基于AMESim和ADAMS联合仿真的发射平台起竖控制方法研究  

Research on the Erecting Control Method with Launcher Joint Simulation by AMESim and ADAMS

作　　者：杨之江[1] 吴林瑞[1] 吴齐才[1] 李德忠[1] 

机构地区：[1]北京航天发射技术研究所,北京100076

出　　处：《导弹与航天运载技术》2016年第2期36-38,46,共4页Missiles and Space Vehicles

摘　　要：建立发射平台起竖系统机械动力学ADAMS模型,液压AMESim模型,控制系统MATLAB/Simulink模型,实现发射平台起竖系统的多平台联合仿真,在此基础上对起竖过程控制方法进行分析研究,得到多级油缸基于角速度闭环控制方法的起竖控制模型。The mechanical system model on ADAMS, the hydraulic system model on AMESim and the control system model on MATLAB/Simulink of the launcher erecting system are established. Then the joint simulation is completed. The erecting control methods is researched based on the joint simulation. The angular velocity closed loop control system model of multi-stage cylinder is obtained.

关 键 词：发射平台起竖系统 联合仿真 ADAMS AMESIM MATLAB 

分 类 号：V554.2[航空宇航科学与技术—人机与环境工程]