基于ADAMS与AMESim的飞行器发射动力学仿真  

Simulation of Launch Dynamics of Aircraft Based on ADAMS and AMESim

作　　者：赵君伟[1] 张家骏[1] 张程[1] 司世才 裘群海 ZHAO Junwei;ZHANG Jiajun;ZHANG Cheng;SI Shicai;QIU Qunhai(China Academy of Launch Vehicle Technology,Beijing 100076,China)

机构地区：[1]中国运载火箭技术研究院,北京100076

出　　处：《弹箭与制导学报》2021年第5期46-52,共7页Journal of Projectiles,Rockets,Missiles and Guidance

摘　　要：基于ADAMS与AMESim联合仿真技术,通过在ADAMS软件中建立发射车和飞行器多体动力学模型,在AMESim中建立发射车液压子系统模型,采用联合仿真方式,对某型飞行器发射出箱过程进行了动态仿真分析。经分析确认,飞行器发射出箱后,姿态角及角速度均正常,满足姿态控制系统起控条件。Based on the joint simulation technology of ADAMS and AMESim,this paper establishes the launch vehicle and aircraft multi-body dynamics model in ADAMS software,establishes the launch vehicle hydraulic subsystem model in AMESim,and adopts joint simulation to carry out the dynamic simulation analysis of the launch process of a certain aircraft.After analysis,it is confirmed that the attitude angle and angular velocity of the aircraft are normal after the vehicle is launched out of the box,which meets the control conditions of the attitude control system.

关 键 词：联合仿真 飞行器 发射 动力学 

分 类 号：TB24[一般工业技术—工程设计测绘]