TY - GEN
T1 - Design and control of a tri-rotor aircraft
AU - Fan, Penghui
AU - Wang, Xinhua
AU - Cai, Kai Yuan
PY - 2010
Y1 - 2010
N2 - In this paper, a tri-rotor aircraft is designed, which can vertically take off and land, and moreover fly forward with a high speed. Two fixed wings are added to the tri-rotor aircraft, therefore, the ability of high-speed forward flight is guaranteed. A controller is presented using back-stepping technique to achieve mode transition control of the aircraft. Finally, the theoretical result is confirmed by computer simulations.
AB - In this paper, a tri-rotor aircraft is designed, which can vertically take off and land, and moreover fly forward with a high speed. Two fixed wings are added to the tri-rotor aircraft, therefore, the ability of high-speed forward flight is guaranteed. A controller is presented using back-stepping technique to achieve mode transition control of the aircraft. Finally, the theoretical result is confirmed by computer simulations.
UR - https://www.scopus.com/pages/publications/77957886540
U2 - 10.1109/ICCA.2010.5524420
DO - 10.1109/ICCA.2010.5524420
M3 - 会议稿件
AN - SCOPUS:77957886540
SN - 9781424451951
T3 - 2010 8th IEEE International Conference on Control and Automation, ICCA 2010
SP - 1972
EP - 1977
BT - 2010 8th IEEE International Conference on Control and Automation, ICCA 2010
T2 - 2010 8th IEEE International Conference on Control and Automation, ICCA 2010
Y2 - 9 June 2010 through 11 June 2010
ER -