导航卫星中断频次的分析方法

面向导航卫星中断频次的定量分析需求,该文分析导航卫星中断产生的主要原因,给出中断频次分析的流程,并针对分析过程中的三个关键问题,研究提出具体实施方法,包括通过相关性分析快速定位底层中断事件,通过中断树建立指标分析模型,并融合在轨数据、地面试验数据快速预估得到底层功能异常率等。最后通过示例进一步说明中断频次分析过程。该文方法已应用于北斗导航卫星工程。     

Availability modeling for periodically inspection system with different lifetime and repair-time distribution

Availability is a main feature of design and operation of all engineering system. Recently,availability evaluation of periodical inspection systems with different structures is at the center of attention due to the wide application in engineering. In this paper, an analytical and probabilistic availability model for periodical inspection system is proposed by a new recursively algorithm,which can achieve limiting average availability and instantaneous availability of periodical inspection system under arbitrary lifetime and repair-time distributions. Then three application examples are presented, the systems lifetime and repair-time are respectively fellow exponential/exponential,Weibull/normal and Weibull/lognormal distribution. Finally, a Weibull/lognormal system is studied to analyze the dynamic relationship between inspection period and availability. The results indicate that the proposed approach can provide the technology support for improving system availability and determining reasonable inspection period.     

卫星控制中心系统平台的高可用设计与实现

卫星控制中心是卫星地面测控管理系统的重要组成部分。随着信息技术的飞速发展和测控关键业务量的增长,高可用性、高可靠性及易维护日益成为卫星控制中心系统的设计目标。为满足卫星测控任务的需求,本文描述了卫星控制中心的网络系统、数据处理系统和数据库集群系统的高可用设计,并给出具体项目的成功实现。     

以可用度为目标的民用飞机不完全预防性维修间隔优化

民用飞机制造商推荐的初始预防性维修间隔通常不考虑运营环境和维修能力的差异,在满足飞机安全性要求的同时,难以达到可用性的最优状态。基于不完全维修理论,采用役龄回退因子修正部件的可靠性模型,以反映维修工作对于部件性能的影响;结合航空公司运行实际情况,以部件可用度为目标函数,可靠度阈值为约束条件,提出不完全维修策略下的预防性维修间隔优化模型,并以某型飞机的空气起动机航线故障数据进行实例验证。结果表明：在满足可靠度阈值的约束条件下,所建立的维修间隔优化模型得出的最优维修间隔与实际相符,该模型合理可行。     

基于半分析式方法的全球导航星座设计

导航星座设计涉及诸多参数的优化组合,设计目标就是寻找一组参数组合,使其构成的星座在指定覆盖区域既能获得最优的星座性能,又节省系统建设成本和星座长期维持费用。首先,提出评价导航星座性能的技术指标、可用性算法以及半分析式星座设计方法;然后,详细论证设计参数对导航星座性能的影响,进而综合分析得到3种全球导航星座设计方案;最后,通过对比研究3种星座方案的性能指标和导航定位仿真结果,说明导航星座设计方法和设计方案的可行性。     

正态分布单元可用度及其影响因素分析

在航空航天系统中,可修复单元的故障密度和修复密度并非总是服从指数分布,实际存在着正态分布情况,不能采用马尔可夫状态转移方法处理。文章以故障密度和修复密度都服从正态分布的产品为例,通过数值求解微分方程组,分析了正态分布单元的可用度变化规律以及影响因素。     

系统稳态可用度抽样检验方案

设系统的故障间隔时间Ｘ和维修时间Ｙ的分布均未知,但Ｘ和Ｙ的变差系数均已知。对于系统稳态可用度,该文给出了它的计量标准型抽样检验方案。     

地空导弹武器系统可用性分析

可用性是构成地空导弹武器系统作战效能、并影响其寿命周期费用的重要因素，是武器系统战术技术指标的重要组成部分。讨论了地空导弹武器系统的可用性要素及各要素之间的相互关系。最后以某地空导弹武器系统为例，对可用性进行了分析。     

Three frequency GNSS navigation prospect demonstrated with semi-simulated data

Three frequency GNSS (Global Navigation Satellite Systems) signals will be fully accessible in the near future. It is theoretically well-understood that the GNSS navigation performance could be improved with introduction of the third frequency signals. However it remains unclear what numerical improvements can be achieved in the varying navigation scenarios. In this paper, we numerically demonstrate the superior navigation prospect of three frequency GNSS compared to dual-frequency case. Since the third frequency pseudorange is not fully accessible at current stage, a semi-simulation method is firstly introduced to generate the third frequency pseudorange based on the dual-frequency GPS pseudorange and phase measurements. Then the three frequency navigation precision, availability and reliability are examined, compared with their dual-frequency counterparts in varying simulated navigation scenarios. The results show that with three frequency GNSS signals the navigation precision can be improved by 10% in both horizontal and vertical components. More promisingly, the availability of navigation solutions is significantly improved (even by 50% for some scenarios) with higher reliability.     

Correlation of GPS signal fades due to ionospheric scintillation for aviation applications

Deep and frequent Global Positioning System (GPS) signal fading due to strong ionospheric scintillation is a major concern for GPS-guided aviation in equatorial areas during high solar activity. A GPS aviation receiver may lose carrier tracking lock under deep fading, and a lost channel cannot be used for position calculation until lock is reestablished. Hence, frequent loss of lock due to frequent fading can significantly reduce the availability of GPS aviation. However, the geometric diversity of the satellites can mitigate scintillation impact on GPS aviation depending on the correlation level of deep fades between satellites. This paper proposes a metric to measure the correlation level of two fading channels from the perspective of GPS aviation. Using this metric, the satellite-to-satellite correlation is studied based on real scintillation data. The low satellite-to-satellite correlation shown in this paper envisions notable availability benefit from the geometric diversity of satellites under strong scintillation. In addition, this paper proposes a way to generate correlated fading processes with arbitrary correlation coefficients. Using this correlated fading process model, the availability of Localizer Performance with Vertical guidance (LPV)-200 under severe scintillation scenarios is analyzed. The result emphasizes the importance of a fast reacquisition capability of an aviation receiver after a brief outage, which is not currently mandated by the aviation receiver performance standards.