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光纤涡轮流量传感器及检测系统研究 总被引:1,自引:0,他引:1
介绍一种利用光学方法检测涡轮转速的光纤涡轮流量传感器及检测系统。它具有信噪比高、量程比大的优点.试验表明,光纤涡轮流量传感器的量程比高达40:1,比常用的磁电式涡轮流量计大3倍,可满足航空发动机过渡态燃油流量的宽量程测量要求.还详细介绍了光纤涡轮流量传感器的结构和工作原理、温度修正原理,以及检测系统的硬件电路。最后给出传感器标定结果,并讨论了在航空发动机燃油测量中的应用。 相似文献
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利用后退归纳法讨论了截尾情况下导弹落点密集度的序贯决策方案 ,给出了确定最优停时的一般方法 ,仿真结果表明了方法的有效性 相似文献
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文章阐述了用于空间大气成分探测傅立叶变换红外光谱仪的国外发展状况,主要介绍了几种国外先进的高分辨率空间大气探测用傅立叶变换红外光谱仪的结构、应用范围和技术指标,比较了这几种设备的优缺点和技术特点。 相似文献
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E. Venechuk M.A. Franzen L.A. Roe D.W.G. Sears 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2008
Sample return from small solar system objects is playing an increasingly important part in solar system exploration. Critical to such missions is a robust, simple, and economic sample collector. We have developed a collector such as this for near-Earth asteroid sample return missions that we have termed the Touch-and-Go Impregnable Pad (TGIP). The collector utilizes a silicone substrate that is pushed into the dust and gravel surface layer of the asteroid. As part of a systematic evaluation of the TGIP, we have investigated the resilience of this substrate to ionizing radiations. Several miniature versions of the collector, containing typically ∼3 g of the collection substrate, were exposed to 0.564 MeV beta particles from a 90Sr source and a 6 MeV electron beam in a linear accelerator to simulate the wide range of energies of solar and galactic ionizing radiation. Various radiation levels up to eight times greater than expected on a six-year asteroid mission (in the case of beta radiation) and 50 times greater than expected (in the case of the 6 MeV electron radiation) were administered to the substrate. After irradiation, the efficiency of the substrate in collecting samples of mock regolith was compared with that of collectors that had not been irradiated. No difference beyond experimental uncertainty was observed and we suggest that the operational TGIP will not be affected adversely by radiation doses expected during a typical six-year inner solar system mission. 相似文献
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J. L. Burch R. Goldstein T. E. Cravens W. C. Gibson R. N. Lundin C. J. Pollock J. D. Winningham D. T. Young 《Space Science Reviews》2007,128(1-4):697-712
The ion and electron sensor (IES) is part of the Rosetta Plasma Consortium (RPC). The IES consists of two electrostatic plasma
analyzers, one each for ions and electrons, which share a common entrance aperture. Each analyzer covers an energy/charge
range from 1 eV/e to 22 keV/e with a resolution of 4%. Electrostatic deflection is used at the entrance aperture to achieve
a field of view of 90°× 360° (2.8π sr). Angular resolution is 5°× 22.5° for electrons and 5°× 45° for ions with the sector
containing the solar wind being further segmented to 5°× 5°. The three-dimensional plasma distributions obtained by IES will
be used to investigate the interaction of the solar wind with asteroids Steins and Lutetia and the coma and nucleus of comet
67P/Churyumov–Gerasimenko (CG). In addition, photoelectron spectra obtained at these bodies will help determine their composition. 相似文献
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针对压制干扰下组网雷达目标检测与跟踪,提出了一种基于压制干扰下雷达量测模型的跟踪技术。该跟踪技术包括压制干扰下量测模型和组网雷达序贯滤波跟踪两部分。压制干扰下量测模型根据雷达采取抗干扰措施前后接收机输入端的信干比分别计算检测概率,进而模拟传感器在压制干扰下对目标的检测情况。组网雷达序贯滤波中,首先对压制干扰下各雷达的量测数据进行串行合并和点迹合成,而后采用基于交互多模型(IMM)的序贯滤波方法对压缩后的数据进行跟踪。该检测与跟踪技术可模拟出雷达在压制干扰下由于检测概率下降造成的目标暂消现象,提高组网雷达跟踪航迹的连续性和稳定性。仿真结果表明了该技术的可行性和有效性。 相似文献