Re-entry Simulation for Reusable Launch Vehicle

被引：0
|
作者：
Xu Zhi
Tang Shuo
机构：
来源：
ICMS2010: PROCEEDINGS OF THE THIRD INTERNATIONAL CONFERENCE ON MODELLING AND SIMULATION, VOL 2: MODELLING AND SIMULATION IN ENGINEERING | 2010年
关键词：
reusable launch vehicle; re-entry; feedback linearization; model predictive control;
D O I：
暂无
中图分类号：
TP39 [计算机的应用];
学科分类号：
081203 ; 0835 ;
摘要：
In this paper the RLV flight control system is designed by combining MPC with Feedback Linearization (FBL). The feedback linearization is based on the full rotational equations of motion rather than on a conventional model derived from time-scale separation. Input state constraints and are applied to MPC algorithms to avoid input saturations, to guarantee a smooth tracking performance with non-linear rotational dynamics and a strong roll-yaw coupling of RLV model. The results of simulation show the control system can follow the parameters of guidance significantly.
引用
收藏
页码：155 / 159
页数：5
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