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991.
Zhenfang Li Zheng Bao Hongyang Wang Guisheng Liao 《IEEE transactions on aerospace and electronic systems》2006,42(2):436-452
A new concept of spaceborne synthetic aperture radar (SAR) implementation has recently been proposed - the constellation of small spaceborne SAR systems. In this implementation, several formation-flying small satellites cooperate to perform multiple space missions. We investigate the possibility to produce high-resolution wide-area SAR images and fine ground moving-target indicator (GMTI) performance with constellation of small spaceborne SAR systems. In particular, we focus on the problems introduced by this particular SAR system, such as Doppler ambiguities, high sparseness of the satellite array, and array element errors. A space-time adaptive processing (STAP) approach combined with conventional SAR imaging algorithms is proposed which can solve these problems to some extent. The main idea of the approach is to use a STAP-based method to properly overcome the aliasing effect caused by the lower pulse-repetition frequency (PRF) and thereby retrieve the unambiguous azimuth wide (full) spectrum signals from the received echoes. Following this operation, conventional SAR data processing tools can be applied to focus the SAR images fully. The proposed approach can simultaneously achieve both high-resolution SAR mapping of wide ground scenes and GMTI with high efficiency. To obtain array element errors, an array auto-calibration technique is proposed to estimate them based on the angular and Doppler ambiguity analysis of the clutter echo. The optimizing of satellite formations is also analyzed, and a platform velocity/PRF criterion for array configurations is presented. An approach is given to make it possible that almost any given sparse array configuration can satisfy the criterion by slightly adjusting the PRF. Simulated results are presented to verify the effectiveness of the proposed approaches. 相似文献
992.
Jie Chang Anhua Wang 《IEEE transactions on aerospace and electronic systems》2006,42(2):527-539
Conventional aircraft power system is a constant-frequency (CF) supply based on mechanical-regulated constant-speed mechanism that has relatively low efficiency. Replacing the CF system with variable-frequency (VF) power improves overall efficiency, and reduce the system's weight and volume. However, this creates a new tier of requirements and design challenges. Novel VF-power architecture is developed with minimization of the power losses throughout the stages of power conversions. Optimal partitioning and grouping of onboard AC loads has been discussed with specific system data. New VF-input multi-functional power converters are also briefly discussed. 相似文献
993.
994.
随着改革开放的进一步深入,我国的民航运输事业也步入了发展的快车道,航空运输总周转量、飞行架次等各项运行指标年均以两位数的幅度攀升。近年来,为了应对和适应日益增长的空中交通流量,提升空管保障水平,部分管制中心开始实施雷达管制,在缩小了安全间隔的同时增强了安全余度, 相似文献
995.
996.
指出了中国民航在适用国际航空货物运输规则时的盲区,分析了产生原因和对民航收入的不利影响,最后提出了相应对策。 相似文献
997.
某型飞机机身合拢总装型架,在设计上采用了先进制造技术。型架上装有目前国际先进的光学坐标系统,型架地基采用整体框架式底盘。型架结构为分散式。按飞机飞行状态在型架中摆放,并由上方起吊形式下架。本文简要介绍了该型架的设计、制造情况及效果。 相似文献
998.
Ts P Dachev E G Stassinopoulous B T Tomov Pl G Dimitrov Yu N Matviichuk V A Shurshakov V M Petrov 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2003,32(1):67-71
The LIULIN-3M instrument is a further development of the LIULIN dosimeter-radiometer, used on the MIR spacestation during the 1988-1994 time period. The LIULIN-3M is designed for continuous monitoring of the radiation environment during the BION-12 satellite flight in 1999. A semiconductor detector with 1 mm thickness and cm2 area is contained in the instrument. Pulse high analysis technique is used to determine the energy losses in the detector. The final data from the instrument are the flux and the dose rate for the exposure time and 256 channels of absorbed dose spectra based on the assumption that the particle flux is normal to the detector. The LIULIN-3M instrument was calibrated by proton fluxes with different energies at the Indiana University Cyclotron Facility in June 1997 and had been used for radiation measurements during commercial aircraft flights. The calibration procedure and some flight results are presented in this paper. 相似文献
999.
1000.
从配方、操作方法、原理等方面介绍了全顺汽车车身涂装底漆线的投槽工艺。较为详细的介绍了涂装前处理工艺和电泳工艺部分的清洗工序。本文对水质的影响也做了简要的分析。 相似文献