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Replace the delayed time feedback mechanism used by the translational states with a direct feedback method. Time constants for velocity and position convergence can be separately adjusted with tunable parameters The method is more computationally more expensive because it requires modification of the output buffer history but is acceptable because it only requires 6 FLOP per buffer index for a total of 30*6 = 180 FLOP The method was not applied to the attitude states because the quaternion operations required at each buffer index would have been computationally prohibitive.