Conference Publications |
| publishDate |
2014 |
| url |
http://dspace.unimap.edu.my:80/dspace/handle/123456789/35415 |
| _version_ |
1643802760862236672 |
| score |
13.214268 |