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首页> 外文期刊>Journal of aerospace engineering >Optimal Station Keeping for XIPS Thrusters in Failure Mode under Eclipse Constraints
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Optimal Station Keeping for XIPS Thrusters in Failure Mode under Eclipse Constraints

机译:Eclipse约束下故障模式下XIPS推进器的最佳站位保持

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摘要

The objective of this paper is to minimize fuel consumption needed for geostationary Earth orbit station keeping by Xenon Ion Propulsion System (XIPS) thrusters in failure mode under eclipse constraints. Two diagonal XIPS thruster pairs, each pair consisting of one north thruster and one south thruster, are mounted on the antinadir face of the satellite. In failure mode, only one diagonal thruster pair fires. The original failure-mode station-keeping strategy without consideration of the eclipse constraints fires the remaining diagonal thrusters a second time with equal duration in the vicinity of similar to 0 degrees or 180 degrees right ascensions (RA), in addition to a first time in the vicinity of similar to 90 and 270 degrees RA, which also results in the problem of excessive fuel consumption. The eclipse constraints are considered in this paper and the feasible firing location for station keeping during eclipse time is established. A optimal failure-mode station-keeping strategy under eclipse constraints is presented with the firing locations and durations of one diagonal thruster pair as design variables. The optimal station-keeping model is built and applied for maintaining a geostationary satellite within a predefined space box. Precise orbital simulation results show that the proposed optimal failure-mode station-keeping strategy can both save fuel and satisfy eclipse constraints. (C) 2016 American Society of Civil Engineers.
机译:本文的目的是在日蚀约束下,以故障模式将氙离子推进系统(XIPS)推进器保持对地静止地球轨道站所需的燃料消耗降至最低。两对对角XIPS推进器对,每对包括一个北向推进器和一个南向推进器,安装在卫星的背面。在故障模式下,只有一对对角推进器会点火。不考虑日食约束的原始故障模式站位保持策略,除了第一次,是在与0度或180度右上角(RA)类似的附近,第二次以相等的持续时间发射其余的对角推进器。接近90度和270度RA的附近,这也导致燃料消耗过多的问题。本文考虑了日食的约束条件,建立了日食期间保持站位的可行点火位置。提出了一种在日食约束下的最优故障模式驻车策略,以一对对角推进器的点火位置和持续时间作为设计变量。建立了最佳的台站保持模型,并将其用于在预定的空间盒内维护对地静止卫星。精确的轨道仿真结果表明,所提出的最优故障模式驻站策略既可以节省燃料,又可以满足日食约束。 (C)2016年美国土木工程师学会。

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