1. Architecture for Combined Energy and Attitude Control System
- Author
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Harlisya Harun, Mohd Nizam Filipski, Renuganth Varatharajoo, and Ibrahim Mustafa Mehedi
- Subjects
Engineering ,Multidisciplinary ,business.industry ,Control engineering ,Transfer function ,Energy storage ,Space exploration ,Flywheel ,Attitude control ,Test case ,Control theory ,Torque ,business ,Energy (signal processing) - Abstract
Combining the energy and attitude control system is a feasible technology for small satellites to improve the space missions. In this Combined Energy and Attitude Control System (CEACS) a double rotating flywheel is used to replace the conventional battery for energy storage as well as to control the attitude of an earth oriented satellite. Each flywheel is to be controlled in the torque mode. The energy and attitude inputs for the flywheels' control architecture are also in the torque mode. All related mathematical representation along with the relevant transfer functions and the required numerical calculation are developed. The goals are to analyze the attitude performance with respect to the ideal and non-ideal test cases for a chosen reference mission.
- Published
- 2005
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