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Reliability
Satellite Power Subsystem
A satellite needs power from its battery, which is recharged by solar panels. The battery has a standby battery.
In[1]:=
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\[ScriptCapitalD]Battery = ExponentialDistribution[1/300]; \[ScriptCapitalD]Solarpanels = ExponentialDistribution[1/1000]; \[ScriptCapitalS]battery = StandbyDistribution[\[ScriptCapitalD]Battery, \ {\[ScriptCapitalD]Battery}]; \[ScriptCapitalR]satellite = ReliabilityDistribution[ solarpanel \[And] battery, {{solarpanel, \[ScriptCapitalD]Solarpanels}, {battery, \ \[ScriptCapitalS]battery}}];
The average number of load cycles the system can stand.
In[2]:=
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\[Mu] = NExpectation[t, t \[Distributed] \[ScriptCapitalR]satellite]
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In[3]:=
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Plot[SurvivalFunction[\[ScriptCapitalR]satellite, t], {t, 0, 800}, Filling -> Axis, PlotStyle -> Thick]
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The improvement potential for the components.
In[4]:=
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Plot[Evaluate@ ImprovementImportance[\[ScriptCapitalR]satellite \.00, t], {t, 0, 800}, PlotLegends -> {"Solar panel", "Battery"}, Filling -> Axis]
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