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排序方式: 共有825条查询结果,搜索用时 31 毫秒
781.
Fan Zhao Dijie Li Yasir Arfat Zhihao Chen Zonglin Liu Yu Lin Chong Ding Yulong Sun Lifang Hu Peng Shang Airong Qian 《Acta Astronautica》2014
Skeletal unloading results in decreased bone formation and bone mass. During long-term space flight, the decreased bone mass is impossible to fully recover. Therefore, it is necessary to develop the effective countermeasures to prevent spaceflight-induced bone loss. Hindlimb Unloading (HLU) simulates effects of weightlessness and is utilized extensively to examine the response of musculoskeletal systems to certain aspects of space flight. The purpose of this study is to investigate the effects of a 4-week HLU in rats and subsequent reloading on the bone mineral density (BMD) and mechanical properties of load-bearing bones. 相似文献
782.
在旋转状态下,研究了涡轮内冷蛇形通道的非稳态换热特性.实验主要针对旋转状态下,通道内流量的变化和系统旋转速度的变化来进行的.结果表明:对于旋转通道的非稳态过程,换热系数的变化呈波动变化过程,且主要发生在实验参数变化的阶段.加速旋转时,角加速度力的作用会加强进气通道前缘面的换热,而降低后缘面的;减速旋转时,情况相反.而且,角加速度力的作用效果容易在旋转开始变化的时刻显现.当旋转速度在2个值之间往复时,换热系数变化呈现滞后环状,旋转速度越高滞后环越大. 相似文献
783.
环路热管温度波动现象的实验分析 总被引:8,自引:3,他引:5
对实验中观察到的环路热管温度波动现象进行了描述和解释.实验发现,较小热载荷和较大热载荷下环路热管容易出现温度波动现象.对于蒸发器充满液体的启动情况,小热载荷启动容易出现毛细芯内的工质蒸发现象,芯内蒸发继而引起冷凝器入口处的温度波动,并且最终导致可变热导区的稳态工作温度偏高.冷凝器出口处的温度波动现象产生的原因是工质充装量和储液器容积的不匹配,冷凝器出口的温度波动可以通过对工质充装量的控制来避免. 相似文献
784.
一种XML相似重复数据的清理方法研究 总被引:5,自引:0,他引:5
针对半结构化数据XML在数据清理中的重要性,研究了如何清理XML相似重复数据,主要工作有:提出一种有效的XML相似重复数据清理方法,该方法具有较强的适应性,任何XML相似检测算法都适用于此;给出一种基于树编辑距离的相似检测算法,该算法能有效地检测XML相似重复数据;采用树编辑距离的上下限优化基于树编辑距离的相似检测算法,避免了不必要的树编辑距离计算,降低了相似检测计算的复杂度,提高了运算效率.此工作为研究XML相似重复数据清理打下基础. 相似文献
785.
Xin Liu Shubi Zhang Qiuzhao Zhang Nan Ding Wei Yang 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2019,63(3):1234-1252
With the Global Navigation Satellite System (GNSS) developing, the single-frequency single-epoch multiple GNSSs (multi-GNSS) relative positioning has become feasible. Since a larger number of the observed satellites make the instantaneous (single-epoch) positioning time-consuming, a proper satellite selection is necessary. Among the present methods, the satellite selection with a fixed high cut-off elevation angle (CEA) is least time-consuming. However, there is no criterion how large a fixed high CEA should be to achieve a high success rate and less time consumption. Besides, a fixed high CEA makes the number of visible satellites largely variable, which affects the success rate. Hence, a satellite selection strategy based on ambiguity dilution of precision (ADOP) is proposed. Firstly, the theoretical proof that the ADOP increases the least when removing satellites are all low-elevation-angle satellites is given, which is important to achieve the fast positioning with a high success rate. Then, the threshold is calculated for a different number of satellites and a given ADOP. The satellites are selected based on their elevation angles from high to low until of the selected satellites becomes smaller than the corresponding threshold; this method is called the extended floating CEA multi-GNSS (EF-multi-GNSS). The comparison of the single-frequency single-epoch positioning performance of the EF-multi-GNSS with the satellite selections based on a fixed low CEA (L-multi-GNSS) and a fixed high CEA (H-multi-GNSS) via the relative positioning experiments shows that: (1) the EF-multi-GNSS with a minimal number of satellites can achieve the fast positioning and a high success rate close to 100%. It can greatly reduce the time consumption of the L-multi-GNSS, by about 64.0%, by selecting 12.6 satellites of 23.4 satellites; (2) the floating CEA of EF-multi-GNSS eliminates the consideration how large a fixed high CEA should be, and a CEA larger than the fixed high CEA of the H-multi-GNSS makes it more suitable for different conditions. 相似文献
786.
787.
788.
Zegang Ding Teng Long Tao Zeng Yu Zhu 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2008,41(11):1822-1826
The deramp range migration algorithm (DRMA) for space-borne spotlight synthetic aperture radar (SAR) is presented, which is based on the two-step algorithm and range migration algorithm. The presented algorithm combines the advantages of SPECAN algorithm and range migration algorithm. Firstly, the presented algorithm performs a bulk azimuth raw data compression to achieve a pixel spacing no larger than the expected azimuth resolution of the fully focused image. Therefore, the azimuth spectral folding phenomenon is overcome. Secondly, the residual and precise focusing of the synthetic aperture radar data is achieved by applying the range migration algorithm. The space-borne SAR focusing parameters’ computation is also described in the paper. At the end of this paper, results are presented which confirm the validity of the presented algorithm. 相似文献
789.
新一代可重复使用运载器RLV(Reusable Launch Vehicle)再入时应具备自主导航的能力,其实现的关键是用机载计算机近实时或实时地生成一条满足各种约束条件的再入轨迹.根据RLV再入的特点,引入了新的假设,对再入轨迹方程进行简化处理,优化难度降低,工作量减少.另外引入次优化轨迹的概念,对控制量(迎角和滚转角)的优化分两步进行,每步只对当中一个控制量进行优化.这样处理能在很大程度上加快算法的收敛速度.仿真结果表明,只需10s左右的时间就能产生一条满足终端约束条件、控制量约束条件和加热率约束条件的次优化轨迹.其结果具有较好的工程应用价值. 相似文献
790.