H-Infinity Static Output-feedback Control for Rotorcraft
- 2 August 2008
- journal article
- Published by Springer Science and Business Media LLC in Journal of Intelligent & Robotic Systems
- Vol. 54 (4), 629-646
- https://doi.org/10.1007/s10846-008-9279-5
Abstract
No abstract availableKeywords
This publication has 20 references indexed in Scilit:
- Evaluating H∞ controllers on the NRC Bell 205 fly-by-wire helicopterControl Engineering Practice, 2001
- Static output feedback controllers: stability and convexityIEEE Transactions on Automatic Control, 1998
- A cone complementarity linearization algorithm for static output-feedback and related problemsIEEE Transactions on Automatic Control, 1997
- Stabilization via static output feedbackIEEE Transactions on Automatic Control, 1993
- State-space solutions to standard H/sub 2/ and H/sub infinity / control problemsIEEE Transactions on Automatic Control, 1989
- Convergence of a numerical algorithm for calculating optimal output feedback gainsIEEE Transactions on Automatic Control, 1985
- Decentralised load-frequency controlIEE Proceedings D Control Theory and Applications, 1985
- Feedback and optimal sensitivity: Model reference transformations, multiplicative seminorms, and approximate inversesIEEE Transactions on Automatic Control, 1981
- Inclusion of Rotor Dynamics in Controller Design for HelicoptersJournal of Aircraft, 1973
- On an iterative technique for Riccati equation computationsIEEE Transactions on Automatic Control, 1968