A discrete-time observer design for spacecraft attitude determination using an orthogonality preserving algorithm
This paper studies a nonlinear discrete-time partial state observer design problem for rigid spacecraft systems, particularly for spacecraft attitude estimation. The construction is inspired by an orthogonalitypreserving numerical algorithm, and it yields a semiglobal practical asymptotic observer....
| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
| Published: |
2011-05.
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| Subjects: | |
| Online Access: | Get fulltext |