Co-simulation Research of Autonomous Landing Control System

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 RLVs 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.

关键词： vertical take-off and landing autonomous landing reusable launch vehicle control system co-simulation research

作者: WANG Zhaoning WU Shengxi DUN Xiangming GU Xingsheng

作者单位: Key Laboratory of Advanced Control and Optimization for Chemical Processes,Ministry of Education,Eas Research Institute of Robotics,Shanghai Jiao Tong University,Shanghai 200240,China

会议类型: 国际会议

会议名称: The 33th Chinese Control Conference第33届中国控制会议

会议地点: 南京

会议语种:英文

页码: 6352-6357

在线出版日期: 2014-07-28（万方平台首次上网日期，不代表论文的发表时间）