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The Operation Fault Simulation and Availability Analysis of Navigation Satellite

机译:导航卫星运行故障仿真与可用性分析

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When the operation faults of satellite navigation system occur, its navigation service performance will be affected. The regional satellite navigation constellation consists of GEO, IGSO and MEO. The space environments and orbit maneuvering situations of the satellites are different, because of their special orbit heights and types. Therefore, satellite fault situations need to be further refined and analyzed. The previous researches mostly discussed the two situations including orbit maneuvering and single event upset, but there is no considering about the randomness of orbit maneuvering or the fault situations of single event upset in different satellite work units. In this paper, the fault situations of single event upset are divided into four work units, including navigation task processing unit, spread spectrum receiver unit, satellite platform unit and satellite clock unit. Then, the specific fault simulation model is set up by the algorithm named Monte Carlo, and all the possible fault types of three kinds of satellites including GEO, IGSO and MEO are analyzed by simulation. Finally, the mathematical model of satellite availability is established, and then the satellite availabilities in different situations of fault types are analyzed comparatively.
机译:当卫星导航系统发生操作故障时,将影响其导航服务性能。区域卫星导航星座由GEO,IGSO和MEO组成。卫星的空间环境和轨道操纵情况因其特殊的轨道高度和类型而有所不同。因此,卫星故障情况需要进一步完善和分析。以往的研究主要讨论了轨道机动和单事件up动这两种情况,但没有考虑轨道操纵的随机性或不同卫星工作单元中单事件up动的故障情况。本文将单事件翻转的故障情况分为导航工作处理单元,扩频接收机单元,卫星平台单元和卫星时钟单元四个工作单元。然后,通过蒙特卡罗算法建立了具体的故障仿真模型,并通过仿真分析了三种卫星的所有可能的故障类型,包括GEO,IGSO和MEO。最后,建立了卫星可用性的数学模型,然后对不同故障类型情况下的卫星可用性进行了比较分析。

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