Design and robustness issues for highly augmented helicopter controls
- 1 November 1992
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 15 (6) , 1375-1380
- https://doi.org/10.2514/3.11399
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
- Beyond singular values and loop shapesJournal of Guidance, Control, and Dynamics, 1991
- Reduced-order modeling and controller design for a high-performance helicopterJournal of Guidance, Control, and Dynamics, 1990
- Design of attitude and rate command systems for helicopters using eigenstructure assignmentJournal of Guidance, Control, and Dynamics, 1989
- Assessment of Digital Flight‐Control Technology for Advanced Combat RotorcraftJournal of the American Helicopter Society, 1989
- Multivariable feedback design: Concepts for a classical/modern synthesisIEEE Transactions on Automatic Control, 1981
- Superiority of transfer function over state-variable methods in linear time-invariant feedback system designIEEE Transactions on Automatic Control, 1975