H∞ control option for a combined energy and attitude control system
A combined energy and attitude control system (CEACS) is a hybrid system that uses flywheels to store energy and provide a simultaneous attitude control in satellites. Previous work appeared in Advances in Space Research (ASR) employing the proportional-derivative (PD) control has proven that CEACS...
| Main Authors: | Ying, Siang Ban, Varatharajoo, Renuganth |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
Committee on Space Research
2013
|
| Online Access: | http://psasir.upm.edu.my/id/eprint/28880/ http://psasir.upm.edu.my/id/eprint/28880/1/H%E2%88%9E%20control%20option%20for%20a%20combined%20energy%20and%20attitude%20control%20system.pdf |
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