TY - GEN
T1 - Attitude and altitude control on board of an ornithopter
AU - Torres, Jazmin Zenteno
AU - Davila, Jorge
AU - Lozano, Rogelio
N1 - Publisher Copyright:
© 2016 IEEE.
PY - 2016/6/30
Y1 - 2016/6/30
N2 - This paper presents the modeling, the design of control laws, for Euler angles and altitude, and their implementation. The proposed controller is based on the backstepping procedure and uses a state feedback linearizing technique to guarantee tracking of the desired Euler angles and altitude on the ornithopter. The provided controller provides exponential convergence to the desired values. Numerical and experimental applications of the proposed algorithm illustrates the performance of the control technique.
AB - This paper presents the modeling, the design of control laws, for Euler angles and altitude, and their implementation. The proposed controller is based on the backstepping procedure and uses a state feedback linearizing technique to guarantee tracking of the desired Euler angles and altitude on the ornithopter. The provided controller provides exponential convergence to the desired values. Numerical and experimental applications of the proposed algorithm illustrates the performance of the control technique.
UR - http://www.scopus.com/inward/record.url?scp=84979775132&partnerID=8YFLogxK
U2 - 10.1109/ICUAS.2016.7502666
DO - 10.1109/ICUAS.2016.7502666
M3 - Contribución a la conferencia
AN - SCOPUS:84979775132
T3 - 2016 International Conference on Unmanned Aircraft Systems, ICUAS 2016
SP - 1124
EP - 1130
BT - 2016 International Conference on Unmanned Aircraft Systems, ICUAS 2016
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 2016 International Conference on Unmanned Aircraft Systems, ICUAS 2016
Y2 - 7 June 2016 through 10 June 2016
ER -