HRangeMeasurement:

Path: SpacecraftEstimation/OrbitEstimation

% Generate the range/range rate measurement matrix and the estimated measurement. 
   This gives the measurements in the form

   y = meas0 + H*dX

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   Form:
   [meas0, h] = HRangeMeasurement( x, d )
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   ------
   Inputs
   ------
   x        (m,:)    State estimate [Position;Velocity;clock bias;clock drift;...] 
   d        (n)      Measurement data structure
                      .rSourceECI  (3,1)  Position of source (ECI)           
                      .vSourceECI  (3,1)  Velocity of source (ECI) 

   -------
   Outputs
   -------
   meas0    (2*n,1)  [range;range rate]
   h        (2*n,m)  H matrix [Hrange;HRange rate]

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Children:

Math: Linear/Dot
Math: Linear/Mag

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