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Thrust-Induced Effects on a Pitching-Up Delta Wing Flow Field: Control of Stalled Wings
| Content Provider | Semantic Scholar |
|---|---|
| Author | Dommelen, Leon L. Van |
| Copyright Year | 1994 |
| Abstract | Abstract : Neural network procedures were explored with the objectives to control a delta wing in the non-linear domain. Results show that neural networks are well suited to represent non-linear computed lift and pressure forces on delta wings. A model problem, the flare maneuver, suggests that neural network controllers can perform well for non-linear systems provided that suitable input and training data are provided to it. |
| File Format | PDF HTM / HTML |
| DOI | 10.2514/6.1994-1856 |
| Alternate Webpage(s) | http://www.dtic.mil/get-tr-doc/pdf?AD=ADA310244 |
| Alternate Webpage(s) | https://doi.org/10.2514/6.1994-1856 |
| Language | English |
| Access Restriction | Open |
| Content Type | Text |
| Resource Type | Article |