Nonlinear control of a twin-lift helicopter configuration
- 1 November 1991
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 14 (6) , 1287-1293
- https://doi.org/10.2514/3.20785
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Pilot/vehicle analysis of a twin-lift helicopter configuration in hoverJournal of Guidance, Control, and Dynamics, 1988
- Nonlinear flight test trajectory controllers for aircraftJournal of Guidance, Control, and Dynamics, 1987
- Stability and Control of the Twin Lift Helicopter SystemJournal of the American Helicopter Society, 1985
- Global transformations of nonlinear systemsIEEE Transactions on Automatic Control, 1983