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排序方式: 共有110条查询结果,搜索用时 62 毫秒
61.
通过对舰船时统设备电磁兼容测试中出现的传导发射和辐射发射超标问题的对策分析,寻找超标原因,并提出有效的解决方案,探讨了设备在元器件选用和生产工艺上如何采取有效措施解决传导发射和辐射发射超标,使产品的EMC满足限值要求。 相似文献
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基于模糊推理的区域路网交通状态分析方法 总被引:2,自引:0,他引:2
为准确判别区域路网的交通状态,对区域路网交通流的宏观特性进行了详细分析,建立了路网交通状态评估指标体系。结合区域路网的拓扑结构与交通流特征,基于模糊推理技术提出了路网交通状态分析方法。以城市主干道路网为例,验证了路网交通状态分析方法的有效性。该方法可应用于在线交通状态分析和历史数据库交通运行特征的提取,为交通管理决策提供基础信息。 相似文献
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由于驾驶行为的不确定性,难以建立精确的车辆跟驰模型。针对这一问题,应用自适应模糊神经推理系统(ANFIS)建立跟驰模型,以跟随车与前车速度差及行车间距为输入量、跟随车的加速度为输出量,建立25条模糊推理规则,将模糊推理规则产生的数据作为车辆跟驰ANFIS模型的训练数据,并利用MATLAB编程对其进行训练。最后,设计了基于车载高精度GPS的跟驰试验,并结合试验数据分别对自适应模糊神经推理系统跟驰模型和传统跟驰模型进行仿真。结果表明,前者输出的跟驰车辆加速度值更接近于真实值。 相似文献
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Bayesian committee of neural networks to predict travel times with confidence intervals 总被引:1,自引:0,他引:1
C.P.IJ. van Hinsbergen J.W.C. van Lint H.J. van Zuylen 《Transportation Research Part C: Emerging Technologies》2009,17(5):498-509
Short-term prediction of travel time is one of the central topics in current transportation research and practice. Among the more successful travel time prediction approaches are neural networks and combined prediction models (a ‘committee’). However, both approaches have disadvantages. Usually many candidate neural networks are trained and the best performing one is selected. However, it is difficult and arbitrary to select the optimal network. In committee approaches a principled and mathematically sound framework to combine travel time predictions is lacking. This paper overcomes the drawbacks of both approaches by combining neural networks in a committee using Bayesian inference theory. An ‘evidence’ factor can be calculated for each model, which can be used as a stopping criterion during training, and as a tool to select and combine different neural networks. Along with higher prediction accuracy, this approach allows for accurate estimation of confidence intervals for the predictions. When comparing the committee predictions to single neural network predictions on the A12 motorway in the Netherlands it is concluded that the approach indeed leads to improved travel time prediction accuracy. 相似文献
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Aircraft mass is a crucial piece of information for studies on aircraft performance, trajectory prediction, and many other topics of aircraft traffic management. However, It is a common challenge for researchers, as well as air traffic control, to access this proprietary information. Previously, several studies have proposed methods to estimate aircraft weight based on specific parts of the flight. Due to inaccurate input data or biased assumptions, this often leads to less confident or inaccurate estimations. In this paper, combined with a fuel-flow model, different aircraft initial masses are computed independently using the total energy model and reference model at first. It then adopts a Bayesian approach that uses a prior probability of aircraft mass based on empirical knowledge and computed aircraft initial masses to produce the maximum a posteriori estimation. Variation in results caused by dependent factors such as prior, thrust and wind are also studied. The method is validated using 50 test flights of a Cessna Citation II aircraft, for which measurements of the true mass were available. The validation results show a mean absolute error of 4.3% of the actual aircraft mass. 相似文献