TY - GEN
T1 - Robust trajectory-tracking method for UAV using nonlinear dynamic inversion
AU - Xie, Zhufeng
AU - Xia, Yuanqing
AU - Fu, Mengyin
PY - 2011
Y1 - 2011
N2 - This paper discusses the flight control strategy based on nonlinear dynamic inversion. A detailed description of a six-degree-of-freedom nonlinear flight control scheme for unmanned aerial vehicles (UAVs) is proposed for tracking the aircraft trajectory in three-dimensional space. Combining the PI control scheme, a nonlinear dynamic inversion controller is designed to linearize the dynamics of UAVs. Also, simulation results are presented to illustrate the effectiveness of the control strategy.
AB - This paper discusses the flight control strategy based on nonlinear dynamic inversion. A detailed description of a six-degree-of-freedom nonlinear flight control scheme for unmanned aerial vehicles (UAVs) is proposed for tracking the aircraft trajectory in three-dimensional space. Combining the PI control scheme, a nonlinear dynamic inversion controller is designed to linearize the dynamics of UAVs. Also, simulation results are presented to illustrate the effectiveness of the control strategy.
UR - https://www.scopus.com/pages/publications/82855176956
U2 - 10.1109/ICCIS.2011.6070308
DO - 10.1109/ICCIS.2011.6070308
M3 - Conference contribution
AN - SCOPUS:82855176956
SN - 9781612841984
T3 - Proceedings of the 2011 IEEE 5th International Conference on Cybernetics and Intelligent Systems, CIS 2011
SP - 93
EP - 98
BT - Proceedings of the 2011 IEEE 5th International Conference on Cybernetics and Intelligent Systems, CIS 2011
T2 - 2011 IEEE 5th International Conference on Cybernetics and Intelligent Systems, CIS 2011
Y2 - 17 September 2011 through 19 September 2011
ER -