SSAD:
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Sun sensor attitude determination for sun-nadir pointing.
The sun sensors may be attached to the spacecraft solar array.
See also SSEye.
Since version 1.
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Form:
[yaw, sAPitch] = SSAD( mSS, eyeCoeff, uSun, roll )
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Inputs
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mSS (n) Magnitude of each sun sensor output
eyeCoeff (m) Eye coefficients where mSS = a[1]*x^0 + a[2]*x^1 +...
where x = cos(theta)
uSun (3,1) Sun vector in the body frame
roll (1,1) Measured roll angle
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Outputs
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yaw (1,1) Yaw Measurement
sAPitch (1,1) Solar array pitch measurement
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Children:
SC: Sensor/SSEye
