Calculation of trim settings for a helicopter rotor by an optimized automatic controller
- 1 January 1984
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 7 (1) , 85-91
- https://doi.org/10.2514/3.8549
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Application of unsteady airfoil theory to rotary wingsJournal of Aircraft, 1980
- Flap-Lag Stability of Helicopter Rotor Blades in Forward FlightJournal of the American Helicopter Society, 1975