Abstract
This paper presents a pilot model for fault detection. The pilot detection process is examined and a model based on an extended Kalman filter is derived. Evaluation is performed using a simulation of a B737. Failures are injected and the detection capabilities of the Kalman filter-based model are demonstrated.
| Original language | English (US) |
|---|---|
| Pages | 3D31-3D39 |
| State | Published - 2001 |
| Event | 20th Digital Avionics Systems Conference Proceedings - Daytona Beach, FL, United States Duration: Oct 14 2001 → Oct 18 2001 |
Other
| Other | 20th Digital Avionics Systems Conference Proceedings |
|---|---|
| Country/Territory | United States |
| City | Daytona Beach, FL |
| Period | 10/14/01 → 10/18/01 |
All Science Journal Classification (ASJC) codes
- Aerospace Engineering
- Electrical and Electronic Engineering