Attitude pointing enhancement for combined energy and attitude control system
This paper extends the previous works that appeared in Acta Astronautica. An approach that incorporates the Active Force Control (AFC) technique into a conventional Proportional-Derivative (PD) controller is proposed for a 50 kg small satellite. Numerical treatments are performed to validate the eff...
| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
| Published: |
Elsevier
2011
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| Online Access: | http://psasir.upm.edu.my/id/eprint/23142/1/Attitude%20pointing%20enhancement%20for%20combined%20energy%20and%20attitude%20control%20system.pdf |