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Earth Observation Mission CFI Software Lib Software User Manual for JAVA |
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| 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 | |
| setWarning() | EECFI.CfiClass | |
| vectorsToQuaternions(double uxVec[], double uyVec[], double uzVec[]) | EECFI.LibFunc | [static] |
1.7.1