Controller design for a nonlinear morphing UAV
| dc.contributor.author | Aponso, Gayanath | |
| dc.contributor.author | Chakravarthy, Animesh | |
| dc.date.accessioned | 2013-11-18T19:49:41Z | |
| dc.date.available | 2013-11-18T19:49:41Z | |
| dc.date.issued | 2013-11-18 | |
| dc.date.published | 2013 | en_US |
| dc.description.abstract | In this work, we provide details of the control design of a morphing UAV capable of variable wing sweep. This morphing capability is assumed to be superimposed on a GENMAV (Generic Micro Air Vehicle) configuration originally developed by the Air Force Research Laboratory (AFRL). The nonlinear aerodynamic model for this aircraft is obtained using the Athena-Vortex Lattice (AVL) method with a quasi-steady state assumption. | en_US |
| dc.description.conference | Kansas Unmanned Systems Conference, Manhattan, KS, October 14-16, 2013 | en_US |
| dc.identifier.uri | http://hdl.handle.net/2097/16814 | |
| dc.language.iso | en_US | en_US |
| dc.publisher | Kansas State University | en_US |
| dc.subject | Aerodynamics | en_US |
| dc.subject | Morphing | en_US |
| dc.subject | Unmanned air vehicles | en_US |
| dc.title | Controller design for a nonlinear morphing UAV | en_US |
| dc.type | Text | en_US |
