Design of flight control systems to meet rotorcraft handling qualities specifications
- 1 January 1993
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 16 (1) , 69-78
- https://doi.org/10.2514/3.11429
Abstract
No abstract availableThis publication has 10 references indexed in Scilit:
- Design of a Multivariable Helicopter Flight Control System for Handling Qualities EnhancementJournal of the American Helicopter Society, 1990
- Reduced-order modeling and controller design for a high-performance helicopterJournal of Guidance, Control, and Dynamics, 1990
- Simulation investigation of the effects of helicopter hovering dynamics on pilot performanceJournal of Guidance, Control, and Dynamics, 1990
- Performance — robustness trade off of eigenstructure assignment applied to rotorcraftThe Aeronautical Journal, 1990
- Literal singular-value-based flight control system design techniquesJournal of Guidance, Control, and Dynamics, 1989
- 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
- Structured stability robustness improvement by eigenspace techniques- A hybrid methodologyJournal of Guidance, Control, and Dynamics, 1989
- Eigenstructure Assignment for Linear SystemsIEEE Transactions on Aerospace and Electronic Systems, 1983
- Robustness results in linear-quadratic Gaussian based multivariable control designsIEEE Transactions on Automatic Control, 1981