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611.
用Ansoft HFSS仿真软件建立了极小型氢频标磁控管微波腔模型结构,对仿真设计的微波腔塞曼频移进行了分析。当磁场引起的频移小于1.42×10-5Hz,塞曼跃迁线宽Δυz小于0.21Hz时,可得磁控管微波腔塞曼相对频移在10-14数量级。当该微波腔取Tb=T2'=0.72s,磁场的不均匀频移参量Em=-1.6×10-5rad时,磁场的不均匀相对频移在10-14数量级。 相似文献
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614.
阐述了利用有限元分析结果进行结构静强度可靠性分析的一种方法。利用工程上较为成熟的一次二阶矩法计算结构单元可靠度,用数值积分法求主要失效模式间的二阶共失效概率,然后采用0Ditlevse的二阶窄边界法计算结构体系的失效概率,最终计算结果与实际相吻合 相似文献
615.
旅客氧气面罩作为旅客氧气系统的重要组成部分,是一种常见的为旅客提供应急氧气的分氧装置,随着国产大飞机项目的深入开展,依照国际通用标准研制了一款持续气流旅客氧气面罩。由于旅客氧气面罩在民用飞机上的广泛装备,要求其必须具备优良的防火性能。针对CCAR-25-R4的第25.853条款和附录F第一部分的防火性能要求,对适航条款进行分析,通过对所研制面罩主体部分的硅胶和聚氯乙烯材料进行模拟切块制样,采用CCAR-25-R4附录F第Ⅰ部分(b)(5)的测试方法对所制备的试样进行水平燃烧试验。结果表明,面罩材料的水平燃烧试验燃烧速率为0,满足CCAR-25-R4附录F第Ⅰ部分第(a)(1)(iv)条款所规定的水平燃烧试验燃烧速率不得超过64mm/min的要求,研制的旅客氧气面罩防火性能满足适航要求。 相似文献
616.
Fossil fuel exhaustion and overdevelopment usually lead to a recession,which is worsened by the environmental pollution.So it is of high priority to develop high-efficiency energy storage device.Here,agreen and environment-friendly strategy is devised to fabricate carbon materials from biomass.By water extraction and alcohol precipitation,polysaccharide is extracted from loquat leaves.After calcining under high temperature,hierarchical porous carbon materials(HPCM)are obtained,possessing a variety of macropores,mesopores and micropores.Such ample and hierarchical pores enable the electrolyte infiltration and the buffering of the volume expansion of sulfur in repeated electrochemical reactions.The structure stability of the entire electrode can thus be well maintained.When evaluated as the scaffold for sulfur,the electrochemical performance of carbon/sulfur composite was tested.Even after 500 cycles,the reversible capacity is retained as high as 485.4 mA·h/g at the current density of 1.6 A/g.It also offers a notable rate capability,attaining the discharge capacity of 700.7 mA·h/g at 2 C.All the electrochemical performance results prove the feasibility of the proposed strategy. 相似文献
617.
TANG Mingjun 《中国航天(英文版)》2018,(1)
正At 12:12 Beijing time on January 19,a LM-11 solid launch vehicle lifted off from the Jiuquan Satellite Launch Center with Jilin 1-07 and 08 satellites and other4 small satellites.The 6 satellites entered their preset orbit precisely.This mission is another breakthrough for launching multiple satellites on one LM-11 rocket since the rocket launched 相似文献
618.
Mingming Wang Jianjun Luo Jing Fang Jianping Yuan 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2018,61(6):1525-1536
The existence of the path dependent dynamic singularities limits the volume of available workspace of free-floating space robot and induces enormous joint velocities when such singularities are met. In order to overcome this demerit, this paper presents an optimal joint trajectory planning method using forward kinematics equations of free-floating space robot, while joint motion laws are delineated with application of the concept of reaction null-space. Bézier curve, in conjunction with the null-space column vectors, are applied to describe the joint trajectories. Considering the forward kinematics equations of the free-floating space robot, the trajectory planning issue is consequently transferred to an optimization issue while the control points to construct the Bézier curve are the design variables. A constrained differential evolution (DE) scheme with premature handling strategy is implemented to find the optimal solution of the design variables while specific objectives and imposed constraints are satisfied. Differ from traditional methods, we synthesize null-space and specialized curve to provide a novel viewpoint for trajectory planning of free-floating space robot. Simulation results are presented for trajectory planning of 7 degree-of-freedom (DOF) kinematically redundant manipulator mounted on a free-floating spacecraft and demonstrate the feasibility and effectiveness of the proposed method. 相似文献
619.
Chao Chen Guobin Chang Fei Luo Shubi Zhang 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2019,63(2):857-870
In GNSS applications, carrier-smoothed-code is a widely used technique to combine code pseudo-range and carrier phase measurements. A dynamical ionospheric delay modeling method is proposed based on Kalman filter and least-squares theory. The level of the process noise is adaptively tuned along with the real-time KF state estimation, based on the online variance component estimation method. Meanwhile, the correlations of the time differenced carrier phase measurements are considered. This approach avoids overly optimistically evaluating the estimate and improves the transient accuracy of the estimates. A real GPS dataset is employed to check the performance of the proposed method under different conditions. The results show that the new algorithm can model the ionospheric delay variation well with different sampling intervals or even in ionospheric abnormal environment. The positioning accuracy can be confirmed, about 21%, 35% and 16% better are obtained in the N, E, and U direction than raw dataset. 相似文献
620.