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1.
本文用自制的装有 BaF_2探头的高探测效率的正电子湮没寿命谱仪测量了在室温下正电子素 o-Ps 与 p-RPhG 及 m-RPhG(R=NO_2,Cl,H,CH_3,cH_3O)在20%(V/V)二氧六环水溶液中的络合形成速度常数。实验结果表明,这些o-Ps-M 络合形成速度常数 K 值均与作为配位体的 p-RPhG、m-RPhG 的碱性解离常数 K 的负对数 pK_2 呈线性函数。这表明上述瞬态络合反应满足线性自由能关系,由此可推断出上述络合反应的一些重要性质。 相似文献
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Changlong Jiang Jianping Xiong Xugang Zhang Huibo Jia Duanyi Xu 《Aerospace and Electronic Systems Magazine, IEEE》2003,18(11):31-34
Most sustained data recording systems in many real-time fields are based on tape equipments. We have developed an innovative sustained data recording system based on disk array which consists of Array Controller Module (ACM), String Controller Module (SCM) and Main Controller Module (MCM). This system has a better performance and higher reliability than the traditional tape recorder and can be used conveniently in many areas of data recording, storing, playback, and remote backup. This novel recording system has been used in radar data recorder for spacecraft orbit tracking and satellite remote sensing data recording successfully. 相似文献
3.
《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2007,39(5):661-667
Monthly median values of foF2, hmF2 and M(3000)F2 parameters, with hourly time interval resolution for the diurnal variation, obtained with DPS-4 digisonde observations at Hainan (19.4°N, 109.0°E) are used to study the low latitude ionospheric variation behavior. The observational results are compared with the International Reference Ionospheric Model (IRI) predictions. The time period coverage of the data used for the present study is from March 2002 to February 2005. Our present study showed that: (1) In general, IRI predictions using CCIR and URSI coefficients follow well the diurnal and seasonal variation patterns of the experimental values of foF2. However, CCIR foF2 and URSI foF2 IRI predictions systematically underestimate the observed results during most time period of the day, with the percentage difference ΔfoF2 (%) values changing between about −5% and −25%, whereas for a few hours around pre-sunrise, the IRI predictions generally overestimate the observational ones with ΔfoF2 (%) sometimes reaching as large as ∼30%. The agreement between the IRI results and the observational ones is better for the year 2002 than for the other years. The best agreement between the IRI results and the observational ones is obtained in summer when using URSI coefficients, with the seasonal average values of ΔfoF2 (%) being within the limits of ±10%. (2) In general, the IRI predicted hmF2 values using CCIR M(3000)F2 option shows a poor agreement with the observational results. However, when using the measured M(3000)F2 as input, the diurnal variation pattern of hmF2 given by IRI2001 has a much better agreement with the observational one with the detailed fine structures including the pre-sunrise and post-sunset peaks reproduced reasonably well. The agreement between the IRI predicted hmF2 values using CCIR M(30,000)F2 option and the observational ones is worst for the afternoon to post-midnight hours for the high solar activity year 2002. During daytime hours the agreement between the hmF2 values obtained with CCIR M(30,000)F2 option and the observational ones is best for summer season. The discrepancy between the observational hmF2 and that obtained with CCIR M(30,000)F2 option stem from the CCIR M(3000)F2 model, which does not produce the small scale structures observed in the measured M(3000)F2. 相似文献
4.
《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2005,35(10):1846-1850
Emissions from solar flares may reveal fast fluctuations, which can be attributed to small-scale injections of energetic electrons. In this paper, we perform numerical calculations of the Hα emission from a flaring atmosphere bombarded by a pulsating electron beam. We assume that the variation of the electron beam flux consists of two components: a fluctuation component and a background component. The results show that the amplitude of Hα fluctuations varies depending on the magnitude of the background flux of the electron beam. In the case of a higher background flux, the Hα fluctuations are more significant than in the case of a lower background flux. This result is compatible with the observations in which the Hα fluctuations appear preferentially near the hard X-ray maximum. 相似文献
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为解决多传感器组网系统的系统误差估计问题,基于多传感器多目标上报信息,研究并提出了一种多传感器多目标系统误差融合估计算法.算法构建了两级融合结构,即第一级对多传感器组合状态估计信息进行反馈融合以改善局部组合状态估计精度,从而间接改善系统误差的估计精度,而第二级对多目标系统误差估计信息进行融合以进一步提高系统误差的估计精度.蒙特卡洛仿真显示算法能有效融合利用多传感器多目标信息,实现多传感器系统误差的实时精确估计. 相似文献
8.
从分析舰艇编队对海作战的流程出发,在决策过程中引入多智能体系统(MAS,Multi-Agent System)理论,建立了编队协同反舰作战Agent模型.针对舰艇编队Agent协作规划过程中受资源约束产生资源占用冲突的问题,建立一种主从式结构多Agent协作规划模型,并提出一种集中与分布规划相结合的MAS协作规划方法.仿真实例表明:该方法可有效实现作战编队各Agent之间的协作与协调,保证舰艇编队在满足资源约束条件下实现预期战术目标. 相似文献
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《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》1987,7(7):19-24
The modern day scientific research balloon has historically maintained an approximate 85% success rate as launched by the USA National Scientific Balloon Facility (NSBF). Failures were across all operational phases and modes. Balloons fabricated after 1980 have met with less favorable results with catastrophic failures on ascent becoming the principle failure mode. In 1983, the USA National Aeronautics and Space Administration (NASA) conducted an intensive investigation to identify the possible causes for these failures. Although the most probable cause was identified as the balloon material, additional contributing factors were identified. One of these factors, balloon stress, was calculated using a stress equation defining only the total required thickness for launch. No model existed to predict the stress distribution in an ascending balloon. Early in 1984, NASA began the development of a stress index model to establish the relative stress magnitudes at any altitude. Studies were conducted applying this model to several hundred balloon flights. The study indicated a strong correlation between stress levels, failure rates, and the point of maximum stress coinciding with observed failure locations. In January 1985, NASA instituted a stress index design and flight specification that all NASA balloons must meet. The details and results of this work are presented. 相似文献