排序方式: 共有14条查询结果,搜索用时 15 毫秒
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文章介绍了测控应答机的现状及研究背景,并对研制中的困难及今后的发展需求进行了分析,提出了通用化测控应答机的设计方案及关键技术,可供通用化测控应答机设计和批量生产参考。 相似文献
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一种双通道测速应答机及其精度分析 总被引:2,自引:0,他引:2
介绍了一种双通道测速应答机的工作原理,并对其非相参通道的测速精度进行了定性分析。 相似文献
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介绍了风云二号(FY-2)气象卫星数传与云图广播转发器分系统的功能、组成,以及频率配置、传输信号特性和增益与功率等主要技术指标.给出了C星分系统转发器的技术改进.阐明了采用的收发多工器、射电天文保护滤波器、固体功率放大器(SSPA)和功能转换开关等关键技术.测试结果和在轨运行状况表明,C星数传与云图广播转发器的性能符合设计任务书要求,在轨运行正常稳定. 相似文献
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Durk Jong Park Kyung Whan Yeom Sang Il Ahn Hyo Suk Lim 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2014
This paper describes the development and validation of a transportable active transponder designed for the image calibration of Korea Multi-Purpose Satellite-5 (KOMPSAT-5) with a synthetic aperture radar (SAR). Ground targets are essential in SAR image calibration. The environment for the deployment of ground targets for SAR image calibration should provide uniformity and minimum interference. The Amazon or deserts are regarded as desirable environments. However, such environments for SAR image calibration are difficult to find in Korea. Thus, it will be advantageous to have an active transponder whose performance will not be severely limited by the absence of such uniform environment. We have therefore developed an active transponder which has an adjustable internal delay and into which the orbit data of an arbitrary satellite can be loaded. The stored obit data with the aid of an internal global positioning system (GPS) receiver and gyroscope enables the active transponder to point to a selected satellite. In addition, a virtual deployment of the active transponder is possible due to its adjustable internal delay. Thus, the developed active transponder can be deployed at any place without environmental constraint. The performance of the developed active transponder is validated using the satellite TerraSAR-X, which is already in operation. The test results show that the active transponder is successfully compliant with the requirements for KOMPSAT-5 image calibration. 相似文献
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N. Pierdicca C. Bignami M. Roca P. Féménias M. Fascetti M. Mazzetta C.N. Loddo A. Martini S. Pinori 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2013
Although the history of spaceborne altimeters goes back to the early seventies, the absolute calibration of the backscattering coefficient has never been deeply investigated. This information has been primarily used to infer the wind speed via an empirical model, and the intercalibration among different satellite altimeters has revealed to be suitable for this purpose, being the wind retrieval based on an empirical relationship. As far as Ku band system is concerned, the sigma naught absolute calibration of the Envisat altimeter (RA-2) has been performed using an active reference target provided by a transponder. This has been exploited during the 6-month Commissioning phase to generate early calibration results. In order to monitor the RA-2 backscatter calibration during the Envisat lifetime, a continuous calibration effort has been carried out by operating the transponder as much as possible. This paper aims to review the entire effort for calibrating the RA-2 sigma naught measurements, which lasted for almost seven years. It presents in detail the adopted methodology and the final outcome of the activity, providing the users with the correction (bias) to get the calibrated sigma naught and analyzing its stability during almost the entire Envisat lifetime. Specifically, it is concluded that the RA-2 backscatter measurements were quite stable, even if a bias of about 1 dB should be considered with respect to the actually released product. Some small changes in the bias as function of time can be identified during most of the Envisat lifetime, consisting in a slight increase in the first two years, followed by a more stable period and a final drop observed at the end of 2009, until the conclusion of the calibration activity (corresponding to the change in Envisat orbit). 相似文献
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阐述了一种仅采用信号源和频谱仪两种仪器,测量幅频特性的新颖方法,并给出了一个测量卫星转发器幅频特性的实际例子。 相似文献