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为准确判断火箭发动机涡轮泵轴承在试验台上试验时发生故障的部位,同时避免通过轴承特征频率诊断轴承故障的方法所带来的不确定性,基于GPS卫星导航定位原理,利用时幅曲线的相位信息,提出一种新的轴承故障诊断方法:振源坐标定位法,即通过四个已知坐标的振动传感器测得同一振动波的时幅曲线相位差判定振源位置。将试验台上轴承和四个振动信号传感器安放在坐标已知的直角坐标系中,利用时幅曲线拐点分析法准确捕获振动信号到达四个传感器的时刻,再利用这四个时刻和已知坐标计算出振源位置坐标,最后根据振源位置坐标判断其是否为轴承故障及具体故障部位。通过仿真计算证明该方法理论上可行。 相似文献
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This paper proposes a fault-tolerant strategy for hypersonic reentry vehicles with mixed aerodynamic surfaces and reaction control systems (RCS) under external disturbances and subject to actuator faults. Aerodynamic surfaces are treated as the primary actuator in normal situations, and they are driven by a continuous quadratic programming (QP) allocator to generate torque com-manded by a nonlinear adaptive feedback control law. When aerodynamic surfaces encounter faults, they may not be able to provide sufficient torque as commanded, and RCS jets are activated to augment the aerodynamic surfaces to compensate for insufficient torque. Partial loss of effective-ness and stuck faults are considered in this paper, and observers are designed to detect and identify the faults. Based on the fault identification results, an RCS control allocator using integer linear programming (ILP) techniques is designed to determine the optimal combination of activated RCS jets. By treating the RCS control allocator as a quantization element, closed-loop stability with both continuous and quantized inputs is analyzed. Simulation results verify the effectiveness of the proposed method. 相似文献
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飞机武器系统易损性评价中几何描述研究 总被引:1,自引:0,他引:1
提出了飞机易损性评价中应提供的几何数据,建立了各类几何及拓扑变换的数学模型,用此模型可计算易损性评价所需的各个标准方位的几何数据。 相似文献
367.
Libo Liu Weixing WanBaiqi Ning Man-Lian ZhangMaosheng He Xinan Yue 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2010
The electron density profiles in the bottomside F2-layer ionosphere are described by the thickness parameter B0 and the shape parameter B1 in the International Reference Ionosphere (IRI) model. We collected the ionospheric electron density (Ne) profiles from the FORMOSAT-3/COSMIC (F3/C) radio occultation measurements from DoY (day number of year) 194, 2006 to DoY 293, 2008 to investigate the daytime behaviors of IRI-B parameters (B0 and B1) in the equatorial regions. Our fittings confirm that the IRI bottomside profile function can well describe the averaged profiles in the bottomside ionosphere. Analysis of the equatorial electron density profile datasets provides unprecedented detail of the behaviors of B0 and B1 parameters in equatorial regions at low solar activity. The longitudinal averaged B1 has values comparable with IRI-2007 while it shows little seasonal variation. In contrast, the observed B0 presents semiannual variation with maxima in solstice months and minima in equinox months, which is not reproduced by IRI-2007. Moreover, there are complicated longitudinal variations of B0 with patterns varying with seasons. Peaks are distinct in the wave-like longitudinal structure of B0 in equinox months. An outstanding feature is that a stable peak appears around 100°E in four seasons. The significant longitudinal variation of B0 provides challenges for further improving the presentations of the bottomside ionosphere in IRI. 相似文献
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He Ying 《中国航天(英文版)》2013,(1):17-18
(Continued) The 83rd Launch On November 18, 2004, a LM-2C launch vehicle was launched from the Xichang Satellite Launch Center with an experimental satellite inserting the satellite into its preset sun-synchronous orbit. Launch Site: Xichang Satellite Launch Center Launch Result: Success At 18:45 Beijing time on November 18, the LM-2C launch vehicle was launched into space. 13 minutes later the satellite separated from the carrier rocket and entered into a sun synchronous orbit of 700km with an inclination of 98.1 degrees and the solar panel of the satellite deployed smoothly. The LM-2C launch vehicle is a two- 相似文献
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文章主要介绍和分析卫星变轨对TDICCD相机系统的MTF、扫描周期的影响,最后分析卫星变轨对卫星覆盖范围的影响。 相似文献