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861.
Yu. A. Kovalev V. I. Vasil’kov M. V. Popov V. A. Soglasnov P. A. Voitsik M. M. Lisakov A. M. Kut’kin N. Ya. Nikolaev N. A. Nizhel’skii G. V. Zhekanis P. G. Tsybulev 《Cosmic Research》2014,52(5):393-402
The results of a large number of the antenna radiometric measurements at bands of 92, 18, 6.2, 1.35, and 1.7-1.2 cm are presented by the data of the standard telemetry system of the Spektr-R spacecraft. Both special sessions of calibration object observations in the mode of a single space radio telescope (SRT) operation and numerous observations of researched sources in the mode of the ground-space interferometer were used. The obtained results agree with the first results of Kardashev et al. (2013), i.e., within 10–15% at bands of 92, 18, and 6.2 cm and 20–25% at the band of 1.35 cm. In the main, the measurements for the eight subbands at wavelengths of 1.7-1.2 cm indicate a monotonic increase in the spectral system equivalent flux density (SEFD) of noise radiation with a frequency consistent with the calculated estimates for the discussed model. The sensitivity of the ground-space interferometer for the five subbands at wavelengths from 1.35 to 1.7 cm can be higher by a factor of 1.5, and for the three subbands from 1.35 to 1.2 cm lower by a factor of 1.5 than at the band of 1.35 cm. The SRT contribution to the interferometer sensitivity proportional to the square root of SEFD is close to the design one at the bands of 92 and 18 cm and decreases the design sensitivity approximately by a factor of 1.5 and 2 at the bands of 6.2 and 1.35 cm, respectively. These differences of implemented values from the design ones were not significantly affected the scientific program implementation. 相似文献
862.
G. Krymsky P. Krymsky Yu. Romaschenko 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》1985,5(4):15-18
The aim of this paper is to investigate processes in the magnetosphere and in particular the problems of the interaction of the solar wind with the Earth's magnetic field to produce large-scale convection, electric fields and longitudinal currents in the magnetosphere. The investigation is carried out in the frame of magnetic hydrodynamics. The reason for such an approach can be found in /1/. When calculating the transfer coefficients, the Böhm approximation is used, i.e. it is considered that the plasma in the near-equatorial part of the magnetosphere (quasiplanar geometry is used in the problem for simplification) is sufficiently turbulent that the condition ωτ ≈ 1 is valid (ω is the Larmor frequency of electrons, τ is effective time between two Quasi-collisions). The main subjects of investigation in this paper are the input near the equatorial boundary layer and the plasma layer of the magnetosphere tail. 相似文献
863.
导弹武器系统中有很多是多次使用的可修复杂系统。对于这种复杂系统,尤其是其寿命周期,预防维修时间及事后维修时间为离散分布时,其最佳预防维修周期难以用一般方法求得。针对这种情况,本文利用蒙特卡罗随机模拟法建立了系统计算模型,并通过模拟计算,得出了最佳预防维修周期的数字仿真结果。此结果可为制定导弹武器最佳修复策略提供依据。 相似文献
864.
高等工科院校会计学专业实践教学体系的构建应充分体现“强化应用、重视实践、突出创新”的人才培养思路,科学地设计出实践教学的各个环节,使实践教学体系整体贯通,在时间上全程化,在结构上层次化,在形式上多元化。 相似文献
865.
Yu.K. Chasovitin V.B. Shushkova T.N. Sykilinda P.F. Denisenko V.V. Sotsky N.E. Shejdakov 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》1985,5(7):21-24
Our empirical model of electron density (ne) for quiet and weakly disturbed geomagnetic conditions (Kp not greater 4) takes account of comparative analysis of existing models and of experimental data obtained by rockets and incoherent scatter radar. The model describes the ne distribution in the 80 to 200 km height range at low and middle latitudes, and to some extent, in the subauroral region. It is presented in analytical form thus allowing one to calculate electron density profiles for any time. The electron density distribution at 140 km depends on the season (day of the year) and on the solar zenith angle. Profile variations during the day are for one season shown. Different from other models, ours specifies the variations during sunrise and sunset and reflects the particular profile shape at night admitting the occurrence of an intermediate layer. 相似文献
866.
867.
868.
A satellite with electrodynamic stabilization system is considered. Based on the method of Lyapunov functions, sufficient conditions of the asymptotic stability of direct equilibrium position of this satellite in the orbital coordinate system under perturbing action of a gravitational moment are obtained. These conditions allow one to ensure a rational choice of parametric control coefficients depending on parameters of the satellite and its orbit. 相似文献
869.
870.
整机总体性能仿真是航空发动机及燃气轮机仿真的重要组成部分,在航空发动机及燃气轮机的设计制造和使用全寿命
周期内发挥着重要作用。综合70多年来航空发动机及燃气轮机总体性能仿真的发展成果,梳理了各时期总体性能仿真的发展历
程。从基本方法、模型精细化、求解算法和修正方法等角度,分析了国内外以部件级模型为代表的基于物理机理的总体性能仿真
方法研究现状;探讨了以人工神经网络、支持向量机和深度学习为代表的人工智能算法在总体性能仿真中的应用现状;介绍了机
载模型、机理-数据混合模型和多维度模型基本方法和主要成果。基于目前的研究成果和技术发展趋势,认为航空发动机及燃气
轮机总体性能仿真应向物理机理模型更精细化、人工智能技术更深入和应用模型构建更为规范化的方向发展。 相似文献