Path: SpacecraftEstimation/AttitudeEstimation
% Performs a covariance analysis of different gyros. ------------------------------------------------------------------------ See also C2DZOH, Plot2D, RW2SDev ------------------------------------------------------------------------ % ------------------------------------------------------------------------- Copyright 1999 Princeton Satellite Systems, Inc. All rights reserved. ------------------------------------------------------------------------- dToDeg = 180/pi; gToRad = pi/180; rHrToPerSec = 1/3600; roType = 'HRG';