A novel design of spacecraft combined attitude & sun tracking system using a versatile fuzzy controller
Purpose – The purpose of this paper is to develop a theoretical design for the alternative attitude control of the rotation about the pitch axis for the nadir-pointing spacecraft in the event of inertial actuator faults. Design/methodology/approach – This paper presents a novel and viable solut...
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| Main Authors: | , |
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| Format: | Article |
| Language: | English |
| Published: |
Emerald Group Publishing
2015
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| Online Access: | http://psasir.upm.edu.my/id/eprint/43535/1/abstract00.pdf http://psasir.upm.edu.my/id/eprint/43535/ http://www.emeraldinsight.com/1748-8842.htm |
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