Optimal control alleviation of tilting proprotor gust response
- 1 March 1977
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 14 (3) , 301-308
- https://doi.org/10.2514/3.44594
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Inclusion of Rotor Dynamics in Controller Design for HelicoptersJournal of Aircraft, 1973
- Linear Optimal ControlJournal of Dynamic Systems, Measurement, and Control, 1971
- Atmospheric turbulence considerations for future aircraft designed to operate at low altitudes.Journal of Aircraft, 1968