Rotor‐State Feedback in the Design of Flight Control Laws for a Hovering Helicopter
- 1 January 1994
- journal article
- Published by AHS International dba Vertical Flight Society in Journal of the American Helicopter Society
- Vol. 39 (1) , 50-62
- https://doi.org/10.4050/jahs.39.50
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Validation of the Dynamic Response of a Blade‐Element UH‐60 Simulation Model in Hovering FlightJournal of the American Helicopter Society, 1991
- Helicopter flight-control design using an H(2) methodPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1991
- Design of attitude and rate command systems for helicopters using eigenstructure assignmentJournal of Guidance, Control, and Dynamics, 1989
- Inclusion of Rotor Dynamics in Controller Design for HelicoptersJournal of Aircraft, 1973