[1]WALLNER E M, SHTESSEL Y. Sliding mode disturbance observerbased control for a reusable launch vehicle[J].Journal of Guidance, Control and Dynamics, 2006,29(6):13151328.
[2]DOMAN D B, NGO A D. Dynamic inversion based adaptivereconfigurable control of the X33 on ascent[J].Journal of Guidance, Control and Dynamics,2002,25(2):275284.
[3]VANSOEST W R, CHU Q P, MULDER J A. Combined feedback linearization and constrained model predictive control for entry flight[J].Journal of Guidance, Control and Dynamics,2006,29(2):427434.
[4]MOOIJ E. Numerical investigation of model reference adaptive control for hypersonic aircraft[J].Journal of Guidance, Control and Dynamics,2001,24(2):315323.
[5]董琦,宗群,王芳,等.基于光滑二阶滑模的可重复使用运载器有限时间再入姿态控制[J].控制理论与应用,2015,32(4):448455.
DONG Q, ZONG Q, WANG F, et al. Finite time smooth secondorder slidingmode controller design for reentry reusable launch vehicle[J].Control Theory & Applications,2015,32(4):448455.
[6]龚宇莲,吴宏鑫.基于特征模型的高超声速飞行器的自适应姿态控制[J].宇航学报,2010,31(9):21222128.
GONG Y L, WU H X. Characteristic modelbased adaptive attitude control for hypersonic vehicle[J].Journal of Astronautics,2010,31(9):21222128.
[7]陈上上,何英姿,刘贺龙.线性自抗扰控制鲁棒稳定性分析[J].控制理论与应用,2016,33(5):662668.
CHEN S S, HE Y Z, LIU H L. On robust stability of linear active disturbance rejection control system[J].Control Theory & Applications,2016,33(5):662668.
[8]韩京清,袁露林.跟踪微分器的离散形式[J].系统科学与数学,1999,19(3):268273. |