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Path: SpacecraftEstimation/OrbitEstimation
% Measurement matrix for range and range rate -------------------------------------------------------------------------- Form: [m, h] = HRangeRangeRate( x, d ) -------------------------------------------------------------------------- ------ Inputs ------ x (6,:) State estimate [Position;Velocity] ------- Outputs ------- m (2,1) [range;range rate] h (2,6) H matrix [Hrange;HRange rate] --------------------------------------------------------------------------
Math: Linear/Mag
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