TY - JOUR
T1 - Robust tracking for hypersonic vehicles subjected to mismatched uncertainties via fixed-time sliding mode control
AU - Guo, Jianguo
AU - Yang, Shengjiang
AU - Guo, Zongyi
N1 - Publisher Copyright:
© IMechE 2021.
PY - 2021/11
Y1 - 2021/11
N2 - This article investigates the robust tracking issue for the longitudinal dynamics of hypersonic vehicles subjected to mismatched uncertainties, and a novel sliding mode control approach is proposed to achieve the fixed-time convergence of tracking errors and satisfactory robustness against mismatched uncertainties. Establishing the control-oriented hypersonic vehicle model as velocity and altitude subsystems with mismatched uncertainties, the article introduces the nonlinear finite-time disturbance observer technique to estimate the uncertainties precisely. With the estimated uncertainties from the observer, the fixed-time sliding mode control is presented to track the velocity and altitude references. Consequently, the effect of the mismatched disturbances can be eliminated and the tracking performance can be improved. The stability of the closed-loop system is also analyzed. Numerical simulation results demonstrate the validity and superiority of the proposed control.
AB - This article investigates the robust tracking issue for the longitudinal dynamics of hypersonic vehicles subjected to mismatched uncertainties, and a novel sliding mode control approach is proposed to achieve the fixed-time convergence of tracking errors and satisfactory robustness against mismatched uncertainties. Establishing the control-oriented hypersonic vehicle model as velocity and altitude subsystems with mismatched uncertainties, the article introduces the nonlinear finite-time disturbance observer technique to estimate the uncertainties precisely. With the estimated uncertainties from the observer, the fixed-time sliding mode control is presented to track the velocity and altitude references. Consequently, the effect of the mismatched disturbances can be eliminated and the tracking performance can be improved. The stability of the closed-loop system is also analyzed. Numerical simulation results demonstrate the validity and superiority of the proposed control.
KW - finite-time disturbance observer
KW - fixed-time stability
KW - Hypersonic vehicle
KW - mismatched uncertainties
KW - tracking control
UR - http://www.scopus.com/inward/record.url?scp=85102686813&partnerID=8YFLogxK
U2 - 10.1177/0954410021990239
DO - 10.1177/0954410021990239
M3 - 文章
AN - SCOPUS:85102686813
SN - 0954-4100
VL - 235
SP - 2145
EP - 2153
JO - Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
JF - Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
IS - 14
ER -