Adaptive Feedback Linearization for the Control of a Typical Wing Section with Structural Nonlinearity
โ Scribed by Jeonghwan Ko; Thomas W. Strganac; Andrew J. Kurdila
- Book ID
- 110262078
- Publisher
- Springer Netherlands
- Year
- 1999
- Tongue
- English
- Weight
- 166 KB
- Volume
- 18
- Category
- Article
- ISSN
- 0924-090X
No coin nor oath required. For personal study only.
๐ SIMILAR VOLUMES
An output feedback controller is proposed for a class of uncertain nonlinear systems preceded by unknown backlash-like hysteresis, where the hysteresis is modeled by a differential equation. The unknown nonlinear functions are approximated by fuzzy systems based on universal approximation theorem, w
The output feedback pole placement problem is solved in an input-output algebraic formalism for linear time-varying (LTV) systems. The recent extensions of the notions of transfer matrices and poles of the system to the case of LTV systems are exploited here to provide constructive solutions based,