TY - JOUR
T1 - Finite-time super-twisting sliding mode control for Mars entry trajectory tracking
AU - Zhao, Zhenhua
AU - Yang, Jun
AU - Li, Shihua
AU - Zhang, Zhenxing
AU - Guo, Lei
N1 - Publisher Copyright:
© 2015 The Franklin Institute. Published by Elsevier Ltd. All rights reserved.
PY - 2015/11
Y1 - 2015/11
N2 - The robust tracking control problem for Mars entry vehicles subject to parameter perturbations, external disturbances and initial state errors during the entry phase is investigated in this paper. A new finite-time super-twisting (FTSTW) control law is proposed by designing a nonsingular terminal sliding mode (NTSM) surface for Mars entry trajectory tracking. The proposed FTSTW controller exhibits not only strong robustness against parameter perturbations, external disturbances and initial state errors but also the property of finite-time convergence of tracking error. Moreover, compared with traditional sliding mode control method, the control input (namely, the bank angle) of the proposed control approach is continuous which effectively avoids high-frequency switching and sharp change of control action. The merits of the proposed method are validated by implementing simulation studies on Mars entry vehicle system with disturbances and uncertainties. The results of a 500-run Monte Carlo simulation show that the proposed controller provides a promising solution for high-precision Mars entry trajectory tracking.
AB - The robust tracking control problem for Mars entry vehicles subject to parameter perturbations, external disturbances and initial state errors during the entry phase is investigated in this paper. A new finite-time super-twisting (FTSTW) control law is proposed by designing a nonsingular terminal sliding mode (NTSM) surface for Mars entry trajectory tracking. The proposed FTSTW controller exhibits not only strong robustness against parameter perturbations, external disturbances and initial state errors but also the property of finite-time convergence of tracking error. Moreover, compared with traditional sliding mode control method, the control input (namely, the bank angle) of the proposed control approach is continuous which effectively avoids high-frequency switching and sharp change of control action. The merits of the proposed method are validated by implementing simulation studies on Mars entry vehicle system with disturbances and uncertainties. The results of a 500-run Monte Carlo simulation show that the proposed controller provides a promising solution for high-precision Mars entry trajectory tracking.
UR - https://www.scopus.com/pages/publications/84946486479
U2 - 10.1016/j.jfranklin.2015.08.022
DO - 10.1016/j.jfranklin.2015.08.022
M3 - 文章
AN - SCOPUS:84946486479
SN - 0016-0032
VL - 352
SP - 5226
EP - 5248
JO - Journal of the Franklin Institute
JF - Journal of the Franklin Institute
IS - 11
ER -