2016
DOI: 10.1007/978-3-319-48989-6_34
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Battery-Aware Scheduling in Low Orbit: The GomX–3 Case

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Cited by 23 publications
(10 citation statements)
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“…However, accurate power budget modeling requires a profound understanding and correct extrapolation of the battery behaviour, which is known to be non-linear. In this sense, authors had addressed the battery-aware task scheduling problem for LEO satellites using detailed battery models [23], [24], but the proposed approach assumed a single (non-networked) satellite. Indeed, the impact on the battery charge of inter-satellite transponders used for inorbit networking has far been disregarded.…”
Section: Introductionmentioning
confidence: 99%
“…However, accurate power budget modeling requires a profound understanding and correct extrapolation of the battery behaviour, which is known to be non-linear. In this sense, authors had addressed the battery-aware task scheduling problem for LEO satellites using detailed battery models [23], [24], but the proposed approach assumed a single (non-networked) satellite. Indeed, the impact on the battery charge of inter-satellite transponders used for inorbit networking has far been disregarded.…”
Section: Introductionmentioning
confidence: 99%
“…Achieving such an ambitious objective will depend on the successful interaction between the space industry and state‐of‐the‐art research on informatics. Among others, in‐orbit satellites such as the GomX–4A and GomX–4B satellites from GomSpace are pioneering efficient space‐terrestrial communication techniques based on extensive support from scheduling computation on ground 3‐6 …”
Section: Introductionmentioning
confidence: 99%
“…Moreover, recent work by the authors have introduced battery‐awareness constraints 5,6 . Results showed that it is crucial to have detailed knowledge on how much power is drained for GSLs and ISLs, especially when in eclipse, where on‐board batteries possibly end up in critically low states of charge 3,4 . Early versions of a Mixed‐Integer Linear Programming (MILP) model computed and designed optimal transponder's duty cycle for a LEO constellation of GomX–4 satellites 5,6 …”
Section: Introductionmentioning
confidence: 99%
“…Many safety-critical systems can be modeled as nonlinear ordinary differential equations (ODEs) which exhibit uncertain parameters due to finite precision measurements, lack of data, or noise [5]. In order to formally decide whether such a system is safe, it is necessary to determine whether the model can reach a bad state [14,9,36]. Since closed-form expressions for reachable sets of nonlinear ODE systems are not known in general [35], it becomes necessary to over-and under-approximate the reachable set.…”
Section: Introductionmentioning
confidence: 99%