MeasEarthSensor:

Path: SC/Sensor

% Returns roll and pitch for a generic earth sensor.
   The sensor frame assumes that z is normal to the focal plane.

   The field "kQ" selects the quaternion from the state vector x. The
   field "kR" selects the spacecraft position.
   The outputs are angle about x (roll) and y (pitch) in the sensor frame.

   If no inputs are given it will return the default data structure.

   Since version 11.
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   Form:
   y = MeasEarthSensor( x, d )
   d = MeasEarthSensor
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   ------
   Inputs    
   ------
   x         (:,1)  State vector
   d         (1,1)  Data structure
                    .kQ            (1,4) Quaternion state
                    .kR            (1,3) Position state
                    .qBToS         (4,n) Body to earth sensor quaternion
                    .bias          (2,n) Bias
                    .scale         (2,n) Scale
                    .noise         (2,n) 1 sigma noise
                    .fOV           (1,1) Field of view
                    .quantization	(1,1) Least significant bit

   -------
   Outputs
   -------
   y         (n,1)   Measurements in counts

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Children:

Common: Quaternion/QForm
Math: Linear/Unit

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