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

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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Bibliographic Details
Main Authors: 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.
Other Authors: hassantanveer@live.com
Format: Working Paper
Language:English
Published: IEEE Conference Publications 2014
Subjects:
Quad-rotor
Attitude and altitude control
Auto-tune PID
Model predictive control (MPC)
Online Access:http://dspace.unimap.edu.my:80/dspace/handle/123456789/35415
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Institution: Universiti Malaysia Perlis
Language: English

Internet

http://dspace.unimap.edu.my:80/dspace/handle/123456789/35415

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