Attitude Control Augmentation for Combined Attitude and Thermal Control System.
An approach that incorporates the Active Force Control (AFC) technique into a conventional Proportional-Derivative (PD) controller is proposed for spacecraft attitude controls. The combined attitude and thermal control system (CATCS) is proposed as an attitude control actuator. All the governing equ...
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| Main Authors: | , |
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| Format: | Article |
| Language: | English English |
| Published: |
2011
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| Online Access: | http://psasir.upm.edu.my/id/eprint/23356/1/Attitude%20Control%20Augmentation%20for%20Combined%20Attitude%20and%20Thermal%20Control%20System.pdf http://psasir.upm.edu.my/id/eprint/23356/ |
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