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1.
Mercury is the target of two space missions: MESSENGER, which carried out its first and second flybys of Mercury on January 14, 2008 and October 6, 2008, and the ESA/JAXA space mission BepiColombo, scheduled to arrive at Mercury in 2020. The preparation of these missions requires a good knowledge of the rotation of Mercury.  相似文献   
2.
知识经济时代图书馆的地位更加重要,对图书馆员也提出了新的要求,因此,搞好图书馆人力资源管理势在必行。通过分析了图书馆人力资源管理的现状及存在的问题,提出和强调了图书馆在人力资源管理方面要以人为本,引入竞争机制、激励机制的新模式。  相似文献   
3.
Since the 1980s a trend has emerged to contain the cost of space missions, which has favored trials in the construction and launch of small satellites. This effort has considerably reduced the cost of the satellites because the construction process uses both traditional components and important technological innovations. There have also been market openings for small satellites, both within the telecommunication sector and for scientific missions and those related to Earth observation. This paper contains the results of a survey of the largest manufacturers of small satellites in Europe and investigates how far (if at all) they have changed the structure of the European space industry. It finds that, through the acquisition of small satellite manufacturers, traditional large companies operating in the field of space in Europe have secured for themselves important technological innovations and market opportunities, while maintaining their oligopolistic position.  相似文献   
4.
以空调制冷故障考核仿真系统为例,介绍空调制冷仿真实验实训系统在国家级试点专业——供热通风与空调工程技术专业教学中的作用。该系统重点解决了空调制冷故障的考核仿真模拟,阐明了仿真技术对于高职高专学生培养的重要性和可行性。仿真实验实训技术在技能型人才培养中将有很大的发展空间。  相似文献   
5.
本文介绍了病态方程组的判定方法,结合一项具体工程指出了病态方程组对工程实践的影响,分析了出现病态方程组的原因,强调了病态方程组判定对工程实践的作用。  相似文献   
6.
通过对我国大学生野外生存生活训练开展的现状与发展趋势分析,探讨在高职院校开展野外生存生活训练的可行性。开展野外生存生活训练可以完善体育课程体系,拓展体育课程内容,使学生掌握有关野外生存的基本知识和基本能力,促进高职学生身心健康和谐发展。  相似文献   
7.
Space deployable structures with large calibers, high accuracy, and large folding ratios are indispensable equipment in the aerospace field. Given that the single-DOF 3RR-3RRR deployable unit cannot be fully folded, this study proposes a 3UU-3URU deployable unit with two kinds of DOF: folding movement and orientation adjustment. First, based on the G-K formula, the DOF of the 3UU-3URU unit is analyzed. Then, the 3UU-3URU unit is used to construct a deployable truss antenna with a curved surface, and the DOF of the whole deployable antenna containing multiple 3UU-3URU units is calculated. The structural design of a deployable antenna with two loops is carried out with specific parameters and geometric relations. Next, a DOF simulation of a basic combination unit composed of three 3UU-3URU units is performed. Finally, a prototype of the basic combination unit is manufactured, and the DOF of the mechanism is experimentally verified.  相似文献   
8.
    
《中国航空学报》2021,34(3):200-224
Unmanned Aircraft Systems (UASs) have advanced technologically and surged exponentially over recent years. Currently, due to safety concerns, most civil operations of UAS are conducted in low-level uncontrolled area or in segregated controlled airspace. As the industry progresses, both operational and technological capabilities have matured to the point where UASs are expected to gain greater freedom of access to both controlled and uncontrolled airspace. Extensive technical and regulatory surveys have been conducted to enable the expanded operations. However, most surveys are derived from the perspective of UAS own operating mechanism and barely consider interactions of their non-segregated activities with the Air Traffic Management (ATM) system. Hence, to fill the gap, this paper presents a survey conducted from the perspective of Air Navigation Service Provider (ANSP), which serves to accommodate these new entrants to the overall national airspace while continuing flight safety and efficiency. The primary objectives of this paper are to: (A) describe what typical ANSP-supplied UAS Traffic Management (UTM) architecture is required to facilitate all types of civil UAS operations; (B) identify three major ANSP considerations on how UAS can be accommodated safely in civil airspace; (C) outline future directions and challenges related with UAS operations for the ANSP.  相似文献   
9.
评价航天测控方案中的测控任务可靠性需要高效的方法,解析法和直接仿真都不能满足该要求.在介绍测控任务模型及其可靠性直接仿真法的基础上,基于不交化最小割集设计了实现近似零方差重要抽样的方法,并给出不交化最小割集的获取算法.通过案例分析,得出不交化最小割集最大获取数量越大,仿真收敛性越好,但相应地耗时也越多的结论.因此,实际应用中,需要在不交化最小割集获取数量与仿真时间二者间进行权衡.  相似文献   
10.
利用不同时刻系统测量噪声具有独立同分布的特点,对脉冲响应进行相关处理,可以提高信噪比。为解决传统的基于脉冲响应的模态辨识算法的辨识精度问题,用某点脉冲响应同参考点响应之间的相关函数代替该点的脉冲响应以形成基于脉冲响应相关函数的模态辨识算法,并从理论上证明脉冲响应相关函数算法的辨识精度优于传统的脉冲响应算法。通过对一个四自由度系统模态频率和阻尼比的仿真辨识,验证了脉冲响应相关函数辨识算法的有效性。  相似文献   
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