H(infinity) helicopter flight control law design with and without rotor state feedback
- 9 August 1993
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Helicopter flight-control design using an H(2) methodPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1991
- Design of attitude and rate command systems for helicopters using eigenstructure assignmentJournal of Guidance, Control, and Dynamics, 1989
- 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