Abstract
Modelling of innovative aircraft such as UAV's, X-wing, tilt body, delta-wing is not easy. This paper presents nonlinear system identification method for modelling air vehicles of complex configuration. This approach is demonstrated through a laboratory helicopter. Extensive time and frequency-domain model-validation tests are employed to instil confidence in the estimated model. The estimated model has a good predictive capability and can be utilized for nonlinear flight simulation studies. The approach presented is suitable for modelling new generation air vehicles.
| Original language | English |
|---|---|
| Pages | 313-320 |
| Number of pages | 8 |
| State | Published - 2000 |
| Externally published | Yes |
| Event | IEEE 2000 National Aerospace and Electronics Conference (NAECON 2000) - Dayton, OH, USA Duration: 10 Oct 2000 → 12 Oct 2000 |
Conference
| Conference | IEEE 2000 National Aerospace and Electronics Conference (NAECON 2000) |
|---|---|
| City | Dayton, OH, USA |
| Period | 10/10/00 → 12/10/00 |
ASJC Scopus subject areas
- General Engineering
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