Co-simulation Research of Autonomous Landing Control System

被引:0
|
作者
Wang Zhaoning [1 ]
Wu Shengxi [1 ]
Dun Xiangming [2 ]
Gu Xingsheng [1 ]
机构
[1] E China Univ Sci & Technol, Minist Educ, Key Lab Adv Control & Optimizat Chem Proc, Shanghai 200237, Peoples R China
[2] Shanghai Jiao Tong Univ, Res Inst Robot, Shanghai 200240, Peoples R China
关键词
vertical take-off and landing; autonomous landing; reusable launch vehicle; control system; co-simulation research;
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 control simulation of the autonomous landing process of a Vertical Take-Off and Landing (VTVL) Reusable Launch Vehicle (RLV) is proposed and we consider the effects of the inner liquid propellant sloshing, elastic vibration, disturbance force, disturbance torque and other complex conditions in the virtual RLV model. On the basis of dynamics modeling of the RLV, we analyzed RLV's landing process. The landing control system was designed under certain conditions. Co-simulation Research was achieved by ADAMS and MATLAB/Simulink. The simulation results show that the control system performs well.
引用
收藏
页码:6352 / 6357
页数:6
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