Path: SpacecraftEstimation/AttitudeEstimation
% An attitude determination system using vector measurements.
The first column of catalog is the magnetometer data.
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Form:
[x, p] = SunMagAttDet( x, p, r, qBToS, bMeas, sensorData, catalog, fScale )
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Inputs
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x (3,1) Attitude [x;y;z]
p (3,3) State covariance matrix
r (m) Measurement noise
qBToS (4,1) Quaternion from body to sensor axes
bMeas (3,1) Measured magnetic field
sensorData (m,3) .xy (2,:) Focal plane data
.validMeas (:) 1 if measurement is valid
catalog (3,p) Catalog of unit vectors
fScale Sensor scale factor
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Outputs
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x (3,1) Attitude [x;y;z]
p (3,3) State covariance matrix
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SpacecraftEstimation: AttitudeEstimation/EKFSSG Common: Quaternion/Q2Mat Math: Linear/Mag Math: Linear/Skew
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