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141.
142.
I. Kutiev P. Marinov A. Belehaki B. Reinisch N. Jakowski 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2009
To improve the accuracy of the real time topside electron density profiles given by the Digisonde software a new model-assisted technique is used. This technique uses the Topside Sounder Model (TSM), which provides the plasma scale height (Hs), O+–H+ transition height (HT), and their ratio Rt = Hs/HT, derived from topside sounder data of Alouette and ISIS satellites. The Topside Sounder Model Profiler (TSMP) incorporates TSM and uses the model quantities as anchor points in construction of topside density (Ne) profiles. For any particular location, TSMP calculates topside Ne profiles by specifying the values of foF2 and hmF2. In the present version, TSMP takes the F2 peak characteristics – foF2, hmF2, and the scale height at hmF2 – from the Digisonde measurements. The paper shows results for the Digisonde stations Athens and Juliusruh. It is found that the topside scale height used in Digisonde reconstruction is less than that extracted from topside sounder profiles. Rough comparison of their bulk distributions showed that they differ by an average factor of 1.25 for locations of Athens and Juliusruh. When the Digisonde scale heights are adjusted by this factor, the reconstructed topside profiles are close to those provided by TSM. Compared with CHAMP reconstruction profiles in two cases, TSMP/Digisonde profiles show lower density between 400 and 2000 km. 相似文献
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144.
弓高弦长法测量圆直径的研究 总被引:1,自引:0,他引:1
王明新 《沈阳航空工业学院学报》2000,17(1):67-69
弓高弦长法测圆直径的一个重要问题,是如何选取最佳测量点。本文从误差的传递着手,严密推证了弓高及弦长测量的标准差取不同值时最佳测量点的位置。 相似文献
145.
以玻璃纤维为原料,采用特殊的三维织造工艺,织制经向剖面为矩形的新型三维夹芯织物。以环氧树脂E-51、9055型固化剂组成树脂基体体系,采用手糊成型工艺将上述机织物复合制成三维织物夹芯复合材料。对高度为10、20及30 mm的三维织物夹芯复合材料的力学性能进行研究,重点分析夹芯层高度对材料压缩与弯曲性能的影响。结果表明:随着夹芯层高度的增加,材料的压缩强度与模量逐渐下降,弯曲强度逐渐上升,弯曲模量逐渐下降,其中纬向弯曲强度明显大于经向。 相似文献
146.
《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2013,52(2):262-271
In this paper we review the lunar laser ranging conducted by the laser altimeter (LALT) on board the KAGUYA lunar explorer (2007–2009). Five aspects of LALT measurements are described: (1) General operational history, (2) Laser shot and data statistics, (3) Revisions to LALT topographic data, (4) Variations in laser output energy, and (5) Peak height analysis of laser echo pulses. LALT was able to range to the lunar surface despite some troubles with respect to laser output energy in the middle of the KAGUYA mission. The time series topographic data set was revised (Ver. 2) by incorporating new lunar gravity model based on KAGUYA and other historical lunar satellite’s orbit data, along with other improvements, for example by incorporating the accurate position of the laser collimator on board the KAGUYA; however, more than half of the acquired range data could not be converted properly due to problems with orbit accuracy during the extended phase of the mission. The spherical harmonic coefficients and the basic lunar figure parameters derived from LALT_LGT_TS agree very well with LRO-LOLA and the Chang’E-1 LAM model. It is possible that partial failure to the laser diode was responsible for the gradual degradation of laser power (0.835 mJ per million shots) and the rapid decrease that occurred over April 9–14, 2008. The laser power also proved to be extremely sensitive to the temperature of the laser oscillator. The peak height ratio – that is peak height telemetry data divided by calculated ratio – is about 19% on average using the mean slope and albedo data from LALT and Spectral Profiler on KAGUYA space craft, respectively, which suggests the performance of peak height measurement is more than 1/5 for more than 70 km altitude, if compared with calculated one. The peak height ratio may be better if we take the effect of small scale topography within a footprint into account. 相似文献
147.
A.D. Akchurin V.V. BochkarevE.Yu. Ryabchenko O.N. Sherstyukov 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2009
The paper describes a new technique that improves precision of the virtual height measurements by a coherent pulse sounding of the ionosphere. Proposed technique is based on the method of maximum likelihood that matches expected and observed spectral domain signatures of the signal intermixed with the noise. Computer simulations show that our technique allows measurements of the echo virtual height with ∼100 m precision even at a much coarser step of the height sampling in the sounder. In experiment, we expect an average 300 m precision of the virtual height measurements for single echoes received during periods of little spread due to ionospheric irregularities. 相似文献
148.
T.L. Gulyaeva 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2011
The International Reference Ionosphere model extended to the plasmasphere, IRI-Plas, presents global electron density profiles and total electron content, TECiri, up to the altitude of the GPS satellites (20,000 km). The model code is modified by input of GPS-derived total electron content, TECgps, so that the topside scale height, Hsc, is obtained minimizing in one step the difference between TECiri and TECgps observation. The topside basis scale height, Hsc, presents the distance in km above the peak height at which the peak plasma density, NmF2, decays by a factor of e (∼2.718). The ionosonde derived F2 layer peak density and height and GPS-derived TECgps data are used with IRI-Plas code during the main phase of more than 100 space weather storms for a period of 1999–2006. Data of seven stations are used for the analysis, and data from five other stations served as testing database. It is found that the topside basis scale height is growing (depressing) when the peak electron density (critical frequency foF2) and electron content are decreased (increased) compared to the median value, and vice versa. Relative variability of the scale height, rHsc, and the instantaneous Hsc are inferred analytically in a function of the instantaneous foF2, median fmF2 and median Hmsc avoiding a reference to geomagnetic indices. Results of validation suggest reliability of proposed algorithm for implementation in an operational mode. 相似文献
149.
基于轴对称N-S方程和7组分18化学反应对20~90 km再入高度下RAMC-Ⅱ飞行器周围流场进行数值模拟,并对算法进行验证。计算了电子密度分布,同时给出了不同再入高度下的碰撞频率、平均温度及总压强分布。通过分析得出电子密度随再入高度的增加先增加后减小,同一再入高度下电子密度沿轴向方向减小,沿着垂直于飞行器表面方向符合高斯分布。最大碰撞频率随着再入高度增加而减小,同一再入高度下沿轴向方向减小。同一再入高度下最大平均温度沿着轴向距离逐渐减小。最大总压强随着再入高度的增加而减小,同一再入高度下最大总压强沿着轴向距离逐渐减小。 相似文献
150.