Design of restructurable flight control systems using feedback linearization
- 1 September 1991
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 14 (5) , 903-911
- https://doi.org/10.2514/3.20730
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
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- Aircraft automatic flight control system with model inversionJournal of Guidance, Control, and Dynamics, 1987
- Application of nonlinear transformations to automatic flight controlAutomatica, 1984
- The structure of decoupled non-linear systemsInternational Journal of Control, 1975
- Diagonalization and inverses for non-linear systems†International Journal of Control, 1970