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基于ADAMS与AMESim的飞行器发射动力学仿真

ZHAO Junwei,ZHANG Jiajun,ZHANG Cheng,SI Shicai,QIU Qunhai

Journal of Projectiles, Rockets, Missiles and Guidance（2021）

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Abstract
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.
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