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无人机动力系统测试装置设计和研究
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作者 夏源隆 韩伟 +3 位作者 任帅阳 孔令豪 张锋伟 何强 《机械设计》 北大核心 2025年第7期115-121,共7页
为了弥补小型无人机动力系统测试装置相关研究的不足,文中围绕可调节旋翼摆放角度的无人机动力系统测试装置进行研究和设计。为满足实际应用需求,提出一种2自由度的无人机动力系统测试装置设计方案,包括设备台架和数据采集系统,模拟无... 为了弥补小型无人机动力系统测试装置相关研究的不足,文中围绕可调节旋翼摆放角度的无人机动力系统测试装置进行研究和设计。为满足实际应用需求,提出一种2自由度的无人机动力系统测试装置设计方案,包括设备台架和数据采集系统,模拟无人机飞行动作并进行动力系统测试。试验结果表明:转速最大相对误差约为0.658%,测量精度较高,该无人机动力系统测试装置的设备台架结构合理,数据采集系统具有较高的稳定性和可靠性,满足工程实际应用需求。 展开更多
关键词 无人机 动力系统测试 装置设计 有限元分析 数据采集
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Modeling approaches to pressure balance dynamic system in shield tunneling 被引量:2
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作者 李守巨 于申 屈福政 《Journal of Central South University》 SCIE EI CAS 2014年第3期1206-1216,共11页
In order to deal with modeling problem of a pressure balance system with time-delay, nonlinear, time-varying and uncertain characteristics, an intelligent modeling procedure is proposed, which is based on artificial n... In order to deal with modeling problem of a pressure balance system with time-delay, nonlinear, time-varying and uncertain characteristics, an intelligent modeling procedure is proposed, which is based on artificial neural network(ANN) and input-output data of the system during shield tunneling and can overcome the precision problem in mechanistic modeling(MM) approach. The computational results show that the training algorithm with Gauss-Newton optimization has fast convergent speed. The experimental investigation indicates that, compared with mechanistic modeling approach, intelligent modeling procedure can obviously increase the precision in both soil pressure fitting and forecasting period. The effectiveness and accuracy of proposed intelligent modeling procedure are verified in laboratory tests. 展开更多
关键词 intelligent modeling neural network pressure balance system excavation chamber analytically modeling approach
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