用于小行星探测的离子推力器技术研究

随着我国深空探测技术的发展,近地小行星的探测已列入实施计划,后续的深空探测活动也在规划中。研究基于国外深空探测技术对离子推力器的技术需求以及应用情况,针对我国小行星探测离子推进技术的应用进行了分析与研究。着重阐述了满足我国首颗近地小行星探测使命的离子推力器研究,以现有成熟离子推力器为基础,对其进行性能提升研究。性能改进后的离子推力器,能够实现40和60mN两种工作模式,通过组合应用,可实现40、60、80、100和120mN共5种推力模式,以满足小行星探测的需求。     

一种挖掘意外规则的方法

采用不确定规则形式表示发现知识和用户的领域知识,提出了发现规则相对于领域规则的前件一致度的概念及其计算方法,在此基础上给出了3种规则意外形式;分析了规则意外度的影响因素,给出了意外性的度量函数;研究了一种意外规则的挖掘方法,该方法不受产生规则的数据挖掘算法限制。实验结果表明,该方法能够有效地遴选出意外规则。     

数据流频繁闭集的在线挖掘

基于算法LossyCounting,提出了数据流频繁闭集的在线挖掘算法LC_Closed(LossyCounting_Closed).设计了基于前缀树的频繁闭集压缩存储结构CI-forest(ClosedItemsets-forest),利用该数据结构可以快速的插入和查询闭集模式,且在处理新的事务数据时能够快速定位相关的历史闭集模式.该算法采用在线的处理方式,提高了算法的实时性.实验的结果证明该算法是有效的.      

数据聚类方法的研究与分析

聚类分析是近年来迅速发展起来的一种新兴的数据处理技术,它在许多领域有着广泛的应用,尤其是在数据挖掘领域。首先阐述了聚类分析的基本概念和分类,然后针对目前几类主要的聚类分析方法,重点分析了基于密度的DBSCAN算法,基于层次的BIRCH算法以及基于网格的Wave Cluster算法这三种具有代表性的聚类方法,分析了它们的优缺点和时间复杂度。最后提及了聚类分析方法的应用范围以及今后需要解决的问题和发展方向。     

SQL Server 2000的数据仓库解决方案

阐述了数据仓库是数据库技术的发展且可以通过OLAP和数据挖掘技术进行强大的多维数据分析,来实现决策支持功能。Microsoft公司推出的SQL Server 2000数据库管理系统提供了完整的数据仓库和OLAP的解决方案:在关系数据库基础上,用一组数据仓库组件(DTS, ANALYSS,复制,转移)来建立数据仓库。该方案提供了多维表达式语言(MDX)和多维数据的分析查询机制,能方便快捷地开发生成和部署数据仓库应用。     

回归分析数据挖掘技术

统计类数据挖掘技术作为数据挖掘技术中较为成熟的一个分支,它采用统计学的方法与数据挖掘的原理对目标数据进行分析和处理。文中针对其中的回归分析技术的原理及应用进行了探讨。     

Encounter trajectories for deep space mission ASTER to the triple near Earth asteroid 2001-SN263. The laser altimeter (ALR) point of view

In cooperation with Russia, the Brazilian deep space mission ASTER plans to send a small spacecraft to investigate the triple asteroid 2001-SN263. The nearest launch opportunities for this project include June 2022 and June 2025. One main exploration campaign is being planned with focus on the largest asteroid (Alpha). Among the instruments under development, a laser altimeter (named ALR) was preliminarily designed and presented in 2010–2011. Many studies to define mission and instruments requirements were performed aiming at the characterization of important issues for the successful realization of the mission. Among them, the identification of a suitable trajectory that could be followed by the ASTER spacecraft in the encounter phase, when the main campaign will take place. This paper describes the effort undertaken with focus on the laser altimeter operation. Possible encounter trajectories were modelled and simulated to identify suitable approach parameters and conditions allowing the accomplishment of the intended investigation. The simulation also involves the instrument operation, considering approach geometry, attitude, relative motion, time/date, and the dynamics of the main asteroid. From the laser altimeter point of view, keeping in mind the desired coverage results (50% minimum surface coverage of asteroid Alpha, complying with horizontal and vertical resolution requirements), results point out crucial features for the encounter trajectory, like the need for a small inclination (10^-6 degrees; with respect to the asteroid's orbit), the most favourable spacecraft positioning (between the Sun and the asteroid) and pointing condition (back to the Sun), the minimum amount of achievable surface coverage (58%, focused on central areas), and the most proper time to conduct the main campaign (January 2025). Concerning the instrument, results offer refined values for divergence angle (500 to 650 μrad, half-cone), pulse repetition frequencies (from 1/20 to 1 Hz), and consequent data generation rates. A simulation tool that can use any 3D generated trajectories as input data was created for the analyses presented here. Although created for the ALR in this mission, this simple analysis tool can be adapted to other instruments in this or other missions.     

浅析数据挖掘在学生体质健康测试中的应用

通过对国内外有关数据挖掘在体育领域中应用的相关文献进行分析,认为数据挖掘能够在学生体质健康测试、国民体质监测数据处理等方面能够充分发挥其潜在的价值。针对数据挖掘技术的基本原理在学生体质健康测试领域的应用进行了研究,阐述其概念、类型及使用方法,并讨论和分析它在学生体质健康测试数据分析工作中的运用,提出基于学生体质健康测试的数据挖掘模式,从而有效地提高学生体质健康水平,为学校体育科研工作提供一些新的研究思路和方法。     

Economic assessment of high-thrust and solar-sail propulsion for near-earth asteroid mining

Asteroid mining has the potential to greatly reduce the cost of in-space manufacturing, production of propellant for space transportation and consumables for crewed spacecraft, compared to launching the required resources from the Earth’s deep gravity well. This paper discusses the top-level mission architecture and trajectory design for these resource-return missions, comparing high-thrust trajectories with continuous low-thrust solar-sail trajectories. The paper focuses on maximizing the economic Net Present Value, which takes the time-cost of finance into account and therefore balances the returned resource mass and mission duration. The different propulsion methods are compared in terms of maximum economic return and sets of attainable target asteroids. Results for transporting resources to geostationary orbit show that the orbital parameter hyperspace of suitable target asteroids is considerably larger for solar sails, allowing for more flexibility in selecting potential target asteroids. Also, results show that the Net Present Value that can be realized is larger when employing solar sailing instead of chemical propulsion. In addition, it is demonstrated that a higher Net Present Value can be realized when transporting volatiles to the Lunar Gateway instead of geostationary orbit. The paper provides one more step towards making commercial asteroid mining an economically viable reality by integrating trajectory design, propulsion technology and economic modelling.     

航天器产品试验过程实时寿命及质量一致性评价技术

在航天器部组件产品试验时存在着海量闲置数据，但由于缺少有效的数据挖掘手段，型号产品的寿命和质量一致性一直得不到有效评估。本文给出了航天器部组件产品实时寿命预测方法和质量一致性评价方法的实施流程，并分析了各类退化预测建模方法和包络建模方法的适用条件。案例验证表明，实时寿命预测可以采用产品性能的实时监测信息，建立产品退化特征预测模型，实现对加速寿命的动态预测；质量一致性评价可以采用历史产品试验信息，构建成功包络线，实现对被试产品是否满足质量一致性要求的有效判别。