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522.
L.H. Deng Z.Q. Qu K.R. Wang X.B. Li 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2012
In this paper, the phase asynchrony between coronal index and sunspot numbers is investigated. It is found that, (1) the sunspot numbers begin one month earlier than coronal index, which should mathematically lead to phase asynchrony between them but with a slight effect; (2) the 11-year Schwabe cycle is the only one period with statistical significance for coronal index and sunspot numbers, and the difference between the length of the Schwabe cycle of them should also lead to phase asynchrony between them; (3) although coronal index and sunspot numbers are coherent in low-frequency components corresponding to the 11-year Schwabe cycle, they are asynchronous in phase in high-frequency components; (4) their different definitions and physical meanings may be a major reason why there is a phase asynchrony between them. 相似文献
523.
脉冲测量雷达卫星标定方法研究 总被引:2,自引:0,他引:2
对脉冲测量雷达卫星标定方法的原理和工程应用等问题进行了研究,提出了标定模型和方法,分析了雷达跟踪能力和卫星定轨保障等工程应用问题,并对标定效果进行了仿真验证。 相似文献
524.
航空自组网(AANET)是一种节点高速运动、网络拓扑持续快速变化的新型自组织网络。针对AANET的特点,提出了一种新的时分多址(TDMA)时隙分配方法。首先,根据高动态航空网络环境中媒体访问控制(MAC)协议的特点,推导出可以共用一个时隙进行通信的连接集合的计算方法,并建立了面向连接的空间复用TDMA(STDMA)时隙分配优化数学模型。然后,提出一种分布式STDMA时隙分配算法IDTA。IDTA不需要中心节点收集网络信息,分为2个同步的进程在发送节点和接收节点同时运行,而且能够根据连接的优先级按需分配时隙。最后,在OMNeT++仿真平台上建立计算机仿真模型,仿真结果显示:IDTA比其他分布式STDMA时隙分配算法更加适用于高动态的航空网络环境。 相似文献
525.
Drilling load modeling and validation based on the filling rate of auger flute in planetary sampling 总被引:1,自引:0,他引:1
Some type of penetration into a subsurface is required in planetary sampling. Drilling and coring, due to its efficient penetrating and cuttings removal characteristics, has been widely applied in previous sampling missions. Given the complicated mechanical properties of a planetary regolith, suitable drilling parameters should be matched with different drilling formations properly. Otherwise, drilling faults caused by overloads could easily happen. Hence, it is necessary to estab-lish a drilling load model, which is able to reveal the relationships among drilling loads, an auger's structural parameters, soil's mechanical properties, and relevant drilling parameters. A concept for the filling rate of auger flute (FRAF) is proposed to describe drilling conditions. If the FRAF index under one group of drilling parameters is less than 1, this means that the auger flute currently removes cuttings smoothly. Otherwise, the auger will be choked with compressed cuttings. In dril-ling operations, the drilling loads on the auger mainly come from the conveyance action, while the drilling loads on the drill bit primarily come from the cutting action. Experiments in one typical lunar regolith simulant indicate that the estimated drilling loads based on the FRAF coincide with the test results quite well. Based on this drilling load model, drilling parameters have been opti-mized. 相似文献
526.
Polypropylene fiber and expansive agent are used in airport concrete to improve its shrinkage cracking resistance and mechanical properties. The concrete specimens with amount content of polypropylene fiber or expansive agent or both of them are prepared. The morphology of specimens is observed by scanning electron microscope, the time when the first crack occurred is recorded through slap test, and the mechanical properties such as compressive strength and impact energies of concrete are measured. The results show that polypropylene fiber in concrete can reduce the shrinkage and delay the first crack, improve the impact resistance obviously, and improve the compressive strength slightly. Expansive agent can compensate the shrinkage and reduce cracks of concrete pavement markedly, and improve the mechanical properties of concrete pavement slightly. The study provides recommendations for cracking control of airport concrete pavement in the future. 相似文献
527.
Zhongchao Liang Haibo Gao Liang DingZongquan Deng Jianjun Qu 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2014
To investigate and improve the mobility of the Lunar Roving Vehicle (LRV), it is necessary to consider the mechanical properties of the interaction between the wheels and the ground. In this paper, a new solution method, the forced-slip solution method, which uses a semi-empirical approach, was presented. That is, given the wheel’s vertical load and drawbar pull or driving torque as known input values, the unknown slip ratio can be resolved. The alternative method involves predicting the mechanics for a given slip ratio. The proposed method correlates better with actual wheel movements, and by studying a single wheel, this solution method can also be used to resolve the mechanical properties of the front and rear wheels in a four-wheel-drive (4WD) LRV configuration. It can also be used to consider the multi-pass effect of the rear wheels on lunar soil. The calculation results show that the 4WD LRV driving efficiency varies with the position of the center of mass. Thus, the LRV driving efficiency can be optimized by adjusting the position of its center of mass. 相似文献
528.
J. Wang J.S. Deng J. Cui L. Cao Y.L. Qiu J.Y. Wei 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2011
The potential effect of the lunar exosphere on the near-ultraviolet sky background emission is predicted for Lunar-based Ultraviolet Telescope (LUT: a funded Chinese scientific payload for the Chang’e-III mission). Using the upper limit on the OH concentration inferred from the recent MIP CHACE results, our calculations show that the sky brightness due to the illuminated exosphere is <8.7 photons−1 cm−2 arcsec−2 within the wavelength range 245–340 nm. By evaluating the signal-to-noise ratios of observations of an AB = 13 mag point source at a series of sky background levels, our analysis indicates that the detection performance of LUT can be moderately degraded by the lunar exosphere emission in most cases. An AB = 13 mag point source can still be detected by the telescope at a signal-to-noise ratio more than 8 when the OH concentration is less than 2 × 108 molecules cm−3. However, the effect on the performance is considerable when the exosphere is as dense as suggested by CHACE. 相似文献
529.
530.