摘要
为提高火箭发射中燃料加注系统的可靠性和安全性,设计了一种用于火箭推进剂加注时自动对接和脱离的机器人本体结构.应用ADAMS对其进行了运动学和动力学仿真分析,得到了在给定输入下加泄连接器的仿真输出曲线.通过分析验证了机构设计的合理性和实用性.
To improve reliability and security of the fueling system in rocket launch, an auto-docking and auto-separating mechanism is designed for the rocket fuel loading. The ADAMS is used to carry out the kinematics and dynamics simulations, getting the connector simulation output curves from the given input ones. The reasonableness and practicality of the designed mechanism are verified by analysis.
出处
《机器人》
EI
CSCD
北大核心
2010年第2期145-149,共5页
Robot
基金
国家863计划资助项目(2007AA04Z249)
