Disturbance observer-based fuzzy control for flexible spacecraft combined attitude & sun tracking system
This paper investigates the combined attitude and sun-tracking control problem in the presence of external disturbances and internal disturbances, caused by flexible appendages. A new method based on Pythagorean trigonometric identity is proposed to drive the solar arrays. Using the control input an...
| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
| Published: |
Elsevier
2017
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| Online Access: | http://psasir.upm.edu.my/id/eprint/61506/ http://psasir.upm.edu.my/id/eprint/61506/1/Disturbance%20observer-based%20fuzzy%20control%20for%20flexible%20spacecraft%20combined%20attitude%20%26%20sun%20tracking%20system.pdf |