Design and test of flight control laws for the Kaman Burro unmanned aerial vehicle
- 14 August 2000
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- Technical Note: Robust Multivariable Control of Rotorcraft in Forward Flight: Impact of Bandwidth on Fatigue LifeJournal of the American Helicopter Society, 1998
- Frequency-Response Method for Rotorcraft System Identification: Flight Applications to BO 105 Coupled Rotor/Fuselage DynamicsJournal of the American Helicopter Society, 1992