Development of attitude control system on RCM3400 microcontroller

This paper describes the development of a nano-satellite altitude control system (ACS) which employ a filter base controller with comparison with a simple adaptive predictive fuzzy logic controller (APFLC) for a 1, 2 and 3 axis orientation using RCM3400 controller. For this the paper describe about the different performance both controller apply in the hardware. The physical interface, module and configuration with several key features are described. The result of the controller apply in to the hardware is shown in this paper. The interface, communication protocol and data handling for the microcontroller are described in this paper.