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SUPPORT SITE |
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SUPPORT SITE |
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Path: SpacecraftEstimation/OrbitEstimation
% Full state measurement of an orbit.
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Form:
y = MeasOrbitState ( x, d )
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Inputs
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x (6,1) State [x;y;z;vX;vY;vZ]
sensorData (.) Structurenoise1Sigma
.noise1Sigma (6,1) State noise
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Outputs
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x (6,1) State measurements [x;y;z;vX;vY;vZ]
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