System Identification for Small, Low-Cost, Fixed-Wing Unmanned Aircraft
- 1 July 2013
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 50 (4), 1117-1130
- https://doi.org/10.2514/1.c032065
Abstract
No abstract availableThis publication has 13 references indexed in Scilit:
- A New System Identification Method Using Short Duration Flight Test InputsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2011
- Frequency Domain System Identification for a Small, Low-Cost, Fixed-Wing UAVPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2011
- System Identification of a Quadrotor Micro Air VehiclePublished by American Institute of Aeronautics and Astronautics (AIAA) ,2010
- Real-Time Dynamic Modeling: Data Information Requirements and Flight-Test ResultsJournal of Aircraft, 2009
- The Equations of MotionPublished by Elsevier BV ,2007
- Development of a Low-Cost Sub-Scale Aircraft for Flight Research: The FASER ProjectPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2006
- Rapid Frequency-Domain Modeling Methods for Unmanned Aerial Vehicle Flight Control ApplicationsJournal of Aircraft, 2004
- Low-Order Equivalent System Identification for the Tu-144LL Supersonic Transport AircraftJournal of Guidance, Control, and Dynamics, 2003
- System Identification Modeling of a Small-Scale Unmanned Rotorcraft for Flight Control DesignJournal of the American Helicopter Society, 2002
- System IdentificationPublished by Wiley ,1999