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151.
航空发动机滑油中舍有摩擦副产生的磨损微粒。通过滑油介质中所含磨损微粒中元素的分析.运用Dempster-Shafer证据融合诊断方法,对航空发动机的磨损状态等进行有效的诊断,确定发动机的磨损程度,以及发动机的磨损部位,从而可对发动机的故障排除作参考。在融合过程中提出了先对每个元素的磨损量和磨损率进行融合,再总体融合的方法。针对Dempster—Sharer证据融合的局限,应用了两种改进的融合方法,并进行比较。实例表明,Dempster—Shafer证据融合是一种有效的航空发动机滑油磨损的故障诊断方法。 相似文献
152.
通过分析目前大多数内地高职院校商务英语实训的模式及其存在的问题,以外贸函电为例,阐明基于网络的商务英语实训模式的可行性和操作方法。表明应用语言类专业学生的综合能力需要通过实训来提高,但由于实训过程的特殊性,我国内地高职院校很难找到真正"工学结合"的实训机会。为了促进企业和学校的合作,应把这类实训活动作为长期活动,为合作的企业提供长期的服务,从而真正实现"工学结合"的目的。 相似文献
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《中国航空学报》2020,33(3):1006-1015
When non-cooperative body attachment occurs in space, the inertia of the new combination and the change of the system’s momentum are unknown. This uncertainty may lead to the instability of the spacecraft’s attitude control. In order to solve this problem, we propose an adaptive control scheme based on the inertia estimation of the new, combined system of non-cooperative body and satellite. This method can allow the new combination of different situations to reach a stable state with a high level of precision and speed. In this paper, the stability of the adaptive control scheme is proven by constructing a Lyapunov function. A simulation environment in which a non-cooperative body attaches to a satellite attaches to is constructed. The simulation shows that the attitude error converges to a small field when using the control scheme, regardless of unfavorable cases, including unknown inertia parameters, added momentum. In addition, the simulation results show the strong robustness of the control scheme for the new combination. 相似文献
156.
Tamara Bandikova Jakob Flury 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2014
The new release of the sensor and instrument data (Level-1B release 02) of the Gravity Recovery and Climate Experiment (GRACE) had a substantial impact on the improvement of the overall accuracy of the gravity field models. This has implied that improvements on the sensor data level can still significantly contribute to arriving closer to the GRACE baseline accuracy. The recent analysis of the GRACE star camera data (SCA1B RL02) revealed their unexpectedly higher noise. As the star camera (SCA) data are essential for the processing of the K-band ranging data and the accelerometer data, thorough investigation of the data set was needed. We fully reexamined the SCA data processing from Level-1A to Level-1B with focus on the combination method of the data delivered by the two SCA heads. In the first step, we produced and compared our own combined attitude solution by applying two different combination methods on the SCA Level-1A data. The first method introduces the information about the anisotropic accuracy of the star camera measurement in terms of a weighing matrix. This method was applied in the official processing as well. The alternative method merges only the well determined SCA boresight directions. This method was implemented on the GRACE SCA data for the first time. Both methods were expected to provide optimal solution characteristic by the full accuracy about all three axes, which was confirmed. In the second step, we analyzed the differences between the official SCA1B RL02 data generated by the Jet Propulsion Laboratory (JPL) and our solution. SCA1B RL02 contains systematically higher noise of about a factor 3–4. The data analysis revealed that the reason is the incorrect implementation of algorithms in the JPL processing routines. After correct implementation of the combination method, significant improvement within the whole spectrum was achieved. Based on these results, the official reprocessing of the SCA data is suggested, as the SCA attitude data are one of the key observations needed for the gravity field recovery. 相似文献
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对于有限可重组合问题 ,通常用母函数方法[1] 作解答 ,但当数据比较大时 ,母函数方法就不太方便。更重要的是 ,母函数方法很难在计算机中实现。本文对几种有限可重组合问题给出了公式型解法 相似文献
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本模型意在寻求净收益R尽可能大而风险ε尽可能小的一种投资组合,先介绍了在期望风险为一定值时单纯形法求解净收益最大的投资组合的全过程。 相似文献