Modelling hinting strategies for geometry theorem proving
数据挖掘与数据分析,数据可视化试题

数据挖掘与数据分析,数据可视化试题1. Data Mining is also referred to as ……………………..data analysisdata discovery(正确答案)data recoveryData visualization2. Data Mining is a method and technique inclusive of …………………………. data analysis.(正确答案)data discoveryData visualizationdata recovery3. In which step of Data Science consume Almost 80% of the work period of the procedure.Accumulating the dataAnalyzing the dataWrangling the data(正确答案)Recapitulation of the Data4. Which Step of Data Science allows the model to consistently improve and provide punctual performance and deliverapproximate results.Wrangling the dataAccumulating the dataRecapitulation of the Data(正确答案)Analyzing the data5. Which tool of Data Science is robust machine learning library, which allows the implementation of deep learning ?algorithms. STableauD3.jsApache SparkTensorFlow(正确答案)6. What is the main aim of Data Mining ?to obtain data from a less number of sources and to transform it into a more useful version of itself.to obtain data from a less number of sources and to transform it into a less useful version of itself.to obtain data from a great number of sources and to transform it into a less useful version of itself.to obtain data from a great number of sources and to transform it into a more useful version of itself.(正确答案)7. In which step of data mining the irrelevant patterns are eliminated to avoid cluttering ? Cleaning the data(正确答案)Evaluating the dataConversion of the dataIntegration of data8. Data Science t is mainly used for ………………. purposes. Data mining is mainly used for ……………………. purposes.scientific,business(正确答案)business,scientificscientific,scientificNone9. Pandas ………………... is a one dimensional labeled array capable of holding data of any type (integer, string, float, python objects, etc.).Series(正确答案)FramePanelNone10. How many principal components Pandas DataFrame consists of ?4213(正确答案)11. Important data structure of pandas is/are ___________SeriesData FrameBoth(正确答案)None of the above12. Which of the following command is used to install pandas?pip install pandas(正确答案)install pandaspip pandasNone of the above13. Which of the following function/method help to create Series? series()Series()(正确答案)createSeries()None of the above14. NumPY stands for?Numbering PythonNumber In PythonNumerical Python(正确答案)None Of the above15. Which of the following is not correct sub-packages of SciPy? scipy.integratescipy.source(正确答案)scipy.interpolatescipy.signal16. How to import Constants Package in SciPy?import scipy.constantsfrom scipy.constants(正确答案)import scipy.constants.packagefrom scipy.constants.package17. ………………….. involveslooking at and describing the data set from different angles and then summarizing it ?Data FrameData VisualizationEDA(正确答案)All of the above18. what involves the preparation of data sets for analysis by removing irregularities in the data so that these irregularities do not affect further steps in the process of data analysis and machine learning model building ?Data AnalysisEDA(正确答案)Data FrameNone of the above19. What is not Utility of EDA ?Maximize the insight in the data setDetect outliers and anomaliesVisualization of dataTest underlying assumptions(正确答案)20. what can hamper the further steps in the machine learning model building process If not performed properly ?Recapitulation of the DataAccumulating the dataEDA(正确答案)None of the above21. Which plot for EDA to check the dependency between two variables ? HistogramsScatter plots(正确答案)MapsTime series plots22. What function will tell you the top records in the data set?shapehead(正确答案)showall of the aboce23. what type of data is useful for internal policymaking and business strategy building for an organization ?public dataprivate data(正确答案)bothNone of the above24. The ………… function can “fill in” NA valueswith non-null data ?headfillna(正确答案)shapeall of the above25. If you want to simply exclude the missing values, then what function along with the axis argument will be use?fillnareplacedropna(正确答案)isnull26. Which of the following attribute of DataFrame is used to display data type of each column in DataFrame?DtypesDTypesdtypes(正确答案)datatypes27. Which of the following function is used to load the data from the CSV file into a DataFrame?read.csv()readcsv()read_csv()(正确答案)Read_csv()28. how to Display first row of dataframe ‘DF’ ?print(DF.head(1))print(DF[0 : 1])print(DF.iloc[0 : 1])All of the above(正确答案)29. Spread function is known as ................ in spreadsheets ?pivotunpivot(正确答案)castorder30. ................. extract a subset of rows from a data fram based on logical conditions ? renamefilter(正确答案)setsubset31. We can shift the DataFrame’s index by a certain number of periods usingthe …………. Method ?melt()merge()tail()shift()(正确答案)32. We can join melted DataFrames into one Analytical Base Table using the ……….. function.join()append()merge()(正确答案)truncate()33. What methos is used to concatenate datasets along an axis ?concatenate()concat()(正确答案)add()merge()34. Rows can be …………….. if the number of missing values is insignificant, as thiswould not impact the overall analysis results.deleted(正确答案)updatedaddedall35. There is a specific reason behind the missing value.What stands for Missing not at randomMCARMARMNAR(正确答案)None of the above36. While plotting data, some values of one variable may not lie beyond the expectedrange, but when you plot the data with some other variable, these values may lie far from the expected value.Identify the type of outliers?Univariate outliersMultivariate outliers(正确答案)ManyVariate outlinersNone of the above37. if numeric values are stored as strings, then it would not be possible to calculatemetrics such as mean, median, etc.Then what type of data cleaning exercises you will perform ?Convert incorrect data types:(正确答案)Correct the values that lie beyond the rangeCorrect the values not belonging in the listFix incorrect structure:38. Rows that are not required in the analysis. E.g ifobservations before or after a particular date only are required for analysis.What steps we will do when perform data filering ?Deduplicate Data/Remove duplicateddataFilter rows tokeep only therelevant data.(正确答案)Filter columns Pick columnsrelevant toanalysisBring the datatogether, Groupby required keys,aggregate therest39. you need to…………... the data in order to get what you need for your analysis. searchlengthorderfilter(正确答案)40. Write the output of the following ?>>> import pandas as pd >>> series1 =pd.Series([10,20,30])>>> print(series1)0 101 202 30dtype: int64(正确答案)102030dtype: int640 1 2 dtype: int64None of the above41. What will be output for the following code?import numpy as np a = np.array([1, 2, 3], dtype = complex) print a[[ 1.+0.j, 2.+0.j, 3.+0.j]][ 1.+0.j]Error[ 1.+0.j, 2.+0.j, 3.+0.j](正确答案)42. What will be output for the following code?import numpy as np a =np.array([1,2,3]) print a[[1, 2, 3]][1][1, 2, 3](正确答案)Error43. What will be output for the following code?import numpy as np dt = dt =np.dtype('i4') print dtint32(正确答案)int64int128int1644. What will be output for the following code?import numpy as np dt =np.dtype([('age',np.int8)]) a = np.array([(10,),(20,),(30,)], dtype = dt)print a['age'][[10 20 30]][10 20 30](正确答案)[10]Error45. We can add a new row to a DataFrame using the _____________ methodrloc[ ]iloc[ ]loc[ ](正确答案)None of the above46. Function _____ can be used to drop missing values.fillna()isnull()dropna()(正确答案)delna()47. The function to perform pivoting with dataframes having duplicate values is _____ ? pivot(unique = True)pivot()pivot_table(unique = True)pivot_table()(正确答案)48. A technique, which when performed on a dataframe, rearranges the data from rows and columns in a report form, is called _____ ?summarisingreportinggroupingpivoting(正确答案)49. Normal Distribution is symmetric is about ___________ ?VarianceMean(正确答案)Standard deviationCovariance50. Write a statement to display “Amount” as x-axis label. (consider plt as an alias name of matplotlib.pyplot)bel(“Amount”)plt.xlabel(“Amount”)(正确答案)plt.xlabel(Amount)None of the above51. Fill in the blank in the given code, if we want to plot a line chart for values of list ‘a’ vs values of list ‘b’.a = [1, 2, 3, 4, 5]b = [10, 20, 30, 40, 50]import matplotlib.pyplot as pltplt.plot __________(a, b)(正确答案)(b, a)[a, b]None of the above52. #Loading the datasetimport seaborn as snstips =sns.load_dataset("tips")tips.head()In this code what is tips ?plotdataset name(正确答案)paletteNone of the above53. Visualization can make sense of information by helping to find relationships in the data and support (or disproving) ideas about the dataAnalyzeRelationShip(正确答案)AccessiblePrecise54. In which option provides A detailed data analysis tool that has an easy-to-use tool interface and graphical designoptions for visuals.Jupyter NotebookSisenseTableau DesktopMATLAB(正确答案)55. Consider a bank having thousands of ATMs across China. In every transaction, Many variables are recorded.Which among the following are not fact variables.Transaction charge amountWithdrawal amountAccount balance after withdrawalATM ID(正确答案)56. Which module of matplotlib library is required for plotting of graph?plotmatplotpyplot(正确答案)None of the above57. Write a statement to display “Amount” as x-axis label. (consider plt as an alias name of matplotlib.pyplot)bel(“Amount”)plt.xlabel(“Amount”)(正确答案)plt.xlabel(Amount)None of the above58. What will happen when you pass ‘h’ as as a value to orient parameter of the barplot function?It will make the orientation vertical.It will make the orientation horizontal.(正确答案)It will make line graphNone of the above59. what is the name of the function to display Parameters available are viewed .set_style()axes_style()(正确答案)despine()show_style()60. In stacked barplot, subgroups are displayed as bars on top of each other. How many parameters barplot() functionhave to draw stacked bars?OneTwoNone(正确答案)three61. In Line Chart or Line Plot which parameter is an object determining how to draw the markers for differentlevels of the style variable.?x.yhuemarkers(正确答案)legend62. …………………..similar to Box Plot but with a rotated plot on each side, giving more information about the density estimate on the y axis.Pie ChartLine ChartViolin Chart(正确答案)None63. By default plot() function plots a ________________HistogramBar graphLine chart(正确答案)Pie chart64. ____________ are column-charts, where each column represents a range of values, and the height of a column corresponds to how many values are in that range.Bar graphHistograms(正确答案)Line chartpie chart65. The ________ project builds on top of pandas and matplotlib to provide easy plotting of data.yhatSeaborn(正确答案)VincentPychart66. A palette means a ________.. surface on which a painter arranges and mixed paints. circlerectangularflat(正确答案)all67. The default theme of the plotwill be ________?Darkgrid(正确答案)WhitegridDarkTicks68. Outliers should be treated after investigating data and drawing insights from a dataset.在调查数据并从数据集中得出见解后,应对异常值进行处理。
基于RF-NSGA-Ⅱ的建筑能耗多目标优化

第38卷第2期2021年4月Vol.38No.2Apr.2021土木工程与管理学报Journal of Civil Engineering and Management基于RF-NSGA-II的建筑能耗多目标优化吴贤国1,杨赛1,王成龙2,王洪涛2,陈虹宇3,朱海军2,王雷1(1.华中科技大学土木与水利工程学院,湖北武汉430074;2.中建三局集团有限公司,湖北武汉430064;3.南洋理工大学土木工程与环境学院,新加坡639798)摘要:本文提出一种随机森林-带精英策略的非支配排序遗传算法(RF-NSGA-II)相结合的方法,基于建筑外围护结构设计优选进行建筑能耗多目标优化。
首先通过建立BIM模型导入DesignBuilder软件,利用正交试验获取建筑外维护结构主要参数与对应能耗的模拟样本集,再将样本数据集用于RF模型预测中进行训练,将训练好的RF回归函数作为适应度函数并作为优化目标之一。
在此基础上引入室内热舒适度函数为另一个适应度函数,采用NSGA-II进行多目标优化,得到Pareto前沿解集并从中利用理想点法得到一组多目标最优解。
通过本研究可以得出:利用RF对建筑能耗进行预测精度高,所得预测效果好,通过NSGA-II算法和理想点法可以获得满足建筑能耗和舒适度要求的外围护设计参数最优取值,结果与实际相符,效果良好。
对实现低建筑能耗和高热舒适度优化具有参考价值。
关键词:建筑能耗模拟;围护结构;随机森林;遗传算法;热舒适度;多目标优化中图分类号:TU201.5文献标识码:A文章编号:2095-0985(2021)02-0001-08Multi-objective Optimization of Building Energy Consumption Based on RF-NSGA-II WU Xianguo1,YANG Sai1,WANG Chenglong2,WANG Hongtao2,CHEN Hongyu3,ZHU Haijun2,WANG Lei(1.School of Civil and Hydraulic Engineering,Huazhong University of Science and Technology,Wuhan430074,China; 2.China Construction Third Engineering Bureau Group Co Ltd, Wuhan430064,China; 3.School of Civil and Environmental Engineering,Nanyang Technological University,Singapore639798,Singapore)Abstract:This paper proposes a combination method of random forest and non-dominated sorting genetic algorithm with elite strategy(RF-NSGA-II),which is based on the optimization of building envelope structure design for multi-objective optimization of building energy consumption.Firstly,by establishing a BIM model and importing it into DesignBuilder software,we use orthogonal experiments to obtain a simulation sample set of the main parameters of the maintenance structure outside the building and the corresponding energy consumption.And then we use the sample data set in the RF model prediction for training and take the trained RF regression function as a fitness function and one of the optimization goals.On this basis,the indoor thermal comfort function is introduced as another fitness function,and NSGA-II is used for multi-objective optimization,and the Pareto frontier solution set is obtained,and a set of multi-objective optimal solutions are obtained by using the ideal point method.Through this research,it can be concluded that the prediction accuracy of building energy consumption by RF is used,and the obtained prediction effect is good.The optimal envelope design parameters can be obtained to meet the requirements of building energy consumption and comfort through NS-GA-II algorithm and ideal point method.The result is consistent with the actual value and the effect is good.It has reference value to realize the optimization of low building energy consumption and high收稿日期:2020-10-05修回日期:2020-12-09作者简介:吴贤国(1964—),女,湖北武汉人,博士,教授,研究方向为土木工程施工及管理(Email:wxg0220@)通讯作者:王成龙(1990—),男,湖北武汉人,工程师,研究方向为土木工程施工及管理(Email:*****************)基金项目:国家重点研发计划(2016YFC0800208);国家自然科学基金(51378235;71571078;51308240)・2・土木工程与管理学报2021年thermal comfort.Key words:building energy consumption simulation;envelope structure;random forest;genetic algorithm;thermal comfort;multi-objective optimization能源消耗一直是世界各国备受关注的问题,其中建筑能耗问题同样需要引起重视。
基于非定常分数阶的岩石时效性蠕变模型

采矿与安全匸程学报Journal of Mining & Safety Engineering 笫38卷笫2期2021年03月Vol.38 No.2Mar. 2021文章编号:1673-3363-(2021 )02-0388-08基于非定常分数阶的岩石时效性蠕变模型刘文博巳张树光",陈雷2(1.广西岩土力学与工程重点实验室,广西桂林541004; 2.辽宁工程技术大学土木工程学院*辽宁 阜新123000: 3.桂林理工人学上木打建筑工程学院,广西桂林541004)摘要 为了研究砂岩在不同围压作用下的蠕变特性,采用MTS 815.02试验机对砂岩进行三轴蠕变试验,进而分析了砂岩在不同围压作用下的蠕变变形规律。
将黏壶黏滞系数非定常化来构建非定常Abel 黏壶,在此基础上对分数阶阶数进行非定常化,进而建立一种基于非定常分数阶的砂岩时效性蠕变本构模型,使得该模型可以更好地描述岩石的加速蠕变变形规律;通过Levenberg-Marquardt 算法对三轴蠕变模型参数进行识别,来验证构建蠕变模型的正确性。
结果表明:在时间和应力双重作用影响下,将分数阶阶数),当做是一个关于应力和时间的函数,构建的非定常分 数阶砂岩三维时效性蠕变本构模型可以很好地描述岩石的加速蠕变变形规律;模型曲线和试验曲 线拟合均在0.95以上,侧面证明了将分数阶阶数非定常化是可行的。
同时,采用单轴蠕变曲线和蠕变模型曲线进行对比,得出试验数据与一维时效性蠕变模型的吻合度也较高,这进一步说明了采用非定常化分数阶阶数建立的一维时效性蠕变模型是可靠的。
关键词分数阶;非定常化;时效性蠕变本构模型;加速蠕变;参数识别中图分类号 TD32 文献标志码 A DOI 10.13545/ki.jmse.2019.0563Time-dependent creep model of rock based onunsteady fractional orderLIU Wenbo 1'2, ZHANG Shuguang 1'3, CHEN Lei 2(1. Guangxi Key Laboratory of Geomechanics and Geotechnical Engineering* Guilin, Guangxi 541004» China ;2. School of Civil Engi n eering a n d Transportation, Liaoning Technical University, Fuxin, Liaoning 123000, China ;3. School of Civil Engineering, Guilin U Diversity of Tech n ology, Guilin, Guangxi 541004, China )Abstract In order to study creep characteristics of sandst o ne un d er different con f ining pressure,triaxial creep test on sandstone was carried out with the testing machine of MTS 815.02, and the creepdefonnation of sandstone under different con f ining pressures was analyzed. An unsteady Abel clay potwas constructed with unsteady viscosity coefficient, based on which the fractional order was sorted interms of unsteady, and a time-dependent creep constitutive model based on unsteady fractionalsandstone was established for better description of accelerated creep deformation law. Finally,parameters of the triaxial creep model was identified with Levenberg ・Ma 「quanit algorithm to verify thecorrectness of the creep model. The results have shown that under dual influence of time and stress, withfractional order y regarded as a flmction of stress and time, the three-dimensional time-dependent creepconstitutive model of unsteady fractional sandstones constructed well describes the law of accelerated收稿日期:2020-11-23 责任编辑:宋爽基金项目:国家自然科学基金项11(51274109)作者简介:刘文博(1990—),男,甘肃省兰州市人,博士,从事地卜匸程与岩看本构模世方面的研究。
英语

The Neutral Grounding Resistor Sizing Using an Analytical Method Based on Nonlinear Transformer Model for Inrush Current MitigationGholamabas M.H.Hajivar Shahid Chamran University,Ahvaz, Iranhajivar@S.S.MortazaviShahid Chamran University,Ahvaz, IranMortazavi_s@scu.ac.irMohsen SanieiShahid Chamran University,Ahvaz, IranMohsen.saniei@Abstract-It was found that a neutral resistor together with 'simultaneous' switching didn't have any effect on either the magnitudes or the time constant of inrush currents. The pre-insertion resistors were recommended as the most effective means of controlling inrush currents. Through simulations, it was found that the neutral resistor had little effect on reducing the inrush current peak or even the rate of decay as compared to the cases without a neutral resistor. The use of neutral impedances was concluded to be ineffective compared to the use of pre-insertion resistors. This finding was explained by the low neutral current value as compared to that of high phase currents during inrush. The inrush currents could be mitigated by using a neutral resistor when sequential switching is implemented. From the sequential energizing scheme performance, the neutral resistor size plays the significant role in the scheme effectiveness. Through simulation, it was found that a few ohms neutral grounding resistor can effectively achieve inrush currents reduction. If the neutral resistor is directly selected to minimize the peak of the actual inrush current, a much lower resistor value could be found.This paper presents an analytical method to select optimal neutral grounding resistor for mitigation of inrush current. In this method nonlinearity and core loss of the transformer has been modeled and derived analytical equations.Index Terms--Inrush current, neutral grounding resistor, transformerI.I NTRODUCTIONThe energizing of transformers produces high inrush currents. The nature of inrush currents have rich in harmonics coupled with relatively a long duration, leads to adverse effects on the residual life of the transformer, malfunction of the protection system [1] and power quality [2]. In the power-system industry, two different strategies have been implemented to tackle the problem of transformer inrush currents. The first strategy focuses on adapting to the effects of inrush currents by desensitizing the protection elements. Other approaches go further by 'over-sizing' the magnetic core to achieve higher saturation flux levels. These partial countermeasures impose downgrades on the system's operational reliability, considerable increases unit cost, high mechanical stresses on the transformer and lead to a lower power quality. The second strategy focuses on reducing the inrush current magnitude itself during the energizing process. Minimizing the inrush current will extend the transformer's lifetime and increase the reliability of operation and lower maintenance and down-time costs. Meanwhile, the problem of protection-system malfunction is eliminated during transformer energizing. The available inrush current mitigation consist "closing resistor"[3], "control closing of circuit breaker"[4],[5], "reduction of residual flux"[6], "neutral resistor with sequential switching"[7],[8],[9].The sequential energizing technique presents inrush-reduction scheme due to transformer energizing. This scheme involves the sequential energizing of the three phases transformer together with the insertion of a properly sized resistor at the neutral point of the transformer energizing side [7] ,[8],[9] (Fig. 1).The neutral resistor based scheme acts to minimize the induced voltage across the energized windings during sequential switching of each phase and, hence, minimizes the integral of the applied voltage across the windings.The scheme has the main advantage of being a simpler, more reliable and more cost effective than the synchronous switching and pre-insertion resistor schemes. The scheme has no requirements for the speed of the circuit breaker or the determination of the residual flux. Sequential switching of the three phases can be implemented through either introducing a mechanical delay between each pole in the case of three phase breakers or simply through adjusting the breaker trip-coil time delay for single pole breakers.A further study of the scheme revealed that a much lower resistor size is equally effective. The steady-state theory developed for neutral resistor sizing [8] is unable to explain this phenomenon. This phenomenon must be understood using transient analysis.Fig. 1. The sequential phase energizing schemeUPEC201031st Aug - 3rd Sept 2010The rise of neutral voltage is the main limitation of the scheme. Two methods present to control the neutral voltage rise: the use of surge arrestors and saturated reactors connected to the neutral point. The use of surge arresters was found to be more effective in overcoming the neutral voltage rise limitation [9].The main objective of this paper is to derive an analytical relationship between the peak of the inrush current and the size of the resistor. This paper presents a robust analytical study of the transformer energizing phenomenon. The results reveal a good deal of information on inrush currents and the characteristics of the sequential energizing scheme.II. SCHEME PERFORMANCESince the scheme adopts sequential switching, each switching stage can be investigated separately. For first-phase switching, the scheme's performance is straightforward. The neutral resistor is in series with the energized phase and this resistor's effect is similar to a pre-insertion resistor.The second- phase energizing is one of the most difficult to analyze. Fortunately, from simulation studies, it was found that the inrush current due to second-phase energizing is lower than that due to first-phase energizing for the same value of n R [9]. This result is true for the region where the inrush current of the first-phase is decreasing rapidly as n R increases. As a result, when developing a neutral-resistor-sizing criterion, the focus should be directed towards the analysis of the first-phase energizing.III. A NALYSIS OF F IRST -P HASE E NERGIZING The following analysis focuses on deriving an inrush current waveform expression covering both the unsaturatedand saturated modes of operation respectively. The presented analysis is based on a single saturated core element, but is suitable for analytical modelling of the single-phase transformers and for the single-phase switching of three-phase transformers. As shown in Fig. 2, the transformer's energized phase was modeled as a two segmented saturated magnetizing inductance in series with the transformer's winding resistance, leakage inductance and neutral resistance. The iron core non-l inear inductance as function of the operating flux linkages is represented as a linear inductor inunsaturated ‘‘m l ’’ and saturated ‘‘s l ’’ modes of operation respectively. (a)(b)Fig. 2. (a) Transformer electrical equivalent circuit (per-phase) referred to the primary side. (b) Simplified, two slope saturation curve.For the first-phase switching stage, the equivalent circuit represented in Fig. 2(a) can accurately represent behaviour of the transformer for any connection or core type by using only the positive sequence Flux-Current characteristics. Based on the transformer connection and core structure type, the phases are coupled either through the electrical circuit (3 single phase units in Yg-D connection) or through the Magnetic circuit (Core type transformers with Yg-Y connection) or through both, (the condition of Yg-D connection in an E-Core or a multi limb transformer). The coupling introduced between the windings will result in flux flowing through the limbs or magnetic circuits of un-energized phases. For the sequential switching application, the magnetic coupling will result in an increased reluctance (decreased reactance) for zero sequence flux path if present. The approach presented here is based on deriving an analytical expression relating the amount of inrush current reduction directly to the neutral resistor size. Investigation in this field has been done and some formulas were given to predict the general wave shape or the maximum peak current.A. Expression for magnitude of inrush currentIn Fig. 2(a), p r and p l present the total primary side resistance and leakage reactance. c R shows the total transformer core loss. Secondary side resistance sp r and leakage reactance sp l as referred to primary side are also shown. P V and s V represent the primary and secondary phase to ground terminal voltages, respectively.During first phase energizing, the differential equation describing behaviour of the transformer with saturated ironcore can be written as follows:()())sin((2) (1)φω+⋅⋅=⋅+⋅+⋅+=+⋅+⋅+=t V (t)V dtdi di d λdt di l (t)i R r (t)V dt d λdt di l (t)i R r (t)V m P ll p pp n p P p p p n p PAs the rate of change of the flux linkages with magnetizing current dt d /λcan be represented as an inductance equal to the slope of the i −λcurve, (2) can be re-written as follows;()(3) )()()(dtdi L dt di l t i R r t V lcore p p P n p P ⋅+⋅+⋅+=λ (4) )()(L core l p c l i i R dtdi−⋅=⋅λ⎩⎨⎧==sml core L L di d L λλ)(s s λλλλ>≤The general solution of the differential equations (3),(4) has the following form;⎪⎩⎪⎨⎧>−⋅⋅+−⋅+−−⋅+≤−⋅⋅+−⋅+−⋅=(5) )sin(//)()( )sin(//)(s s 22222221211112121111λλψωττλλψωττt B t e A t t e i A t B t e A t e A t i s s pSubscripts 11,12 and 21,22 denote un-saturated and saturated operation respectively. The parameters given in the equation (5) are given by;() )(/12221σ⋅++⎟⎟⎠⎞⎜⎜⎝⎛⋅−++⋅=m p c p m n p c m m x x R x x R r R x V B()2222)(/1σ⋅++⎟⎟⎠⎞⎜⎜⎝⎛⋅−++⋅=s p c p s n p c s m x x R x x R r R x V B⎟⎟⎟⎟⎟⎠⎞⎜⎜⎜⎜⎜⎝⎛⋅−+++=⋅−−⎟⎟⎟⎠⎞⎜⎜⎜⎝⎛−c p m n p m p c m R x x R r x x R x σφψ111tan tan ⎟⎟⎟⎟⎟⎠⎞⎜⎜⎜⎜⎜⎝⎛⋅−+++=⋅−−⎟⎟⎟⎠⎞⎜⎜⎜⎝⎛−c p s n p s p c m R R r x x R x σφψ112tan tan )sin(111211ψ⋅=+B A A )sin(222221s t B A A ⋅−⋅=+ωψ mp n p m p m p m p c xx R r x x x x x x R ⋅⋅+⋅−⋅+−⋅+⋅⋅⋅=)(4)()(21211σστm p n p m p m p m p c xx R r x x x x x x R ⋅⋅+⋅−⋅++⋅+⋅⋅⋅=)(4)()(21212σστ s p n p s p s p s p xx R r x x x x x x c R ⋅⋅+⋅−⋅+−⋅+⋅⋅⋅=)(4)()(21221σστ sp n p s p s p sp c xx R r x x x x x x R ⋅⋅+⋅−⋅++⋅+⋅⋅⋅=)(4)()(21222σστ ⎟⎟⎠⎞⎜⎜⎝⎛−⋅==s rs s ri i λλλ10 cnp R R r ++=1σ21221112 , ττττ>>>>⇒>>c R , 012≈A , 022≈A According to equation (5), the required inrush waveform assuming two-part segmented i −λcurve can be calculated for two separate un-saturated and saturated regions. For thefirst unsaturated mode, the current can be directly calculated from the first equation for all flux linkage values below the saturation level. After saturation is reached, the current waveform will follow the second given expression for fluxlinkage values above the saturation level. The saturation time s t can be found at the time when the current reaches the saturation current level s i .Where m λ,r λ,m V and ωare the nominal peak flux linkage, residual flux linkage, peak supply voltage and angular frequency, respectivelyThe inrush current waveform peak will essentially exist during saturation mode of operation. The focus should be concentrated on the second current waveform equation describing saturated operation mode, equation (5). The expression of inrush current peak could be directly evaluated when both saturation time s t and peak time of the inrush current waveform peak t t =are known [9].(10))( (9) )(2/)(222222121//)()(2B eA t e i A peak peak t s t s n peak n n peak R I R R t +−⋅+−−⋅+=+=ττωψπThe peak time peak t at which the inrush current will reachits peak can be numerically found through setting the derivative of equation (10) with respect to time equal to zero at peak t t =.()(11) )sin(/)(022222221212221/ψωωττττ−⋅⋅⋅−−−⋅+−=+−⋅peak t s t B A t te A i peak s peakeThe inrush waveform consists of exponentially decaying'DC' term and a sinusoidal 'AC' term. Both DC and AC amplitudes are significantly reduced with the increase of the available series impedance. The inrush waveform, neglecting the relatively small saturating current s i ,12A and 22A when extremely high could be normalized with respect to theamplitude of the sinusoidal term as follows; (12) )sin(/)()(2221221⎥⎦⎤⎢⎣⎡−⋅+−−⋅⋅=ψωτt t t e B A B t i s p(13) )sin(/)()sin()( 22221⎥⎦⎤⎢⎣⎡−⋅+−−⋅⋅−⋅=ψωτωψt t t e t B t i s s p ))(sin()( 2s n n t R R K ⋅−=ωψ (14) ωλλλφλφωλλφωmm m r s s t r m s mV t dt t V dtd t V V s=⎪⎭⎪⎬⎫⎪⎩⎪⎨⎧⎥⎥⎦⎤⎢⎢⎣⎡⎟⎟⎠⎞⎜⎜⎝⎛−−+−⋅=+⋅+⋅⋅==+⋅⋅=−∫(8) 1cos 1(7))sin((6))sin(10The factor )(n R K depends on transformer saturation characteristics (s λand r λ) and other parameters during saturation.Typical saturation and residual flux magnitudes for power transformers are in the range[9]; .).(35.1.).(2.1u p u p s <<λ and .).(9.0.).(7.0u p r u p <<λIt can be easily shown that with increased damping 'resistance' in the circuit, where the circuit phase angle 2ψhas lower values than the saturation angle s t ⋅ω, the exponential term is negative resulting in an inrush magnitude that is lowerthan the sinusoidal term amplitude.B. Neutral Grounding Resistor SizingBased on (10), the inrush current peak expression, it is now possible to select a neutral resistor size that can achieve a specific inrush current reduction ratio )(n R α given by:(15) )0(/)()(==n peak n peak n R I R I R α For the maximum inrush current condition (0=n R ), the total energized phase system impedance ratio X/R is high and accordingly, the damping of the exponential term in equation (10) during the first cycle can be neglected; [][](16))0(1)0()0(2212=⋅++⎥⎦⎤⎢⎣⎡⋅−+===⎟⎟⎠⎞⎜⎜⎝⎛+⋅⋅n s p c p s pR x n m n peak R x x R x x r R K V R I c s σ High n R values leading to considerable inrush current reduction will result in low X / R ratios. It is clear from (14) that X / R ratios equal to or less than 1 ensure negative DC component factor ')(n R K ' and hence the exponential term shown in (10) can be conservatively neglected. Accordingly, (10) can be re-written as follows;()[](17) )()(22122n s p c p s n p R x m n n peak R x x R x x R r V R B R I c s σ⋅++⎥⎦⎤⎢⎣⎡⋅−+=≈⎟⎟⎠⎞⎜⎜⎝⎛+⋅Using (16) and (17) to evaluate (15), the neutral resistorsize which corresponds to a specific reduction ratio can be given by;[][][](18) )0()(1)0( 12222=⋅++⋅−⋅++⋅−+⋅+=⎥⎥⎦⎤⎢⎢⎣⎡⎥⎥⎦⎤⎢⎢⎣⎡=n s p c p s p n s p c p s n p n R x x R x x r R x x R x x R r R K σσα Very high c R values leading to low transformer core loss, it can be re-written equation (18) as follows [9]; [][][][](19) 1)0(12222s p p s p n p n x x r x x R r R K +++++⋅+==α Equations (18) and (19) reveal that transformers require higher neutral resistor value to achieve the desired inrush current reduction rate. IV. A NALYSIS OF SECOND-P HASE E NERGIZING It is obvious that the analysis of the electric and magnetic circuit behavior during second phase switching will be sufficiently more complex than that for first phase switching.Transformer behaviour during second phase switching was served to vary with respect to connection and core structure type. However, a general behaviour trend exists within lowneutral resistor values where the scheme can effectively limitinrush current magnitude. For cases with delta winding or multi-limb core structure, the second phase inrush current is lower than that during first phase switching. Single phase units connected in star/star have a different performance as both first and second stage inrush currents has almost the same magnitude until a maximum reduction rate of about80% is achieved. V. NEUTRAL VOLTAGE RISEThe peak neutral voltage will reach values up to peak phasevoltage where the neutral resistor value is increased. Typicalneutral voltage peak profile against neutral resistor size is shown in Fig. 6- Fig. 8, for the 225 KVA transformer during 1st and 2nd phase switching. A del ay of 40 (ms) between each switching stage has been considered. VI. S IMULATION A 225 KVA, 2400V/600V, 50 Hz three phase transformer connected in star-star are used for the simulation study. The number of turns per phase primary (2400V) winding is 128=P N and )(01.0pu R R s P ==, )(05.0pu X X s P ==,active power losses in iron core=4.5 KW, average length and section of core limbs (L1=1.3462(m), A1=0.01155192)(2m ), average length and section of yokes (L2=0.5334(m),A2=0.01155192)(2m ), average length and section of air pathfor zero sequence flux return (L0=0.0127(m),A0=0.01155192)(2m ), three phase voltage for fluxinitialization=1 (pu) and B-H characteristic of iron core is inaccordance with Fig.3. A MATLAB program was prepared for the simulation study. Simulation results are shown in Fig.4-Fig.8.Fig. 3.B-H characteristic iron coreFig.4. Inrush current )(0Ω=n RFig.5. Inrush current )(5Ω=n RFig.6. Inrush current )(50Ω=n RFig.7. Maximum neutral voltage )(50Ω=n RFig.8. Maximum neutral voltage ).(5Ω=n RFig.9. Maximum inrush current in (pu), Maximum neutral voltage in (pu), Duration of the inrush current in (s)VII. ConclusionsIn this paper, Based on the sequential switching, presents an analytical method to select optimal neutral grounding resistor for transformer inrush current mitigation. In this method, complete transformer model, including core loss and nonlinearity core specification, has been used. It was shown that high reduction in inrush currents among the three phases can be achieved by using a neutral resistor .Other work presented in this paper also addressed the scheme's main practical limitation: the permissible rise of neutral voltage.VIII.R EFERENCES[1] Hanli Weng, Xiangning Lin "Studies on the UnusualMaloperation of Transformer Differential Protection During the Nonlinear Load Switch-In",IEEE Transaction on Power Delivery, vol. 24, no.4, october 2009.[2] Westinghouse Electric Corporation, Electric Transmissionand Distribution Reference Book, 4th ed. East Pittsburgh, PA, 1964.[3] K.P.Basu, Stella Morris"Reduction of Magnetizing inrushcurrent in traction transformer", DRPT2008 6-9 April 2008 Nanjing China.[4] J.H.Brunke, K.J.Frohlich “Elimination of TransformerInrush Currents by Controlled Switching-Part I: Theoretical Considerations” IEEE Trans. On Power Delivery, Vol.16,No.2,2001. [5] R. Apolonio,J.C.de Oliveira,H.S.Bronzeado,A.B.deVasconcellos,"Transformer Controlled Switching:a strategy proposal and laboratory validation",IEEE 2004, 11th International Conference on Harmonics and Quality of Power.[6] E. Andersen, S. Bereneryd and S. Lindahl, "SynchronousEnergizing of Shunt Reactors and Shunt Capacitors," OGRE paper 13-12, pp 1-6, September 1988.[7] Y. Cui, S. G. Abdulsalam, S. Chen, and W. Xu, “Asequential phase energizing method for transformer inrush current reduction—part I: Simulation and experimental results,” IEEE Trans. Power Del., vol. 20, no. 2, pt. 1, pp. 943–949, Apr. 2005.[8] W. Xu, S. G. Abdulsalam, Y. Cui, S. Liu, and X. Liu, “Asequential phase energizing method for transformer inrush current reduction—part II: Theoretical analysis and design guide,” IEEE Trans. Power Del., vol. 20, no. 2, pt. 1, pp. 950–957, Apr. 2005.[9] S.G. Abdulsalam and W. Xu "A Sequential PhaseEnergization Method for Transformer Inrush current Reduction-Transient Performance and Practical considerations", IEEE Transactions on Power Delivery,vol. 22, No.1, pp. 208-216,Jan. 2007.。
geoscientific model development

geoscientific model developmentGeoscientific model development refers to the development of models that simulate the physical, chemical, and biological processes occurring in an area of the Earth's landscape. This modelling is done with a combination of data and computer simulations to create a model of the area that can be used to make predictions regarding the future conditions of the area, as well as to assess the impact of human activities, such as land use and energy sources, on the environment.Geoscientific models are used in a variety of applications and research, including environmental decision-making, climate forecasting, resource exploration and management, and engineering and planning. For example, geoscientific models have been used to predict the impacts of climate change on global sea levels, identify population trends in different parts of the world, develop land use plans for sustainable development, and assess potential earthquake hazards.Developing an effective geoscientific model requires the interdisciplinary integration of data from several sources. This includes geospatial data like topography, hydrology, and climate, as well as observational data from satellites, aircraft, and other sources. The data is then used to create a 3D computer representation of the area, which is then used to simulate the various processes and interactions thataffect the area.Geoscientific modelling is constantly evolving andbecoming increasingly sophisticated. As computer power and capabilities continue to improve, so too do the modelling techniques and algorithms used to create geoscientific models. This is allowing for more realistic simulations of theEarth's environment, which will improve our understanding of the impacts of human activities on the planet.。
finetuning后的模型参数

finetuning后的模型参数随着大数据时代的到来,深度学习成为了人工智能领域的热门技术之一。
其中,模型参数调整是深度学习中最重要也是最困难的任务之一。
这就是为什么finetuning(微调)成为了大多数人使用的技术之一。
本文旨在探讨finetuning后的模型参数。
1.什么是finetuningfinetuning是指在训练好的模型上进行微调,以适应新的数据集或任务。
在深度学习中,卷积神经网络被广泛应用于图像分类、目标检测、分割等任务中。
在这些任务中,通常需要大量的标注数据才能获得足够的准确性。
但对于许多实际应用场景,标注数据往往是有限的,这就需要我们在不足的标注数据量下,提高模型的分类准确率,这就需要finetuning技术的应用。
2.finetuning过程finetuning是基于已经训练好的模型进行调整。
它的过程通常包括以下几个步骤:(1)选择基础模型。
通常情况下,我们会选择在大规模的数据集上进行训练的预训练模型,例如ResNet、VGG等。
(2)修改全连接层(或者其他分类器)。
我们需要根据新的任务需求,修改末层的全连接层或其他分类器来适应新的任务。
(3)设置学习率。
由于新的数据集与基础模型的差异较大,我们需要对学习率进行微调,以便获得更好的性能。
(4)迭代训练。
在finetuning的过程中,我们需要迭代训练模型,以便更好地适应新的数据集和新的任务。
(5)模型评估。
为了获得最好的性能,我们需要对模型进行评估,通常情况下可以使用精度、召回率、F1值等指标来评估模型的性能。
3.finetuning后的模型参数finetuning后的模型参数通常会比基础模型的参数略多。
这是因为在finetuning的过程中,我们通常会修改末层的全连接层或其他分类器,这就需要添加新的参数。
另外,在迭代训练的过程中,我们还需要微调原始模型的参数,以适应新的数据集。
因此,finetuning后的模型参数通常会略多于基础模型的参数。
finetuning工作原理

finetuning工作原理标题:深入理解Finetuning工作原理一、引言Finetuning,即微调技术,是深度学习领域中一种重要的模型优化方法。
它在预训练模型的基础上进行进一步的训练调整,以适应新的特定任务或数据集,尤其在自然语言处理(NLP)和计算机视觉(CV)等领域得到了广泛应用。
本文旨在详细介绍finetuning的工作原理及其在实际应用中的重要性。
二、Finetuning基本概念Finetuning的核心思想是在一个已经在大规模无标注数据上预训练好的模型基础上,针对目标特定任务的数据进行针对性训练。
这个预训练模型通常已经在类似的任务上积累了丰富的特征表示能力,例如BERT、GPT等在NLP领域的预训练模型,或者ImageNet预训练的CNN模型在CV领域。
三、Finetuning工作原理1. 预训练阶段:首先,模型在大规模且多样化的数据集上进行训练,通过自监督或无监督的方式学习到通用的、高质量的特征表示。
这一阶段的目标是让模型掌握基础的模式识别和理解能力。
2. 微调阶段:随后,在预训练模型的基础上,针对具体任务(如文本分类、情感分析、图像识别等),使用相对较小但具有针对性的任务数据集进行finetune。
在这一阶段,通常会保留预训练模型的大部分权重不变,仅对输出层或部分隐藏层的参数进行更新,有时也会根据需要调整整个模型的参数。
通过最小化新任务上的损失函数,使模型能够基于已有的通用知识,快速适应并学会解决特定任务。
3. 迭代优化:在微调过程中,模型根据目标任务的标签信息进行反向传播,不断调整参数以最小化特定任务的损失函数,最终达到提升模型在目标任务上的性能的目的。
四、Finetuning的优势与挑战优势:- 利用预训练模型可以大大减少对大规模标注数据的依赖,有效应对小样本学习问题。
- 能够快速迁移至新的任务,缩短开发周期,提高模型性能。
挑战:- 微调过程需要谨慎对待,过度微调可能导致过拟合,尤其是当目标任务数据量有限时。
IATA AHM目录

Airport Handling ManualEffective 1 January—31 December 201838NOTICEDISCLAIMER. The information contained in thispublication is subject to constant review in the lightof changing government requirements and regula-tions. No subscriber or other reader should act onthe basis of any such information without referringto applicable laws and regulations and/or withouttak ing appropriate professional advice. Althoughevery effort has been made to ensure accuracy, theInternational Air Transport Association shall not beheld responsible for any loss or damage caused byerrors, omissions, misprints or misinterpretation ofthe contents hereof. Furthermore, the InternationalAir Transport Association expressly disclaims anyand all liability to any person or entity, whether apurchaser of this publication or not, in respect ofanything done or omitted, and the consequencesof anything done or omitted, by any such person orentity in reliance on the contents of this publication.Opinions expressed in advertisements appearing inthis publication are the advertiser’s opinions and donot necessarily reflect those of IATA. The mentionof specific companies or products in advertisementdoes not imply that they are endorsed or recom-mended by IATA in preference to others of a simi-lar nature which are not mentioned or advertised.© International Air Transport Association. AllRights Reserved. No part of this publication maybe reproduced, recast, reformatted or trans-mitted in any form by any means, electronic ormechanical, including photocopying, record-ing or any information storage and retrieval sys-tem, without the prior written permission from:Senior Vice PresidentAirport, Passenger, Cargo and SecurityInternational Air Transport Association800 Place VictoriaP.O. Box 113Montreal, QuebecCANADA H4Z 1M1Airport Handling ManualMaterial No.: 9343-38ISBN 978-92-9229-505-9© 2017 International Air Transport Association. All rights reserved.TABLE OF CONTENTSPage Preface (xv)Introduction (xvii)General (1)AHM001Chapter0—Record of Revisions (1)AHM011Standard Classification and Numbering for Members Airport Handling Manuals (2)AHM012Office Function Designators for Airport Passenger and Baggage Handling (30)AHM020Guidelines for the Establishment of Airline Operators Committees (31)AHM021Guidelines for Establishing Aircraft Ground Times (34)AHM050Aircraft Emergency Procedures (35)AHM070E-Invoicing Standards (53)Chapter1—PASSENGER HANDLING (91)AHM100Chapter1—Record of Revisions (91)AHM110Involuntary Change of Carrier,Routing,Class or Type of Fare (92)AHM112Denied Boarding Compensation (98)AHM120Inadmissible Passengers and Deportees (99)AHM140Items Removed from a Passenger's Possession by Security Personnel (101)AHM141Hold Loading of Duty-Free Goods (102)AHM170Dangerous Goods in Passenger Baggage (103)AHM176Recommendations for the Handling of Passengers with Reduced Mobility(PRM) (105)AHM176A Acceptance and Carriage of Passengers with Reduced Mobility(PRM) (106)AHM180Carriage of Passengers with Communicable Diseases (114)AHM181General Guidelines for Passenger Agents in Case of SuspectedCommunicable Disease (115)Chapter2—BAGGAGE HANDLING (117)AHM200Chapter2—Record of Revisions (117)AHM210Local Baggage Committees (118)AHM211Airport Operating Rules (124)Airport Handling ManualPageChapter2—BAGGAGE HANDLING(continued)AHM212Interline Connecting Time Intervals—Passenger and Checked Baggage (126)AHM213Form of Interline Baggage Tags (128)AHM214Use of the10Digit Licence Plate (135)AHM215Found and Unclaimed Checked Baggage (136)AHM216On-Hand Baggage Summary Tag (138)AHM217Forwarding Mishandled Baggage (139)AHM218Dangerous Goods in Passengers'Baggage (141)AHM219Acceptance of Firearms and Other Weapons and Small Calibre Ammunition (142)AHM221Acceptance of Power Driven Wheelchairs or Other Battery Powered Mobility Aidsas Checked Baggage (143)AHM222Passenger/Baggage Reconciliation Procedures (144)AHM223Licence Plate Fallback Sortation Tags (151)AHM224Baggage Taken in Error (154)AHM225Baggage Irregularity Report (156)AHM226Tracing Unchecked Baggage and Handling Damage to Checked and UncheckedBaggage (159)AHM230Baggage Theft and Pilferage Prevention (161)AHM231Carriage of Carry-On Baggage (164)AHM232Handling of Security Removed Items (168)AHM240Baggage Codes for Identifying ULD Contents and/or Bulk-Loaded Baggage (169)Chapter3—CARGO/MAIL HANDLING (171)AHM300Chapter3—Record of Revisions (171)AHM310Preparation for Loading of Cargo (172)AHM311Securing of Load (174)AHM312Collection Sacks and Bags (177)AHM320Handling of Damaged Cargo (178)AHM321Handling of Pilfered Cargo (179)AHM322Handling Wet Cargo (180)AHM330Handling Perishable Cargo (182)AHM331Handling and Protection of Valuable Cargo (184)AHM332Handling and Stowage of Live Animals (188)AHM333Handling of Human Remains (190)Table of ContentsPageChapter3—CARGO/MAIL HANDLING(continued)AHM340Acceptance Standards for the Interchange of Transferred Unit Load Devices (191)AHM345Handling of Battery Operated Wheelchairs/Mobility AIDS as Checked Baggage (197)AHM350Mail Handling (199)AHM351Mail Documents (203)AHM353Handling of Found Mail (218)AHM354Handling of Damaged Mail (219)AHM355Mail Security (220)AHM356Mail Safety (221)AHM357Mail Irregularity Message (222)AHM360Company Mail (224)AHM380Aircraft Documents Stowage (225)AHM381Special Load—Notification to Captain(General) (226)AHM382Special Load—Notification to Captain(EDP Format and NOTOC Service) (231)AHM383Special Load—Notification to Captain(EDP NOTOC Summary) (243)AHM384NOTOC Message(NTM) (246)Chapter4—AIRCRAFT HANDLING AND LOADING (251)AHM400Chapter4—Record of Revisions (251)AHM411Provision and Carriage of Loading Accessories (252)AHM420Tagging of Unit Load Devices (253)AHM421Storage of Unit Load Devices (263)AHM422Control of Transferred Unit Load Devices (268)AHM423Unit Load Device Stock Check Message (273)AHM424Unit Load Device Control Message (275)AHM425Continued Airworthiness of Unit Load Devices (279)AHM426ULD Buildup and Breakdown (283)AHM427ULD Transportation (292)AHM430Operating of Aircraft Doors (295)AHM431Aircraft Ground Stability—Tipping (296)AHM440Potable Water Servicing (297)AHM441Aircraft Toilet Servicing (309)Airport Handling ManualPageChapter4—AIRCRAFT HANDLING AND LOADING(continued)AHM450Standardisation of Gravity Forces against which Load must be Restrained (310)AHM451Technical Malfunctions Limiting Load on Aircraft (311)AHM453Handling/Bulk Loading of Heavy Items (312)AHM454Handling and Loading of Big Overhang Items (313)AHM455Non CLS Restrained ULD (316)AHM460Guidelines for Turnround Plan (323)AHM462Safe Operating Practices in Aircraft Handling (324)AHM463Safety Considerations for Aircraft Movement Operations (337)AHM465Foreign Object Damage(FOD)Prevention Program (340)Chapter5—LOAD CONTROL (343)AHM500Chapter5—Record of Revisions (343)AHM501Terms and Definitions (345)AHM503Recommended Requirements for a New Departure Control System (351)AHM504Departure Control System Evaluation Checklist (356)AHM505Designation of Aircraft Holds,Compartments,Bays and Cabin (362)AHM510Handling/Load Information Codes to be Used on Traffic Documents and Messages (368)AHM513Aircraft Structural Loading Limitations (377)AHM514EDP Loading Instruction/Report (388)AHM515Manual Loading Instruction/Report (404)AHM516Manual Loadsheet (416)AHM517EDP Loadsheet (430)AHM518ACARS Transmitted Loadsheet (439)AHM519Balance Calculation Methods (446)AHM520Aircraft Equipped with a CG Targeting System (451)AHM530Weights for Passengers and Baggage (452)AHM531Procedure for Establishing Standard Weights for Passengers and Baggage (453)AHM533Passengers Occupying Crew Seats (459)AHM534Weight Control of Load (460)AHM536Equipment in Compartments Procedure (461)AHM537Ballast (466)Table of ContentsPageChapter5—LOAD CONTROL(continued)AHM540Aircraft Unit Load Device—Weight and Balance Control (467)AHM550Pilot in Command's Approval of the Loadsheet (468)AHM551Last Minute Changes on Loadsheet (469)AHM561Departure Control System,Carrier's Approval Procedures (471)AHM562Semi-Permanent Data Exchange Message(DEM) (473)AHM564Migration from AHM560to AHM565 (480)AHM565EDP Semi-Permanent Data Exchange for New Generation Departure Control Systems (500)AHM570Automated Information Exchange between Check-in and Load Control Systems (602)AHM571Passenger and Baggage Details for Weight and Balance Report(PWR) (608)AHM580Unit Load Device/Bulk Load Weight Statement (613)AHM581Unit Load Device/Bulk Load Weight Signal (615)AHM583Loadmessage (619)AHM587Container/Pallet Distribution Message (623)AHM588Statistical Load Summary (628)AHM590Load Control Procedures and Loading Supervision Responsibilities (631)AHM591Weight and Balance Load Control and Loading Supervision Training and Qualifications (635)Chapter6—MANAGEMENT AND SAFETY (641)AHM600Chapter6—Record of Revisions (641)AHM610Guidelines for a Safety Management System (642)AHM611Airside Personnel:Responsibilities,Training and Qualifications (657)AHM612Airside Performance Evaluation Program (664)AHM615Quality Management System (683)AHM616Human Factors Program (715)AHM619Guidelines for Producing Emergency Response Plan(s) (731)AHM620Guidelines for an Emergency Management System (733)AHM621Security Management (736)AHM633Guidelines for the Handling of Emergencies Requiring the Evacuation of an Aircraft During Ground Handling (743)AHM650Ramp Incident/Accident Reporting (745)AHM652Recommendations for Airside Safety Investigations (750)AHM660Carrier Guidelines for Calculating Aircraft Ground Accident Costs (759)Airport Handling ManualChapter7—AIRCRAFT MOVEMENT CONTROL (761)AHM700Chapter7—Record of Revisions (761)AHM710Standards for Message Formats (762)AHM711Standards for Message Corrections (764)AHM730Codes to be Used in Aircraft Movement and Diversion Messages (765)AHM731Enhanced Reporting on ATFM Delays by the Use of Sub Codes (771)AHM780Aircraft Movement Message (774)AHM781Aircraft Diversion Message (786)AHM782Fuel Monitoring Message (790)AHM783Request Information Message (795)AHM784Gate Message (797)AHM785Aircraft Initiated Movement Message(MVA) (802)AHM790Operational Aircraft Registration(OAR)Message (807)Chapter8—GROUND HANDLING AGREEMENTS (811)AHM800Chapter8—Record of Revisions (811)AHM801Introduction to and Comments on IATA Standard Ground Handling Agreement(SGHA) (812)AHM803Service Level Agreement Example (817)AHM810IATA Standard Ground Handling Agreement (828)AHM811Yellow Pages (871)AHM813Truck Handling (872)AHM815Standard Transportation Documents Service Main Agreement (873)AHM817Standard Training Agreement (887)AHM830Ground Handling Charge Note (891)AHM840Model Agreement for Electronic Data Interchange(EDI) (894)Chapter9—AIRPORT HANDLING GROUND SUPPORT EQUIPMENT SPECIFICATIONS (911)AHM900Chapter9—Record of Revisions (911)AHM901Functional Specifications (914)AHM904Aircraft Servicing Points and System Requirements (915)AIRBUS A300B2320-/B4/C4 (917)A300F4-600/-600C4 (920)A310–200/200C/300 (926)A318 (930)A319 (933)Table of ContentsPageChapter9—AIRPORT HANDLING GROUND SUPPORT EQUIPMENT SPECIFICATIONS(continued) AHM904Aircraft Doors,Servicing Points and System Requirements for the Use of Ground Support Equipment(continued)A320 (936)A321 (940)A330-200F (943)A330-300 (948)A340-200 (951)A340-300 (955)A340-500 (959)A340-600 (962)Airbus350900passenger (965)AIRBUS A380-800/-800F (996)ATR42100/200 (999)ATR72 (1000)AVRO RJ70 (1001)AVRO RJ85 (1002)AVRO RJ100 (1003)B727-200 (1004)B737–200/200C (1008)B737-300,400,-500 (1010)B737-400 (1013)B737-500 (1015)B737-600,-700,-700C (1017)B737-700 (1020)B737-800 (1022)B737-900 (1026)B747–100SF/200C/200F (1028)B747–400/400C (1030)B757–200 (1038)B757–300 (1040)Airport Handling ManualPageChapter9—AIRPORT HANDLING GROUND SUPPORT EQUIPMENT SPECIFICATIONS(continued) AHM904Aircraft Doors,Servicing Points and System Requirements for the Use of Ground Support Equipment(continued)B767—200/200ER (1041)B767—300/300ER (1044)B767—400ER (1048)B777–200/200LR (1051)B777–300/300ER (1055)Boeing787800passenger (1059)BAe ATP(J61) (1067)Bombardier CS100 (1068)Bombardier CS300 (1072)CL-65(CRJ100/200) (1076)DC8–40/50F SERIES (1077)DC8–61/61F (1079)DC8–62/62F (1081)DC8–63/63F (1083)DC9–15/21 (1085)DC9–32 (1086)DC9–41 (1087)DC9–51 (1088)DC10–10/10CF (1089)DC10–30/40,30/40CF (1091)EMBRAER EMB-135Regional Models (1092)EMBRAER EMB-145Regional Models (1094)Embraer170 (1096)Embraer175 (1098)Embraer190 (1100)Embraer195 (1102)FOKKER50(F27Mk050) (1104)FOKKER50(F27Mk0502) (1106)Chapter9—AIRPORT HANDLING GROUND SUPPORT EQUIPMENT SPECIFICATIONS(continued) AHM904Aircraft Doors,Servicing Points and System Requirements for the Use of Ground Support Equipment(continued)FOKKER70(F28Mk0070) (1108)FOKKER100(F28Mk0100) (1110)FOKKER100(F28Mk0100) (1112)IL-76T (1114)MD-11 (1116)MD–80SERIES (1118)SAAB2000 (1119)SAAB SF-340 (1120)TU-204 (1122)AHM905Reference Material for Civil Aircraft Ground Support Equipment (1125)AHM905A Cross Reference of IATA Documents with SAE,CEN,and ISO (1129)AHM909Summary of Unit Load Device Capacity and Dimensions (1131)AHM910Basic Requirements for Aircraft Ground Support Equipment (1132)AHM911Ground Support Equipment Requirements for Compatibility with Aircraft Unit Load Devices (1136)AHM912Standard Forklift Pockets Dimensions and Characteristics for Forkliftable General Support Equipment (1138)AHM913Basic Safety Requirements for Aircraft Ground Support Equipment (1140)AHM914Compatibility of Ground Support Equipment with Aircraft Types (1145)AHM915Standard Controls (1147)AHM916Basic Requirements for Towing Vehicle Interface(HITCH) (1161)AHM917Basic Minimum Preventive Maintenance Program/Schedule (1162)AHM920Functional Specification for Self-Propelled Telescopic Passenger Stairs (1164)AHM920A Functional Specification for Towed Passenger Stairs (1167)AHM921Functional Specification for Boarding/De-Boarding Vehicle for Passengers withReduced Mobility(PRM) (1169)AHM922Basic Requirements for Passenger Boarding Bridge Aircraft Interface (1174)AHM923Functional Specification for Elevating Passenger Transfer Vehicle (1180)AHM924Functional Specification for Heavy Item Lift Platform (1183)AHM925Functional Specification for a Self-Propelled Conveyor-Belt Loader (1184)AHM925A Functional Specification for a Self-Propelled Ground Based in-Plane LoadingSystem for Bulk Cargo (1187)Chapter9—AIRPORT HANDLING GROUND SUPPORT EQUIPMENT SPECIFICATIONS(continued) AHM925B Functional Specification for a Towed Conveyor-Belt Loader (1190)AHM926Functional Specification for Upper Deck Catering Vehicle (1193)AHM927Functional Specification for Main Deck Catering Vehicle (1197)AHM930Functional Specification for an Upper Deck Container/Pallet Loader (1201)AHM931Functional Specification for Lower Deck Container/Pallet Loader (1203)AHM932Functional Specification for a Main Deck Container/Pallet Loader (1206)AHM933Functional Specification of a Powered Extension Platform to Lower Deck/Container/ Pallet Loader (1209)AHM934Functional Specification for a Narrow Body Lower Deck Single Platform Loader (1211)AHM934A Functional Specification for a Single Platform Slave Loader Bed for Lower DeckLoading Operations (1213)AHM936Functional Specification for a Container Loader Transporter (1215)AHM938Functional Specification for a Large Capacity Freighter and Combi Aircraft TailStanchion (1218)AHM939Functional Specification for a Transfer Platform Lift (1220)AHM941Functional Specification for Equipment Used for Establishing the Weight of aULD/BULK Load (1222)AHM942Functional Specification for Storage Equipment Used for Unit Load Devices (1224)AHM950Functional Specification for an Airport Passenger Bus (1225)AHM951Functional Specification for a Crew Transportation Vehicle (1227)AHM953Functional Specifications for a Valuable Cargo Vehicle (1229)AHM954Functional Specification for an Aircraft Washing Machine (1230)AHM955Functional Specification for an Aircraft Nose Gear Towbar Tractor (1232)AHM956Functional Specification for Main Gear Towbarless Tractor (1235)AHM957Functional Specification for Nose Gear Towbarless Tractor (1237)AHM958Functional Specification for an Aircraft Towbar (1240)AHM960Functional Specification for Unit Load Device Transport Vehicle (1242)AHM961Functional Specification for a Roller System for Unit Load Device Transportation on Trucks (1245)AHM962Functional Specification for a Rollerised Platform for the Transportation of Twenty Foot Unit Load Devices that Interfaces with Trucks Equipped to Accept Freight ContainersComplying with ISO668:1988 (1247)AHM963Functional Specification for a Baggage/Cargo Cart (1249)AHM965Functional Specification for a Lower Deck Container Turntable Dolly (1250)AHM966Functional Specification for a Pallet Dolly (1252)Chapter9—AIRPORT HANDLING GROUND SUPPORT EQUIPMENT SPECIFICATIONS(continued) AHM967Functional Specification for a Twenty Foot Unit Load Device Dolly (1254)AHM968Functional Specification for Ramp Equipment Tractors (1256)AHM969Functional Specification for a Pallet/Container Transporter (1257)AHM970Functional Specification for a Self-Propelled Potable Water Vehicle with Rear orFront Servicing (1259)AHM971Functional Specification for a Self-Propelled Lavatory Service Vehicle with Rear orFront Servicing (1262)AHM972Functional Specifications for a Ground Power Unit for Aircraft Electrical System (1265)AHM973Functional Specification for a Towed Aircraft Ground Heater (1269)AHM974Functional Specification for Aircraft Air Conditioning(Cooling)Unit (1272)AHM975Functional Specifications for Self-Propelled Aircraft De-Icing/Anti-Icing Unit (1274)AHM976Functional Specifications for an Air Start Unit (1278)AHM977Functional Specification for a Towed De-Icing/Anti-Icing Unit (1280)AHM978Functional Specification for a Towed Lavatory Service Cart (1283)AHM979Functional Specification for a Towed Boarding/De-Boarding Device for Passengers with Reduced Mobility(PRM)for Commuter-Type Aircraft (1285)AHM980Functional Specification for a Self-Propelled Petrol/Diesel Refueling Vehicle forGround Support Equipment (1287)AHM981Functional Specification for a Towed Potable Water Service Cart (1289)AHM990Guidelines for Preventative Maintenance of Aircraft Towbars (1291)AHM994Criteria for Consideration of the Investment in Ground Support Equipment (1292)AHM995Basic Unit Load Device Handling System Requirements (1296)AHM997Functional Specification for Sub-Freezing Aircraft Air Conditioning Unit (1298)Chapter10—ENVIRONMENTAL SPECIFICATIONS FOR GROUND HANDLING OPERATIONS (1301)AHM1000Chapter10—Record of Revisions (1301)AHM1001Environmental Specifications for Ground Handling Operations (1302)AHM1002Environmental Impact on the Use of Ground Support Equipment (1303)AHM1003GSE Environmental Quality Audit (1305)AHM1004Guidelines for Calculating GSE Exhaust Emissions (1307)AHM1005Guidelines for an Environmental Management System (1308)Chapter11—GROUND OPERATIONS TRAINING PROGRAM (1311)AHM1100Chapter11—Record of Revisions (1311)AHM1110Ground Operations Training Program (1312)Appendix A—References (1347)Appendix B—Glossary (1379)Alphabetical List of AHM Titles (1387)IATA Strategic Partners..............................................................................................................................SP–1。
- 1、下载文档前请自行甄别文档内容的完整性,平台不提供额外的编辑、内容补充、找答案等附加服务。
- 2、"仅部分预览"的文档,不可在线预览部分如存在完整性等问题,可反馈申请退款(可完整预览的文档不适用该条件!)。
- 3、如文档侵犯您的权益,请联系客服反馈,我们会尽快为您处理(人工客服工作时间:9:00-18:30)。
Modeling Hinting Strategies for GeometryTheorem ProvingNoboru Matsuda1 and Kurt VanLehnIntelligent Systems ProgramUniversity of Pittsburghmazda@, vanlehn@Abstract. This study characterizes hinting strategies used by a human tutor tohelp students learn geometry theorem proving. Current tutoring systems fortheorem proving provide hints that encourage (or force) the student to follow afixed forward and/or backward chaining strategy. In order to find out if humantutors observed a similar constraint, a study was conducted with students prov-ing geometry theorems individually with a human tutor. When working success-fully (without hints), students did not consistently follow the forward and/orbackward chaining strategy. Moreover, the human tutor hinted steps that wereseldom ones that would be picked by such tutoring systems. Lastly, we discov-ered a simple categorization of hints that covered 97% of the hints given by thehuman tutor.1 IntroductionAs a first step in designing an improved intelligent tutoring system for geometry theorem proving, we sought to characterize the hints given by a human tutor to stu-dents trying to prove geometry theorems. Little is known about the mechanism of effective hinting strategy [1, 2], but c urrent tutoring systems have relatively simple, inflexible hinting policies. Some tutoring systems demand that the students follow a prescribed problem solving strategy, such as forward or backward chaining [3], so their hints are always aimed at the next step taken by the prescribed strategy. Other tutoring systems accept any correct inference even if it is not on an ideal solution path [4], but when a student reaches an impasse, the tutor provides a hint on the next step that is a strict backward or forward inference no matter what assertions the st udent has made so far. Not only are the steps targeted by hints often quite inflexibly chosen, the hints themselves are usually a simple human-authored sequence that proceeds from general hints to specific hints, and usually culminates in a “bottom out” hint that describes exactly what the student should enter. We hypothesize that human tutors 1 This research was supported by NSF Grant 9720359.P. Brusilovsky et al. (Eds.): UM2003, LNAI 2702, pp.373-377, 2003© Springer-Verlag Berlin Heidelberg 2003have less rigid hinting policies, and this might cause increased learning.This paper tests the first conjecture by characterizing the hinting strategy of a single human tutor.2. The studyNine students were randomly selected from a Japanese middle school. Three ge-ometry proof-problems were used. Two problems were construction problems, which require students to draw additional lines by compasses and straightedges to complete a proof. Each student solved problems individually while thinking out aloud. The tutor was asked to provide hints only when the students could not otherwise proceed. The sessions were videotaped and transcribed. The students’ utterances were segmented so that a single segment corresponds to a proof step or a response to the tutor’s as-sistance. The tutor’s utterances were segmented so that a single segment corresponds to a hint. The following sections present an analysis of these protocol data.3. Students’ Problem Solving StrategiesIn order to determine whether students followed the forward and/or backward chaining strategies prescribed by tutoring system for theorem proving, we located individual students’ utterances in a proof tree and observed a pattern of progress in their proof. As an example, Fig. 1 shows a chronological progress of a student’s reasoning. The goal to be proven is shown at the top of the tree, with the givens at the bottom. A branching link shows a conjunctive justification. Nodes with a rectangle show the propositions that this student asserted. The numbers on their shoulder show the order of assertion. Since the proposition Bx//AP is a premise for both ∠BxM=∠APM and ∠PAM=∠MBx, the first assertion is located on two places.As shown in the figure, this student built up a proof neither in a strict forward chaining nor in a strict backward chaining manner. Rather she seems to assert facts (i.e., propositions) that were eventually recognized. This opportunistic ordering is not peculiar to this particular student. All students participating in our study showed the same behavior.4. Topics of Hint EventsWe observed 31 hint events, each consisting of a sequence of hints on the same topic. They were categorized into 4 types of hint events; (a) 10 hint events for a next step, (b) 14 hint events for a justification of proposition that the student had just me n-tioned, (c) 3 hint events for a geometry construction, (d) 1 hint event to get started on a proof, and (e) 3 hint events t hat do not fall under any of these types. Because tutor-ing systems often follow rigid policies when selecting the target step for a next -step hint, we analyzed the 10 next -step hint events in more detail.∠APM = ∠BQM∠BQM =∠BxMBMxFig. 1. A typical progress of student’s input over a proof treeIf we define a step to be applying a postulate to some premises and producing a conclusion, then the human tutor always provided a next-step hint on a single step (as opposed to discussing a generic strategy and no steps). Steps can be categorized by which elements (premises, conclusions) have been mentioned already by the student or tutor. In particular, let us use the first two letters of the classification to show whether the conclusion is asserted (C1) or not asserted (C0), and the second two let-ters for whether all the premises are asserted (Pa), none are asserted (P0), only some of the prem ises are asserted (Ps), or all but one premises are asserted (P1). Table 1 shows the results of applying this classification to the protocol data. It indicates the number of times a step was chosen as target (first row) and the number of steps avail-able at the time a next -step help event began (second row).The human tutor always chose either C0Pa or C0P1 as a target of a next -step hint event. Several existing tutoring systems, such as GPT [3], ANGLE [4], and CPT [5], choose target steps that would be picked by forward or backward chaining, whichmeans either C0Pa or C1P0. Clearly, the human tutor’s target steps seldom agreed with those that would be chosen by these tutoring systems.Table 1. Frequency of motivation of hinting in the ‘next step’ hint events5. A Classification of HintsSo far, we have di scussed only hint events and their targets, but not the hints that comprise hint events. In order to understand the structure of human tutoring better, this section categorizes the hints from the hint-events for justifications, next-steps, and the first step of the proof. There were 90 hints observed in these 25 hint events.The individual hints were organized into a Cartesian product with respect to the fo-cus and format of the hint. There are four categories regarding the focus of hint: (1) a hint on a whole application of a postulate (e.g., “Remember if two sides of triangle are equal, then the base angles are also equal”), (2) a hint on a premise of a postulate ap-plication (e.g., “If you want to prove these two angles are equal, what should be true among these two segments?”), (3) a hint on a conclusion of a postulate application (e.g., “What can you conclude about the base angles in a triangle with two equal sides?”), and (4) a hint on a proposition apparently involved in a postulate applic ation but not mentioning it explicitly (e.g., “Can you say anything about these two seg-ments?”).We observed five different forms of hint; (1) a direct exhibition, (2) a question as k-ing a whole postulate/proposition, (3) a question asking about a relationship in the proposition, (4) a question asking about the elements involved in a proposition, and (5) mentioning or pointing to a related c onfiguration in the problem figure.As an illustration of this Cartesian product categorization, Table 2 shows all possi-ble hints for a proof step that invokes the theorem of isosceles triangle (i.e., if two sides of a triangle are equal, then the base angles are also equal).We could classify 87 hints (out of 90; 97%) with the coding schema shown in Table 2. The parenthesized num bers in Table 2 shows the number of hints in each category.Table 2. The type of hints for a next-step hint6. ConclusionThe analysis of protocol data gathered from students in middle school has shown several aspects of hinting in a learning context where the tutor acts as a helper for students to overcome an impasse.We found that students tend to make opportunistic assertions that follow neither a strict forward nor backward chaining order.Accepting their reasoning style might be beneficial for students, but it requires that the tutoring system be more complex so that it can provide an appropriate hi nt de-pending on the students’ reasoning. We discovered that human tutors prefer to hint steps where one or more premises have been mentioned, although not necessarily recently, and the conclusion has not been me ntioned. It is not clear yet how the tutor decides which step to pick when there are several that meet this criterion. The human tutor’s policy for choosing target steps does not correspond to the policies of existing tutoring systems for theorem proving, but it might be easy to modify such systems to follow the human tutor’s policy.Moreover, 97% of the hints observed in our study fell into a simple Cartesian pro d-uct categorization. This categorization appears amenable to incorporation in the hint generation module of a tutoring system.References1. Hume, G., J. Michael, A. Rovick, and M. Evens, Hinting as a tactic in one-on-onetutoring. Journal of the Learning Sciences, 1996. 5(1): p. 23-47.2. DiPaolo, R.E., A.C. Graesser, D.J. Hacker, and H.A. White, Hints in Human andComputer Tutoring, in The impact of media on technology of instruction, M. Rabi-nowitz, Editor. 2002, Erlbaum: Mahwah, NJ.3. Anderson, J.R., C.F. Boyle, and G. Yost, The geometry tutor. Proceedings of theInternational Joint Conference on Artificial Intelligence, 1985: p. 1-7.4. Koedinger, K.R. and J.R. Anderson, Reifying implicit planning in geometry: Guide-lines for model-based intelligent tutoring system design, in Computers as cognitive tools, S.P. Lajoie and S.J. Derry, Editors. 1993, Lawrence Erlbaum A ssociates: Hills-dale, NJ. p. 15-45.5. Scheines, R. and W. Sieg, Computer Environments for Proof Construction. Interac-tive Learning Environments, 1994. 4(2): p. 159-169.。