Proceedings of the 25th Intersociety Energy Conversion Engineering Conference
DOI: 10.1109/iecec.1990.716540
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A Spacecraft Electrical Battery Model And Simulator

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Cited by 7 publications
(7 citation statements)
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“…In general, complex load models will add state variables to the overall current-loop state-space description through the driving-point admittance In such cases, the currentloop state equations will generally be more complicated than those summarized in (12). Gains might have to be adapted and/or different compensation schemes might be needed for different loads.…”
Section: Givenmentioning
confidence: 98%
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“…In general, complex load models will add state variables to the overall current-loop state-space description through the driving-point admittance In such cases, the currentloop state equations will generally be more complicated than those summarized in (12). Gains might have to be adapted and/or different compensation schemes might be needed for different loads.…”
Section: Givenmentioning
confidence: 98%
“…This made it easy to step from (10) to (11), while developing the full-state equations (12) for the current loop in the previous section. For a more complicated LTI load model, the delay model of the voltage loop may not be as easy to apply.…”
Section: B Zoh Modelmentioning
confidence: 99%
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“…Most batteries, on the other hand, tend to exhibit nonlinear driving point currentholtage characteristics. It is often possible, however, to develop LTI or piecewise LTI battery models; see [13] for example.…”
Section: B Zero-order-hold Modelmentioning
confidence: 99%