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221.
介绍航天容错计算机(CPU)容错的一种硬件设计方案。这种方案采用四台CPU的冗余来实现CPU的自检测,以达到CPU容错的目的。 相似文献
222.
大学教育不能忽视学生文化素质、人文精神、人格品德和价值观的培养。大学语文是人文素质教育其中的基石。文章从大学语文课程的开设意义及其发展现状和存在的问题入手,提出构建大学语文立体课程体系的对策,并对体系的构建进行了思考和分析。 相似文献
223.
理工科院校《应用写作》课程教学改革之我见 总被引:1,自引:0,他引:1
当前的理工科院校对于培养提高学生人文素质能力普遍存在重视程度不够、多口头提倡,行动力不够等问题,相应的,作为培养人文素养手段之一的应用写作课程,其开设状况也不尽如人意,存在着诸多问题。作者根据相关调查结果,结合实际教学经验,从课程安排、教学观念和方法、教材编订、课程考核方法和教师能力培养等方面提出了建议。 相似文献
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V.P. Chuprova S.K. GerasimovaV.G. Grigoryev P.A. KrivoshapkinG.F. Krymsky V.P. MamrukovaV.M. Migunov A.N. PrikhodkoG.V. Shafer G.V. Skripin Ye.Ye. SorokinS.A. Starodubtsev V.E. Timofeev 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2009
Some unknown historical facts of cosmic ray studies in the north-east of the former Soviet Union related to the Yakutsk scientific group are reported for the benefit of the international scientific community. It focuses on the founders of Yu.G. Shafer Institute of Cosmophysical Research and Aeronomy of Siberian Branch of Russian Academy of Sciences. A chronology of measurements of cosmic ray intensity variations since 1949 in Yakutia (Sakha Republic; NE Siberia) is given. In particular, for the first time the data of the first solar cosmic ray event registered at Yakutsk (GLE04), with a small ionization chamber S-2 (volume: 20 L) are presented. Moreover, the data of the large ionization chamber ASK-1 (volume: 950 L) for the 1953–2003 period useful for specialists in the field of cosmic ray variations are also shown. 相似文献
227.
通过对1000MW超超临界锅炉四级过热器出口集箱和主蒸汽管道进行试验研究,发现锅炉管道存在环缝焊接式样不合格的问题.通过对管道SA-335P122材料进行力学性能分析,并结合试验数据,提出了新的工艺流程,采用了新的焊接材料和焊接工艺,通过试验验证了焊接流程的合理性,使产品制造一次合格. 相似文献
228.
本文利用一级轻气炮实验技术,对注装梯恩梯药进行了高应变率下的动态冲击实验,对实验方法进行了改进,设计了一种新型的轻气炮延伸炮管。根据实验数据结果,得到了注装TNT装药的冲击Hugoniot参数。 相似文献
229.
The aircraft engine multi-loop control system is described and the switching control theory is introduced to solve the regulating and protecting control problems in this paper. The aircraft engine multi-loop control system is firstly described and the control problems are formulated. Secondly, the theory of the smooth switching control is devoted and a new extended scheme for the smooth switching of a switched control system is introduced. Then, for the key technologies of aero-engines switching control, a design algorithm is presented which can determine which candidate controller should be put in feedback with the plant to achieve a desired performance and the procedure to design the aircraft engine multi-loop control system is detailed. The switching performance objectives and the switching scheme are given and a family of PID controllers and compensators is designed. The simulation shows that using the switching control design method can not only improve the dynamic performance of the aircraft engine control system and reduce the switching times, but also guarantee the stability in some peculiar occasions. 相似文献
230.
Gang Li Shuren Guo Jing Lv Kanglian Zhao Zehua He 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2021,67(5):1701-1708
Short Message Communication (SMC) is a featured service of BeiDou Navigation Satellite System (BDS). After its successful deployment in 2003, Regional Short Message Communication (RSMC) service has been continuously serving China and its neighboring countries and regions, especially in life safety scenarios. In this paper, the architecture of the Global Short Message Communication (GSMC) system is proposed based on the medium earth orbit (MEO) constellation and the crosslinks of the global BeiDou navigation system (BDS-3). Three subtypes of GSMC service, i.e. positioning report, emergency search and rescue (SAR) and regular SMC are designed in accordance with the technical characteristic of integration of navigation and communication in BDS-3, which supports future wide applications of GSMC. The performance of the designed GSMC system is analyzed by numerical calculations. As BDS-3 was officially announced completion on July 31, 2020, GSMC has been providing initial service. First test results of the in orbit GSMC payloads are also presented in the paper to verify the designed capabilities. Preliminary results also show that the requirements of Global Maritime Distress and Safety System (GMDSS) can also be fulfilled. 相似文献