Application of discrete time sliding mode control to a spacecraft in 6DoF
This paper presents the application of two separate discrete time sliding mode controllers, developed in conjunction with a potential function guidance method, to provide control in both position and attitude for a rigid, holonomic spacecraft body. The system is demonstrated in MATLABTM simulations...
| Main Authors: | , |
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| Format: | Article |
| Language: | English |
| Published: |
2010-04-30.
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| Subjects: | |
| Online Access: | Get fulltext |