Abstract
Six methods of training neural networks to represent aerodynamic data are compared. Prior research has shown that the extended Kalman filter provides speed and accuracy advantages over the back-propagation method, and further quickening of training is desirable. We investigate four filter-based approaches (standard filter without process "noise", setting lower bounds on estimate-error covariance, periodically re-initializing the estimate-error covariance, and adding fictitious "process noise") and compare them to approaches incorporating genetic algorithms. A genetic algorithm uses a global search of the network weight space to identify feasible weights. Here, the algorithm is used independently and as a starting step for an extended Kalman filter. While the initial global search is intuitively appealing and may have value in some applications, the randomly initialized additive-noise filter is found to be the fastest training method in the present study.
| Original language | English (US) |
|---|---|
| Pages | 598-604 |
| Number of pages | 7 |
| State | Published - 1997 |
| Event | 22nd Atmospheric Flight Mechanics Conference, 1997 - New Orleans, United States Duration: Aug 11 1997 → Aug 13 1997 |
Other
| Other | 22nd Atmospheric Flight Mechanics Conference, 1997 |
|---|---|
| Country/Territory | United States |
| City | New Orleans |
| Period | 8/11/97 → 8/13/97 |
All Science Journal Classification (ASJC) codes
- General Energy
- Aerospace Engineering