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) |
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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 |
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Country/Territory | United States |
City | Providence, RI |
Period | 8/16/04 → 8/19/04 |
ASJC Scopus subject areas
- Engineering(all)