Attitude control optimization for a small-scale unmanned helicopter
- 14 August 2000
- conference paper
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- A multidisciplinary flight control development environment and its application to a helicopterIEEE Control Systems, 1999
- Frequency-Response Method for Rotorcraft System Identification: Flight Applications to BO 105 Coupled Rotor/Fuselage DynamicsJournal of the American Helicopter Society, 1992