Identification of UH‐60 Stability Derivative Models in Hover from Flight Test Data
- 1 January 1995
- journal article
- Published by AHS International dba Vertical Flight Society in Journal of the American Helicopter Society
- Vol. 40 (1) , 32-46
- https://doi.org/10.4050/jahs.40.32
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Analysis of propulsion system dynamics in the validation of a high-order state space model of the UH-60Published by American Institute of Aeronautics and Astronautics (AIAA) ,1992
- Preliminary design features of the RASCAL - A NASA/Army rotorcraft in-flight simulatorPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1992
- Frequency-Response Method for Rotorcraft System Identification: Flight Applications to BO 105 Coupled Rotor/Fuselage DynamicsJournal of the American Helicopter Society, 1992
- Validation of the Dynamic Response of a Blade‐Element UH‐60 Simulation Model in Hovering FlightJournal of the American Helicopter Society, 1991
- System identification requirements for high-bandwidth rotorcraft flight control system designJournal of Guidance, Control, and Dynamics, 1990
- Technical Note: Dynamic Inflow for Practical ApplicationsJournal of the American Helicopter Society, 1988