Publication:
Development of attitude control system on RCM3400 microcontroller for Nano-satellite applications
Development of attitude control system on RCM3400 microcontroller for Nano-satellite applications
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Date
2009-10-11
Authors
Muhyi Yaakop
Sazali Yaacob
Abdul Rahman Mohd Saad
M Harihran
R. Nagarajan
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Universiti Malaysia Perlis (UniMAP)
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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.
Keywords
Artificial satellites -- Attitude control systems,
Artificial satellites,
RCM3400 microcontroller,
Attitude control system (ACS),
Kalman filtering