Earth Observation Mission CFI Software Lib Software User Manual for JAVA |
CfiClass() | EECFI.CfiClass | |
eulerToMatrix(double eulerAngles[]) | EECFI.LibFunc | [static] |
getRotatedVectors(double xsInit[], double ysInit[], double zsInit[], double angle[]) | EECFI.LibFunc | [static] |
getRotationAngles(double xsInit[], double ysInit[], double zsInit[], double xsFin[], double ysFin[], double zsFin[]) | EECFI.LibFunc | [static] |
LibFunc() | EECFI.LibFunc | |
matrixToEuler(double matrix[][]) | EECFI.LibFunc | [static] |
quaternionsInterpol(final QuaternionsInterpolationCfg cfg, double time_1, double q1[], double time_2, double q2[], double time_out) | EECFI.LibFunc | [static] |
quaternionsToVectors(double quaternions[]) | EECFI.LibFunc | [static] |
resetWarning() | EECFI.CfiClass | [static] |
setSilent() | EECFI.LibFunc | [static] |
setVerbose() | EECFI.LibFunc | [static] |
setWarning() | EECFI.CfiClass | [static] |
vectorsToQuaternions(double uxVec[], double uyVec[], double uzVec[]) | EECFI.LibFunc | [static] |