Abstract
In this article, the design, system modeling and control of a new hybrid type of Unmanned Aerial Vehicle (UAV) is presented. Based on the flight principles of the Dos Samara UAV, a new vehicle that combines the capability of hovering, like a helicopter, and high speed-increased endurance flying, like a fixed-wing aircraft, is designed. The nonlinear dynamics model of the aircraft operating in helicopter mode is derived and linearized around hovering operation. Based on this model an LQ-controller is designed. The performance of the overall system is examined in simulation studies.
| Original language | English (US) |
|---|---|
| Title of host publication | 2012 IEEE International Conference on Robotics and Automation, ICRA 2012 |
| Publisher | Institute of Electrical and Electronics Engineers Inc. |
| Pages | 3645-3650 |
| Number of pages | 6 |
| ISBN (Print) | 9781467314039 |
| DOIs | |
| State | Published - Jan 1 2012 |
| Event | 2012 IEEE International Conference on Robotics and Automation, ICRA 2012 - Saint Paul, MN, United States Duration: May 14 2012 → May 18 2012 |
Other
| Other | 2012 IEEE International Conference on Robotics and Automation, ICRA 2012 |
|---|---|
| Country | United States |
| City | Saint Paul, MN |
| Period | 5/14/12 → 5/18/12 |
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ASJC Scopus subject areas
- Software
- Control and Systems Engineering
- Artificial Intelligence
- Electrical and Electronic Engineering
Cite this
Revisited Dos Samara unmanned aerial vehicle : Design and control. / Alexis, Kostas; Tzes, Antonios.
2012 IEEE International Conference on Robotics and Automation, ICRA 2012. Institute of Electrical and Electronics Engineers Inc., 2012. p. 3645-3650 6224559.Research output: Chapter in Book/Report/Conference proceeding › Conference contribution
}
TY - GEN
T1 - Revisited Dos Samara unmanned aerial vehicle
T2 - Design and control
AU - Alexis, Kostas
AU - Tzes, Antonios
PY - 2012/1/1
Y1 - 2012/1/1
N2 - In this article, the design, system modeling and control of a new hybrid type of Unmanned Aerial Vehicle (UAV) is presented. Based on the flight principles of the Dos Samara UAV, a new vehicle that combines the capability of hovering, like a helicopter, and high speed-increased endurance flying, like a fixed-wing aircraft, is designed. The nonlinear dynamics model of the aircraft operating in helicopter mode is derived and linearized around hovering operation. Based on this model an LQ-controller is designed. The performance of the overall system is examined in simulation studies.
AB - In this article, the design, system modeling and control of a new hybrid type of Unmanned Aerial Vehicle (UAV) is presented. Based on the flight principles of the Dos Samara UAV, a new vehicle that combines the capability of hovering, like a helicopter, and high speed-increased endurance flying, like a fixed-wing aircraft, is designed. The nonlinear dynamics model of the aircraft operating in helicopter mode is derived and linearized around hovering operation. Based on this model an LQ-controller is designed. The performance of the overall system is examined in simulation studies.
UR - http://www.scopus.com/inward/record.url?scp=84864454200&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=84864454200&partnerID=8YFLogxK
U2 - 10.1109/ICRA.2012.6224559
DO - 10.1109/ICRA.2012.6224559
M3 - Conference contribution
AN - SCOPUS:84864454200
SN - 9781467314039
SP - 3645
EP - 3650
BT - 2012 IEEE International Conference on Robotics and Automation, ICRA 2012
PB - Institute of Electrical and Electronics Engineers Inc.
ER -