|
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] |
| 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() | EECFI::CfiClass | |
| ~LibFunc() | EECFI::LibFunc | [inline, virtual] |
1.7.1