Helicopter flight-control design using an H(2) method
- 12 August 1991
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Principal component analysis in linear systems: Controllability, observability, and model reductionIEEE Transactions on Automatic Control, 1981
- Analytical Design of a High Performance Stability and Control Augmentation System for a Hingeless Rotor HelicopterJournal of the American Helicopter Society, 1979
- Analytical Design of a High Performance Stability and Control Augmentation System for a Hingeless Rotor HelicopterJournal of the American Helicopter Society, 1979