Two degree-of-freedom spacecraft attitude controller
Two degree-of-freedom controller is designed together with its governing equations for a spacecraft pitch attitude control. The attitude controller incorporates the Active Force Control (AFC) technique into the conventional Proportional-Derivative (PD) controller based spacecraft pitch attitude loop...
| 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/23143/ http://psasir.upm.edu.my/id/eprint/23143/ http://psasir.upm.edu.my/id/eprint/23143/1/Two%20degree-of-freedom%20spacecraft%20attitude%20controller.pdf |