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971.
T. Ma J. Chang N. Zhang M.S. Cai Y.Z. Gong H.S. Tang R.J. Zhang N.S. Wang M. Yu J.P. Mao S.B. Su Z. Fang R. Xu Y.M. Hu Q. Gu Y.L. Zhou A.A. Xu L.G. Liu 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2008
Gamma-ray spectrometer (GRS) is included in the payload of Chinese first lunar mission Chang’E-1 that will be launched in 2007. Specific objectives of the GRS are to map abundance of O, Si, Fe, Ti, U, Th, K, and perhaps, Mg, Al, and Ca to depths of about 20 cm. There are remarkable advantages for GRS application to remote sensing elemental materials over the entire lunar surface: large effective area and good ability for background rejection. We will describe the design of GRS and present its performance in this paper. Moreover, the GRS calibration will also be introduced. 相似文献
972.
G. S. Zaslavskiy V. A. Stepan’yants A. G. Tuchin A. V. Pogodin E. N. Filippova A. I. Sheikhet 《Cosmic Research》2014,52(5):353-364
The results of refining the parameters of the Spektr-R spacecraft (RadioAstron project) motion after it was launched into the orbit of the Earth’s artificial satellite in July 2011 showed that, at the beginning of 2013, the condition of staying in the Earth’s shadow was violated. The duration of shading of the spacecraft exceeds the acceptable value (about 2 h). At the end of 2013 to the beginning of 2014, the ballistic lifetime of the spacecraft completed. Therefore, the question arose of how to correct the trajectory of the motion of the Spektr-R satellite using its onboard propulsion system. In this paper, the ballistic parameters that define the operation of onboard propulsion system when implementing the correction, and the ballistic characteristics of the orbital spacecraft motion before and after correction are presented. 相似文献
973.
A mechanical model of the line-of-sight stabilization system for the optical device mounted on a movable carrier vehicle is considered. The nonlinear Lagrange equations of motion for a four-axis gimbal suspension are derived. Requirements on design and parameters for the passive line-of-sight shock absorption system of the optoelectronic payload are worked out. 相似文献
974.
N. F. Averkiev S. A. Vlasov V. V. Salov V. V. Kiselev 《Russian Aeronautics (Iz VUZ)》2016,59(4):474-479
A method of finding the aircraft optimal route by means of task-oriented replacement of the functional being optimized is proposed. 相似文献
975.
976.
CW radar signals and processors are discussed. The use of the periodic ambiguity function (PAF) to analyze the delay-Doppler performance of CW signals and their corresponding correlation receivers, is extended to include weight function effects. This work provides tools which can predict the delay-Doppler response of almost any phase-coded CW radar. Examples demonstrate that a combination of CW signals having perfect periodic autocorrelation, a matched reference signal with a large number of modulation periods and a smooth weight function, can create a delay-Doppler response with extremely low sidelobes, strongly resembling the response of a coherent pulse train 相似文献
977.
Franceschetti G. Mazzeo A. Mazzocca N. Pascazio V. Schirinzi G. 《IEEE transactions on aerospace and electronic systems》1991,27(2):343-353
A parallel architecture especially designed for a synthetic-aperture-radar (SAR) processing algorithm based on an appropriate two-dimensional fast Fourier transform (FFT) code is presented. The algorithm is briefly summarized, and the FFT code is given for the one-dimensional case, although all results can be immediately generalized to the double FFT. The computer architecture, which consists of a toroidal net with transputers on each node, is described. Parametric expressions for the computational time of the net versus the number of nodes are derived. The architecture allows drastic reduction of the processing time, preserving elaboration accuracy and flexibility 相似文献
978.
I M Shirobokova N S Pechurkin 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2001,27(9):1593-1598
A mathematical model was used to study the response of ecosystems of different structures to external impact. The response was measured as a sensitivity coefficient: the magnitude of the system's response vs. the change of the factor in the inflow. The formula has been obtained to calculate the sensitivity coefficient for ecosystems containing different numbers of trophic links. The derived sensitivity coefficients demonstrate that the degree of compensation for the external impact can differ depending on the type of system regulation and the length of the trophic chain. E. g. the sensitivity coefficient decreases with complexity of trophic links in an ecosystem for top-down controlled systems and impact of degree of openness on sensitivity e.g. closed ecosystems show higher sensitivity then fully open ecosystem to impacts also bottom-up control system show less sensitivity then top-down. Grant numbers: N99-04-96017, N25. 相似文献
979.
The paper deals with the problems of deformation and damage of the materials of structural components of complex shape subjected to cyclic loading by convective thermal flows which induces in them non-uniform temperature and thermal-stress fields. A new testing technique is proposed employing the use of models of different shape and, in particular, those of wedge-shape prism type. Variation of the level of thermal stresses and temperatures, as well as of the degree of non-uniformity of temperature and stress fields, is effected by changing the models dimensions under the given thermal loading conditions. It is shown that in simultaneous testing of a great number of models of different size it is possible to obtain information sufficient for deriving the equations of the material state under complex thermo-mechanical loading in aggressive gas flows. Examples are presented of practical application of the technique proposed. 相似文献
980.