TY - JOUR
T1 - Disturbance Observer-Based Nonlinear Model Predictive Control for Air-Breathing Hypersonic Vehicles
AU - Guo, Jianguo
AU - Peng, Qian
AU - Zhou, Jun
N1 - Publisher Copyright:
© 2018 American Society of Civil Engineers.
PY - 2019/1/1
Y1 - 2019/1/1
N2 - The disturbance-observer-based nonlinear model predictive control (DOB-NMPC) for air-breathing hypersonic vehicles (AHVs) is proposed in this paper. The longitudinal dynamic model of generic AHVs is first redesigned and optimized for prediction, whereas the cost function of nonlinear model predictive control (NMPC) is designed with series expansions and derivative feedback. A disturbance-observer-based control (DOBC) law is then developed for enhancing robustness in the presence of external disturbances and parameter uncertainties. The relationship among tracking errors, sample time, and estimation errors is finally investigated. Compared with existing tracking control for AHVs, the proposed DOB-NMPC achieves tracking commands effectively without sacrificing the nominal tracking performance, and the convergence range of tracking errors is verified by stability analysis and simulation studies.
AB - The disturbance-observer-based nonlinear model predictive control (DOB-NMPC) for air-breathing hypersonic vehicles (AHVs) is proposed in this paper. The longitudinal dynamic model of generic AHVs is first redesigned and optimized for prediction, whereas the cost function of nonlinear model predictive control (NMPC) is designed with series expansions and derivative feedback. A disturbance-observer-based control (DOBC) law is then developed for enhancing robustness in the presence of external disturbances and parameter uncertainties. The relationship among tracking errors, sample time, and estimation errors is finally investigated. Compared with existing tracking control for AHVs, the proposed DOB-NMPC achieves tracking commands effectively without sacrificing the nominal tracking performance, and the convergence range of tracking errors is verified by stability analysis and simulation studies.
KW - Air-breathing hypersonic vehicle
KW - Derivative feedback
KW - Disturbance observer
KW - Model predictive control
KW - Stability analysis
UR - http://www.scopus.com/inward/record.url?scp=85054258288&partnerID=8YFLogxK
U2 - 10.1061/(ASCE)AS.1943-5525.0000948
DO - 10.1061/(ASCE)AS.1943-5525.0000948
M3 - 文章
AN - SCOPUS:85054258288
SN - 0893-1321
VL - 32
JO - Journal of Aerospace Engineering
JF - Journal of Aerospace Engineering
IS - 1
M1 - 04018121
ER -