TY - JOUR
T1 - Optimal adaptive integral sliding mode control for reentry vehicle attitude
AU - Geng, Jie
AU - Liu, Xiang Dong
AU - Sheng, Yong Zhi
AU - Cong, Bing Long
PY - 2013/9
Y1 - 2013/9
N2 - In this paper, an optimal adaptive integral sliding mode control (OAISMC) strategy is proposed for the reentry vehicle with a strong coupling, nonlinearity and uncertainty. Firstly, the State Dependent Riccati Equation (SDRE) is used to design the attitude controller for the nonlinear reentry vehicle without uncertainties. Then the integral sliding mode control theory is applied to reentry vehicle with parameter variations or external disturbances. By combining the integral sliding mode control theory with SDRE, the optimal performance index is achieved and the uncertainties can be rejected. Moreover, by using an adaptively adjusted switching gain, the upper bound of the lumped uncertainty is not required to be known. A sliding mode disturbance observer is introduced to improve the control performance. Finally, simulation is made in the presence of external disturbance and as well as perturbation by aerodynamic coefficients and atmospheric density. The validity and robustness of the proposed strategies are verified by simulation results.
AB - In this paper, an optimal adaptive integral sliding mode control (OAISMC) strategy is proposed for the reentry vehicle with a strong coupling, nonlinearity and uncertainty. Firstly, the State Dependent Riccati Equation (SDRE) is used to design the attitude controller for the nonlinear reentry vehicle without uncertainties. Then the integral sliding mode control theory is applied to reentry vehicle with parameter variations or external disturbances. By combining the integral sliding mode control theory with SDRE, the optimal performance index is achieved and the uncertainties can be rejected. Moreover, by using an adaptively adjusted switching gain, the upper bound of the lumped uncertainty is not required to be known. A sliding mode disturbance observer is introduced to improve the control performance. Finally, simulation is made in the presence of external disturbance and as well as perturbation by aerodynamic coefficients and atmospheric density. The validity and robustness of the proposed strategies are verified by simulation results.
KW - Adaptive integral sliding mode
KW - Disturbance observer
KW - Reentry attitude control
KW - State Dependent Riccati Equation (SDRE)
UR - http://www.scopus.com/inward/record.url?scp=84886619728&partnerID=8YFLogxK
U2 - 10.3873/j.issn.1000-1328.2013.09.006
DO - 10.3873/j.issn.1000-1328.2013.09.006
M3 - Article
AN - SCOPUS:84886619728
SN - 1000-1328
VL - 34
SP - 1215
EP - 1223
JO - Yuhang Xuebao/Journal of Astronautics
JF - Yuhang Xuebao/Journal of Astronautics
IS - 9
ER -