文献类型：期刊文献

英文题名：Co-simulation research of autonomous landing control system

作者：Wang, Zhaoning[1]; Wu, Shengxi[1]; Dun, Xiangming[2]; Gu, Xingsheng[1]

机构：[1] Key Laboratory of Advanced Control and Optimization for Chemical Processes, Ministry of Education, East China University of Science and Technology, Shanghai, 200237, China; [2] Research Institute of Robotics, Shanghai Jiao Tong University, Shanghai, 200240, China

年份：2014

起止页码：6352

外文期刊名：Proceedings of the 33rd Chinese Control Conference, CCC 2014

收录：EI(收录号：20144300119260)

语种：英文

外文关键词：Control systems - Launch vehicles - MATLAB - Process control - Reusable rockets - Vibrations (mechanical)

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. ? 2014 TCCT, CAA.