Simulation of Time-Delay Based Path-Tracking Control of Reusable Launch Vehicle

被引:1
作者
Cho, Woosung [1 ]
Lee, HyeongJin [1 ]
Lee, Yeol [1 ]
Ko, Sangho [1 ]
机构
[1] Korea Aerosp Univ, Sch Aerosp & Mech Engn, Goyang, South Korea
关键词
Reusable Launch Vehicle; Time-delay Control; Nonlinear Path-following Guidance Method; Re-entry;
D O I
10.5139/JKSAS.2021.49.8.627
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This paper deals with a study for the guidance control of reusable launch vehicle. For this purpose, modeling of the equation of motion of a reusable launch vehicle with 6 degrees of freedom was performed. With this model, an optimal re-entry path was created and a path-following guidance control simulation was performed to follow the optimal re-entry path. For the design of the path-following guidance controller, the attitude controller applying a time-delay technique that is resistant to modeling uncertainty, disturbance and failure. And the nonlinear path-following guidance law were used. Guidance control simulation using a classical PD controller was performed and compared with the guidance control simulation of a reusable launch vehicle applying a time delay technique.
引用
收藏
页码:627 / 636
页数:10
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