Quaternion Parameterization and a Simple Algorithm for Global Attitude Estimation
- 1 July 1998
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 21 (4), 669-672
- https://doi.org/10.2514/2.4290
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
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- Robust attitude stabilization of spacecraft using nonlinear quaternion feedbackIEEE Transactions on Automatic Control, 1995
- The attitude control problemIEEE Transactions on Automatic Control, 1991
- Three-axis attitude determination from vector observationsJournal of Guidance and Control, 1981
- A Least Squares Estimate of Satellite AttitudeSiam Review, 1965