The SDRE based Second Order Integral Sliding Mode Control for Attitude of Reentry Vehicle

被引:0
|
作者
Geng Jie [1 ,2 ]
Sheng Yongzhi [1 ,2 ]
Liu Xiangdong [1 ,2 ]
Wang Liang [1 ,2 ]
机构
[1] Beijing Inst Technol, Sch Automat, Beijing 100081, Peoples R China
[2] Minist Educ, Key Lab Complex Syst Intelligent Control & Decis, Beijing 100081, Peoples R China
基金
高等学校博士学科点专项科研基金;
关键词
Flight vehicle control; State dependent Riccati equation(SDRE); Second order integral sliding mode; DEPENDENT RICCATI EQUATION; DC MOTORS; TRACKING;
D O I
暂无
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
In this paper, a state dependent Riccati equation-based second order integral sliding mode control(SSOISMC) algorithm is proposed for the reentry vehicle with a strong coupling, nonlinearity and uncertainty. Firstly, the state dependent Riccati equation (SDRE) controller is developed to approach the attitude controller for the nonlinear reentry vehicle without uncertainties. Then the second order integral sliding mode control theory is proposed to combine sliding mode with SDRE, and it is applied to reentry vehicle with parameter variations or external disturbances. The achievement of the second order sliding phase is proved. By the proposed control law, the optimal performance index is achieved and the uncertainties are rejected, furthermore, the chattering is alleviated. Finally, simulation is made through the assumption that aerodynamic parameters and atmospheric density are perturbed. The validity and robustness of the proposed strategies are verified by simulation results.
引用
收藏
页码:441 / 446
页数:6
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