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为满足复合材料制造技术出口的要求,将一种复合材料用树脂胶由单组份状态改变为双组份状态,以达到提升其贮存期的目的。通过试验确定了该双组份树脂胶的配方及其贮存期,提高了树脂胶的使用寿命,为K8飞机出口提供了技术支持。 相似文献
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本文提出了一个高超声速非烧蚀钝体化学非平衡尾流流场的简化模型和简化的空气化学模型。应用该模型计算尾流的积分电子密度。计算结果与实验数据符合得很好。在此基础上,以P_∞D_N=375mmHg·mm为例,初步论证了尾流双尺度律的适用程度与范围,为弹道靶模型实验提供正确的导向。 相似文献
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针对卫星导航接收机性能易受多径信号的影响,提出了一种基于窄相关的BOC信号的多径减弱方法。该方法通过调整本地伪码相位使码跟踪环路和载波跟踪环路工作在受多径影响小的自相关函数副峰上,有效地减小了多径信号对环路的影响,性能优于传统的窄相关技术,且几乎不增加设备的复杂度和计算量。通过对BOC(1,1)和BOC(10,5)的仿真分析表明:该方法能有效减小多径引起的误差,对延迟大于0.5个码片的多径信号能起到完全抑制的效果。最后本文还对该方法在低信噪比下的应用给出了建议。
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任志刚 《西安航空技术高等专科学校学报》2006,24(1):15-16
利用无线收发技术和计算机控制管理技术,来实现和完成汽车电子牌照的检测与车辆的管理,其特点是自动检查车牌,自动完成各种控制,该系统安装、测试、维修简单,成本低、效益高。 相似文献
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在红外成像制导技术的算法研究中,目标红外图像序列是进行仿真验算的基础,通常真实的图像序列较难获得,本文通过建立空间目标的透《视投影模型来模拟红外成的过程,并由计算机作图得到目标的二值图像,为目标识别、跟踪算法及制导率的仿真验算打下了基础。 相似文献
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M. Nakajima T. Mihara K. Makishima H. Niko 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2006,38(12):2756-2758
We report on the luminosity dependent change of the cyclotron resonance energy obtained from a transient X-ray pulsar, 4U 0115+63. Using RXTE data observed on 1999 March, we found that the fundamental resonance energy stayed constant (11 keV) when the source luminosity was above 5 × 1037 erg s−1. As the luminosity decreased below 5 × 1037 erg s−1, the fundamental resonance energy gradually increased up to 16 keV at 0.16 × 1037 erg s−1. The luminosity dependence of the resonance energy can be understood by the change of the accretion column height. 相似文献
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本文利用元件和系统两者的一次性检测数据或定期检测数据,用EM算法给出由指数寿命型元件串联而成的系统的可靠性的估计。本文还给出了数字实例。 相似文献
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《中国航空学报》2020,33(12):3437-3446
Fault tolerance designs are essential techniques for systems that require high levels of reliability, such as aircraft or spacecraft control system. Imperfect Fault Coverage (IFC) may lead to the failure of a system or subsystem even with adequate redundancy. Previous studies of IFC mostly concentrated on evaluating Coverage Factor (CF), whereas the system failure behaviors with IFC have rarely been involved. Failures that occur in low-layer may be covered by high-layer. However, if the coverage is imperfect, uncovered failure will have functional and physical impact on the system behavior. In this thesis, the failure behavior and reliability of IFC of multi-layer systems are studied and a Binary Decision Diagram (BDD)-based modeling and simulation method are proposed to evaluate system reliability. As a case, the failure behavior of an aero engine electronic controller with IFC is studied. The results show that the IFC may impact system behavior without taking the IFC into account, the system maintenance intervals may reduce, and thus the maintenance costs will increase. 相似文献