共查询到20条相似文献,搜索用时 0 毫秒
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The performance of Earth observation satellites is usually analyzed by real data or system simulation, which is accurate but not systematic. Modelling satellite service systems with queueing theory and analysing the performance statistics systematically will provide a useful guide in designing satellite systems. Earth observation satellites could be regarded as a two tandem server system with a finite buffer in between, providing two-stage service: image capture and image download service. In this paper, we introduce the queueing models for different service systems: the pure image capture service system, the two-stage service system with Poisson distribution download service, the pure download service system, and the two-stage system with general download service. Formulated solutions are given and some results are shown. From this work we can see queueing theory provides a good way to analyse the performance of small earth observation satellites, which is useful for system mission analysis and optimisation in design stage. 相似文献
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I. Bekey 《Acta Astronautica》1979,6(12):1669-1683
Technology advances expected by the late 1980 or early 1990 time period will allow the construction of powerful and complex communications satellites with large multibeam antennas and very many transponders, and their operation and maintenance in geostationary orbit. The high sensitivity and effective radiated power of such satellites will enable the Earth stations using them to shrink dramatically in size and cost, thus becoming readily available to very large numbers of users as well as making possible new kinds and levels of communications services simply not possible with smaller satellites. This paper briefly describes three such new designs, concerning electronic mail transmission, educational TV distribution, and mass personal communications; it compares the users' service costs with those of terrestrial networks designed for the same performance. 相似文献
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This paper presents a summary report and the major results of a Workshop on Small Satellites for Latin America, held at the National Institute for Space Research (INPE) in São José dos Campos, Brazil, at the initiative of the Sub-Committee on Small Satellites for Developing Nations of the International Academy of Astronautics (IAA). 相似文献
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Mazlan Othman 《Acta Astronautica》2003,52(9-12):687-690
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To achieve the size reductions needed to lower the costs of space imaging, every part of a satellite (telescope, detector, digitization, image compression, memory, telemetry, and of course satellite platform) has to be improved. With regard to the instrument, new dimensioning rules, new optical designs, and new detection systems allow significant gains. Better balance between detector and optics modulation transfer function (MTF) performances can be achieved. Though the involved solutions raise the question of signal level, the latter can be solved with the use of TDI (Time Delay and Integration) detection. The instrumental choices, the optical system under investigation and how the above techniques are allowed for in the next generation SPOT satellites development studies led by CNES will be presented in this paper, showing how they can achieve the goal of weight reductions. 相似文献
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The extensive coverage of the USA by cable television has posed a major hurdle for successful use of direct broadcast satellites. However, the potential for DBS service is improving because of breakthroughs in development of digital video compression and the availability of high-power satellites, combined with ample allocations of radio spectrum and orbital slots to DBS service. The success of DBS applications will depend critically on (a) the cost of small-antenna home receiving terminals, (b) operating expenses, and (c) demand for new services, such as HDTV, that could be provided by DBS systems more quickly and cheaply than through terrestrial transmission. 相似文献
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This paper presents some approaches to the development of advanced detectors and to miniaturized instrument design which are pursued in the Institute of Space Sensor Technology of DLR (the German Aerospace Research Establishment). The instrument design approach is demonstrated for a low-weight (3 kg) dual camera system with narrow-angle in-track stereo and wide-angle multispectral features. Each camera has its own signal processor and 0,5 G Bit mass memory. The activities for advanced detector development are concentrated on two different kinds of detectors and instrumentations: infrared detector arrays and instruments at wavelengths out to about 240 μm, and superheterodyne receivers in the submillimeter and far-infrared spectral ranges. 相似文献
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Direct Broadcast Satellites covering large countries such as Canada, require more than one spacecraft, located at different orbital positions, as well as the use of multiple shaped beams. This would minimize eclipse requirements over several time zones, provide increased capacity by frequency reuse and permit the use of cost effective ground receivers.Two such satellites are envisaged, one covering Eastern Canada, the other Western Canada, using two different sets of three highly shaped beams. This paper is the result of a feasibility study of a satellite antenna designed such that while at either orbital location it can be reconfigured in orbit, by ground command and hence can save the cost of one additional spare spacecraft.An offset parabolic reflector is proposed for the 12 GHz downlink, with a switched “dual feed” structure, consisting of two separate but contiguous sets of pyramidal horns and their associated beam forming networks (BFN). Only one BFN set is used at any one orbital location. Detailed radiation patterns demonstrate good beamshaping capabilities, with coverage efficiencies of the order of 94%. Other considerations such as the effect of orbital locations, gain equalization and TWTA standardization are discussed.It is concluded that a satellite, reconfigurable in orbit with a “dual feed” antenna, is feasible and cost effective, for a DBS spare as well as for the main spacecraft. 相似文献
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加强自主创新推动军工制造业高效数控工艺技术发展 总被引:1,自引:0,他引:1
党的十六届五中全会指出“国防科技工业要坚持军民结合、寓军于民,继续调整改造和优化结构,健全军民互动合作的协调机制,提高产品的研发和制造水平,增强平战转换能力、”“坚持以信息化带动工业化,广泛应用高技术和先进适用技术改造提升制造业”,为国防科技工业的发展提出了明确要求。国防科技工业是国家战略性产业,也是国家制造业的重要组成部分。国防科技工业的发展对增强国防实力,促进国防现代化和高技术发展,带动其他产业及提高工业化整体水平有着重要的作用。军工产品的研制生产离不开数控装备的支撑,它的独特需求又带动了数控装备和技… 相似文献
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Jana K. Hettling 《Space Policy》2003,19(1):33-39
This paper examines the use of remote sensing satellites for verification in public international law. Verification always depends on the specific agreement or mission to be verified. There are no general framework rules: the means of verification and the verifying authorities vary from agreement to agreement and from mission to mission. Rapid technological development and the intensifying international cooperation have led to an increasing number of international verification missions. Whereas, in the past, verification was at the heart of intelligence and national services, the commercialization of the remote sensing industry and the information revolution have supported the creation of joint initiatives in this field. Traditionally, verification is associated with disarmament and arms control treaties, but the paper will underline that this is only one field of application for verification missions. It is important to note that there is no binding international regime specifically addressing such activity. The lack of legal certainty in this field also applies to the use of remotely sensed data as evidence in legal proceedings. 相似文献
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Santiago Astrain 《Acta Astronautica》1981,8(11-12)
This article provides several illustrations of the growing economic importance and scope of communications satellite service and discusses how rapid development of new telecommunications systems, particularly those that include communications satellite systems, serve as a major stimulant of economic growth. There is evidence that communications satellites are capable of making important economic contributions to developed and developing countries alike. The rapid proliferation of separate communications satellites, although stimulating economic growth, is giving rise to concerns about intersystem connectivity and saturation of the available radio frequencies in geosynchronous orbit. The growth of the communications satellite industry to an activity level of perhaps $10,000 million per annum by the mid-to-late-1980s could assist in the development of multipurpose space platforms that could minimize the problems created by satellite proliferation. 相似文献
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Miniaturization techniques enable the realization of very small satellites with interesting capabilities in space science. The University of Würzburg contributed in the scope of the cubesat program with its own pico satellite UWE-1, which is in orbit since October 2005. Despite reliable and stable operation of the on-board data handling (OBDH) system during the UWE-1 mission, the successor UWE-2 will be equipped with a more sophisticated, modular and extensible OBDH system, which was designed to facilitate the further development of the UWE satellite platform. The OBDH system was designed for high reliability and stability, but with an easier extension capability. The modular structure of the new system thus supports potential transfer to other satellite platforms. 相似文献
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In extension to common applications such as groundtrack displays and antenna steering, the SGP4 orbit model is proposed for operational orbit determination in small satellite missions. SGP4 is an analytical orbit model for Low-Earth orbiting satellites that is widely used for the propagation of NORAD twoline elements. Twoline elements may hence be generated completely independent of NORAD. Their use as exclusive source of orbital information simplifies the operations concept and reduces mission costs through the extensive use of existing low-cost mission support software. Due to small computer resource requirements of 8–10kByte, the SGP4 model may also be applied for onboard orbit computations making use of e.g. a 80186 processor, thus ensuring full compatibility of ground-based and onboard operations. The proposed approach is particularly suited in combination with a space-borne GPS receiver, were the C/A-code navigation solutions are treated as measurements that are adjusted in a least-squares sense using the SGP4 model. As consequence, inherent drawbacks of the pure navigation solutions such as data gaps and scatter as well as limited velocity accuracy are avoided, while the operational navigation activities are kept at a minimum. The feasibility of the concept is illustrated based on real GPS navigation data from the TOPEX/Poseidon and the MIR space station with an inherent data quality of 50–100 m. It is shown that 3 hours of data within a 4 day period are sufficient to keep the position error within 4 km, that is considered sufficient for most applications. 相似文献