TY - GEN
T1 - An aircraft adaptive control architecture based on nominal controller
AU - Zhang, Bo
AU - Wang, Shushan
PY - 2012
Y1 - 2012
N2 - This paper presents adaptive control architecture for the safe flight of a transport aircraft under adverse operating conditions and uncertainties. This architecture combines a nominal controller based on an LQR with integral action, and an adaptive controller that accommodates for actuator saturation and disturbances. In this paper, we consider the control of the C-5 transport aircraft, which is similar to the Generic Transport Model. We delineate the underlying nonlinear dynamic model and introduce various upsets, damages, and failures by representing these various adverse conditions in the form of uncertainties.
AB - This paper presents adaptive control architecture for the safe flight of a transport aircraft under adverse operating conditions and uncertainties. This architecture combines a nominal controller based on an LQR with integral action, and an adaptive controller that accommodates for actuator saturation and disturbances. In this paper, we consider the control of the C-5 transport aircraft, which is similar to the Generic Transport Model. We delineate the underlying nonlinear dynamic model and introduce various upsets, damages, and failures by representing these various adverse conditions in the form of uncertainties.
KW - Adaptive control architecture
KW - Aircraft
KW - Nominal controller
UR - http://www.scopus.com/inward/record.url?scp=84859171704&partnerID=8YFLogxK
U2 - 10.4028/www.scientific.net/AMR.490-495.105
DO - 10.4028/www.scientific.net/AMR.490-495.105
M3 - Conference contribution
AN - SCOPUS:84859171704
SN - 9783037853849
T3 - Advanced Materials Research
SP - 105
EP - 109
BT - Mechatronics and Intelligent Materials II
T2 - 2nd International Conference on Mechatronics and Intelligent Materials 2012, MIM 2012
Y2 - 18 May 2012 through 19 May 2012
ER -