Abstract
The problem of autonomous aerial refueling autopilot design is considered using techniques from differential games and adaptive control. A closed-loop linear reference model is built using a differential game approach. This way derived optimal control is augmented with an adaptive signal for compensation of vortex induced uncertainties.
| Original language | English (US) |
|---|---|
| Title of host publication | Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference |
| Pages | 2745-2755 |
| Number of pages | 11 |
| Volume | 4 |
| State | Published - 2004 |
| Externally published | Yes |
| Event | Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference - Providence, RI, United States Duration: Aug 16 2004 → Aug 19 2004 |
Other
| Other | Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference |
|---|---|
| Country/Territory | United States |
| City | Providence, RI |
| Period | 8/16/04 → 8/19/04 |
ASJC Scopus subject areas
- Engineering(all)