Please use this identifier to cite or link to this item: http://dspace.unimap.edu.my:80/xmlui/handle/123456789/7319
Title: Development of Attitude Control System on RCM3400 microcontroller for Nano-satellite applications
Authors: Muhyi, Yaakop
Sazali, Yaacob
Abdul Rahman, Mohd Saad
Harihran, M.
Nagarajan, R.
Keywords: Artificial satellites -- Attitude control systems
Artificial satellites
RCM3400 microcontroller
Attitude control system (ACS)
Kalman filtering
Issue Date: 11-Oct-2009
Publisher: Universiti Malaysia Perlis
Citation: p.3A7 1 - 3A7 5
Series/Report no.: Proceedings of the International Conference on Man-Machine Systems (ICoMMS 2009)
Abstract: This paper describes the development of a nano-satellite attitude control system (ACS) which employ a Kalman filter based controller and a simple adaptive predictive fuzzy logic controller (APFLC) for a 1, 2 and 3 axis orientation using RCM3400 microcontroller. This paper presents the performance comparison of the APFLC and Kalman filter based controller implemented in the hardware. The physical interface module, configuration with several key features, communication protocol and data handling for the micro-controller are also described.
Description: Organized by School of Mechatronic Engineering (UniMAP) & co-organized by The Institution of Engineering Malaysia (IEM), 11th - 13th October 2009 at Batu Feringhi, Penang, Malaysia.
URI: http://dspace.unimap.edu.my/123456789/7319
Appears in Collections:Conference Papers
Sazali Yaacob, Prof. Dr.
Ramachandran, Nagarajan, Prof. Dr.

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