Earth Observation Mission CFI Software Lib Software User Manual |
CfiClass() | EECFI::CfiClass | |
eulerToMatrix(double eulerAngles[3], double matrix[3][3]) | EECFI::LibFunc | [static] |
getRotatedVectors(double xsInit[3], double ysInit[3], double zsInit[3], double angle[3], double xsFin[3], double ysFin[3], double zsFin[3]) | EECFI::LibFunc | [static] |
getRotationAngles(double xsInit[3], double ysInit[3], double zsInit[3], double xsFin[3], double ysFin[3], double zsFin[3], double angle[3]) | EECFI::LibFunc | [static] |
LibFunc() | EECFI::LibFunc | [inline] |
matrixToEuler(double matrix[3][3], double eulerAngles[3]) | EECFI::LibFunc | [static] |
quaternionsInterpol(const QuaternionsInterpolationCfg &cfg, double time_1, double q1[4], double time_2, double q2[4], double time_out, double q_out[4]) | EECFI::LibFunc | [static] |
quaternionsToVectors(double quaternions[4], double uxVec[3], double uyVec[3], double uzVec[3]) | EECFI::LibFunc | [static] |
resetWarning() | EECFI::CfiClass | |
setWarning() | EECFI::CfiClass | |
throwWarn | EECFI::CfiClass | [protected] |
vectorsToQuaternions(double uxVec[3], double uyVec[3], double uzVec[3], double quaternions[4]) | EECFI::LibFunc | [static] |
~CfiClass() EXCEPT | EECFI::CfiClass | |
~LibFunc() NOEXCEPT | EECFI::LibFunc | [inline, virtual] |