Gust Load Alleviation for an Aeroelastic System Using Nonlinear Control
The author develops a nonlinear longitudinal model of an aircraft modeled by rigid fuselage, tail, and wing, where the wing is attached to the fuselage with a torsional spring. The main focus of this research is to retain the full nonlinearities associated with the system and to perform gust load al...
| Main Author: | |
|---|---|
| Other Authors: | |
| Format: | Others |
| Language: | en_US |
| Published: |
2010
|
| Subjects: | |
| Online Access: | http://hdl.handle.net/1969.1/ETD-TAMU-2009-08-1504 |