Rotorcraft flight control system design based on multi-criterion parametric optimization
- 7 August 1995
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Rotorcraft Control System Design for Uncertain Vehicle Dynamics Using Quantitative Feedback TheoryJournal of the American Helicopter Society, 1994
- Robust crossfeed design for hovering rotorcraftInternational Journal of Robust and Nonlinear Control, 1994
- Flying quality analysis and flight evaluation of a highly augmented combat rotorcraftJournal of Guidance, Control, and Dynamics, 1991
- Synthesis of a helicopter full authority controllerPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989