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661.
Application of hybrid regularization method for tomographic reconstruction of midlatitude ionospheric electron density 总被引:1,自引:0,他引:1
Yibin Yao Jun Tang Jian Kong Liang Zhang Shun Zhang 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2013
Reconstructing ionospheric electron density (IED) is an ill-posed inverse problem, with classical Tikhonov regularization tending to smooth IED structures. By contrast, total variation (TV) regularization effectively resists noise and preserves discontinuities of the IED. In this paper, we regularize the inverse problem by incorporating both Tikhonov and TV regularization. A specific formulation of the proposed method, called hybrid regularization, is introduced and investigated. The method is then tested using simulated data for the actual positions of the GPS satellites and ground receivers, and also applied to the analysis of real observation data under quiescent and disturbed ionospheric conditions. Experiments demonstrate the effectiveness, and illustrate the validity and reliability of the proposed method. 相似文献
662.
进行机翼故障情况下的飞行包线估算可为驾驶员正确操纵和包线保护控制提供必要的信息.考虑到飞机机翼故障的动力学特点,提出一种动态飞行包线估算方法.建立故障参数模型,应用最小二乘辨识算法进行气动参数辨识与故障诊断;基于参数辨识结果估算飞行包线;根据故障特点,分别对系统进行配平计算,在每个配平点建立飞行包线数据库,根据故障诊断结果实时调用包线库中的数据,形成当前时刻的飞行包线. 相似文献
663.
大厚度铝合金矩形机箱在拼焊生产过程中,存在组装难度大,焊缝质量不易保证,焊后变形大等问题.针对铝合金矩形机箱焊后马鞍型和螺旋型变形特点,选用表面定位方式,设计了多种类型的夹板,完成了箱体焊接工装的设计.在此基础上,采用真空电子束焊,通过严格的工艺措施完成了机箱的拼焊,获得了深宽比符合要求的焊缝,保证了机箱结构的完整性.经检测,矩形机箱满足设计要求.实践证明,此工装和工艺方案可行,对类似构件的制造有指导意义. 相似文献
664.
研究了双螺杆挤出机生产纤维增强热塑性塑料时,纤维股数、双螺杆转速、塑料喂料量与纤维含量的关系,通过调节此三个参数,纤维含量可精确控制在±0.1wt%的范围内.当主机螺杆转速和塑料喂料量,或纤维股数和塑料喂料量同时增加,挤出造粒产量将提高相同倍数,而纤维含量保持不变.本方法高效可行、精确可控,容易为操作者所掌握,特别适用于指导生产实践. 相似文献
665.
666.
Drilling load modeling and validation based on the filling rate of auger flute in planetary sampling 总被引:1,自引:0,他引:1
Some type of penetration into a subsurface is required in planetary sampling. Drilling and coring, due to its efficient penetrating and cuttings removal characteristics, has been widely applied in previous sampling missions. Given the complicated mechanical properties of a planetary regolith, suitable drilling parameters should be matched with different drilling formations properly. Otherwise, drilling faults caused by overloads could easily happen. Hence, it is necessary to estab-lish a drilling load model, which is able to reveal the relationships among drilling loads, an auger's structural parameters, soil's mechanical properties, and relevant drilling parameters. A concept for the filling rate of auger flute (FRAF) is proposed to describe drilling conditions. If the FRAF index under one group of drilling parameters is less than 1, this means that the auger flute currently removes cuttings smoothly. Otherwise, the auger will be choked with compressed cuttings. In dril-ling operations, the drilling loads on the auger mainly come from the conveyance action, while the drilling loads on the drill bit primarily come from the cutting action. Experiments in one typical lunar regolith simulant indicate that the estimated drilling loads based on the FRAF coincide with the test results quite well. Based on this drilling load model, drilling parameters have been opti-mized. 相似文献
667.
Lili Yan Jian Wang Xiaohua Hao Zhiguang Tang 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2014
Precise glacier information is important for assessing climate change in remote mountain areas. To obtain more accurate glacier mapping, rough set theory, which can deal with vague and uncertainty information, was introduced to obtain optimal knowledge rules for glacier mapping. Optical images, thermal infrared band data, texture information and morphometric parameters were combined to build a decision table used in our proposed rough set theory method. After discretizing the real value attributes, decision rules were calculated through the decision rule generation algorithm for glacier mapping. A decision classifier based on the generated rules classified the multispectral image into glacier and non-glacier areas. The result of maximum likelihood classification (MLC) was used to compare with the result of the classification based on the rough set theory. Confusion matrix and visual interpretation were used to evaluate the overall accuracy of the results of the two methods. The accuracies of the rough set method and maximum likelihood classification were compared, yielding overall accuracies of 94.15% and 93.88%, respectively. It showed the area difference based on rough set was smaller by comparing the glacier areas of the rough set method and MLC with visual interpreter, respectively. The high accuracy for glacier mapping and the small area difference for glacier based on rough set theory demonstrated that this method was effective and promising for glacier mapping. 相似文献
668.
669.
低速全模颤振试验悬挂支撑系统 总被引:1,自引:0,他引:1
为适应日益增多的低速风洞全模颤振试验的需要,发展颤振试验技术,在气动中心低速所3.2m 风洞建立了一套通用的悬挂支撑系统。该悬挂系统分为垂直和水平两部分,水平悬挂系统由水平钢索装置和张紧机构组成。系统可提供模型沉浮、俯仰、横侧向、偏航和滚转5个方向的自由度;可单独改变模型某一方向的自由度而不影响其它方向的自由度;可确保模型上下、左右、前后位置都处于试验段正中心;可方便地调整模型的迎角和滚转角。对采用该悬挂系统的颤振模型,文中提供了技术要求和参数选择方法。采用同一颤振模型在3.2m 风洞与TsAGI的T-103风洞进行了对比试验,得到的颤振临界速度、频率基本一致,证明该套悬挂系统设计合理,可以应用于低速全模颤振试验。 相似文献
670.
汤小平 《民用飞机设计与研究》2014,(1):6-10
就基本的管理规律和参数而言,所有航空产品的研制基本一致,但因为市场和客户的不同,民用航空产品研制在体系建设和技术覆盖面方面有自己的特点,尤其是适航规章要求和客户使用环境不同,使得民用航空产品的研制必须要更多地把产品全寿命周期的技术成功和运行支持纳入早期的研制活动,这必然带来在研制体系和技术能力建设方面的差异化,而早日识别和把握这些差别是民用航空产品产业健康发展的必须。 相似文献