PG-EAM - Graduate Program in Aeronautical and Mechanical Engineering
PT EN
Article 2014

A Framework for Development of Satellite Attitude Control Algorithms

Authors

de Athayde Costa e Silva, Marsil
de Figueiredo, Helosman Valente
Boglietti, Benjamin Gilles Nicolas
Saotome, Osamu
Kienitz, Karl Heinz

Journal of Control Automation and Electrical Systems , vol. 25 , no. 6 , pp. 657-667

ISSN: 21953880

6
Citations
6
Authors

Abstract

© 2014, Brazilian Society for Automatics--SBA.This paper proposes a framework that combines three different environments with decreasing level of abstraction: model-in-the-loop, software-in-the-loop and hardware-in-the-loop. The purpose of the framework is to support the early detection of errors in the development of satellite control systems. Associated with the framework, the paper presents the MuSat simulator, a testbed for the development of satellite attitude controllers. MuSat is composed of a sphere that rotates with three degrees of freedom, supported by an air bearing system. The on-board computer of MuSat follows the integrated modular architecture, proposed for avionics systems. In order to illustrate both the framework and the testbed, we present the development of a non-linear control scheme. Results indicate that the designed control system fulfils the specified requirements. The example highlights the contribution of each environment of the framework for control system verification.

Keywords

Attitude control simulator Hardware-in-the-loop Model-based development Software-in-the-loop

Control and Systems Engineering (ENGI) Energy Engineering and Power Technology (ENER) Computer Science Applications (COMP) Electrical and Electronic Engineering (ENGI)
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Last Update: 2026-06-25
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