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Robust and optimal attitude control of spacecraft with inertia uncertainties using minimal kinematic parameters.
- Source :
-
Aerospace Science & Technology . Jul2016, Vol. 54, p276-285. 10p. - Publication Year :
- 2016
-
Abstract
- In this paper a robust and optimal attitude control design that uses the minimal kinematic parameters and angular velocities feedback is presented for the three-axis attitude stabilization of spacecraft with inertia uncertainties. After proposing a new class of robust attitude control laws for the three-axis attitude stabilization of spacecraft with inertia uncertainties, it is shown that the proposed robust attitude control laws are optimal with respect to performance indices. A numerical example is given to illustrate the theoretical results presented in this paper. [ABSTRACT FROM AUTHOR]
Details
- Language :
- English
- ISSN :
- 12709638
- Volume :
- 54
- Database :
- Academic Search Index
- Journal :
- Aerospace Science & Technology
- Publication Type :
- Academic Journal
- Accession number :
- 115800142
- Full Text :
- https://doi.org/10.1016/j.ast.2016.04.027