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Breath in, breath out how healthy are the batteries on Mars and Venus Express?

机译:呼吸,呼吸火星和金星的电池有多健康?

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I. Introduction Mars and Venus Express are operational since 2003 and 2005, respectively. Combined, this is more than 14 years in flight of two similar spacecraft, yet operating in very different environments. Both S/C had their mission extended multiple times up to now and this process continues. The spacecraft budgets were designed for the original duration (around 1000 days for each mission), and estimates on battery capacity degradation logically cover only that period. To be able to assess the current health state of the batteries, and to gather trends for predictive models, the Flight Control Team had to develop its own empirical methods based on data available from telemetry. A thorough assessment resembling laboratory conditions is not possible due to several factors: no calibration of the sensing equipment possible in-flight, no possibility to remove the battery from the circuit, no possibility to control the discharge rate, no possibility to control the thermal environment. The method developed and used consists of fitting a model of the battery voltage (based on the 'state-of-charge vs. EMF' curve) to the voltage measurements as obtained from telemetry. The model optimizes the initial energy capacity degradation factor and the losses due to internal resistance dissipation. To obtain significant data for analysis the operators had to plan for dedicated longer discharges, as data available from routine eclipses was not sufficient to obtain a significant excursion of the EMF curve outside its linear initial part. Following recommendations from industry, ESA specialists and documentation, the teams also decided to keep MEX and VEX batteries at a lower State of Charge (SoC) outside eclipse periods. This is done by forcing the End-of-Charge voltage which yielded (temporary) battery capacity recovery. This paper explains the methodology used and discusses the results obtained and compares the Mars Express (MEX) and Venus Express (VEX) results and degradation predictions.
机译:I.简介MARS和金星EXPRESS分别为2003年和2005年以来运作。合并,这是在两种类似的航天器飞行中超过14年,但在非常不同的环境中运行。 S / C都有他们的使命延长到现在,这一过程继续。航天器预算设计用于原始持续时间(每个任务约1000天),并且电池容量降级的估算逻辑地覆盖该期间。为了能够评估电池的当前健康状况,并收集预测模型的趋势,飞行控制团队必须根据遥测提供的数据开发自己的实证方法。由于若干因素,不可能进行彻底的评估,这是不可能的:无需校准传感设备可以在飞行中,无法从电路中取出电池,无需控制放电速度,无需控制热环境。无法控制热环境。开发和使用的方法包括拟合电池电压的模型(基于充电状态与EMF'曲线)到从遥测中获得的电压测量值。该模型优化了初始能量能力劣化因子和由于内部电阻耗散而损耗。为了获得有关分析的重要数据,运营商必须计划专用更长的放电,因为从日常食用的数据提供的数据不足以获得其线性初始部分之外的EMF曲线的显着偏移。在行业,ESA专家和文件的建议之后,该团队还决定将MEX和VEX电池放在日食外时期的较低的充电状态(SOC)。这是通过强制充电结束电压来完成的(临时)电池容量恢复。本文解释了所使用的方法,并讨论获得的结果并比较MARS Express(MEX)和金星表达(VEX)结果和退化预测。

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