APMFile() | | 100% | | n/a | 0 | 1 | 0 | 12 | 0 | 1 |
getHasManeuver() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
setEpochComment(List) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setEulerComment(List) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setSpinComment(List) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setSpacecraftComment(List) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getManeuver(int) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
addManeuver(APMFile.APMManeuver) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setEpoch(AbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setQuaternionFrameAString(String) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setQuaternionFrameBString(String) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setAttitudeQuaternionDirection(String) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setQuaternion(Quaternion) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setQuaternionDot(Quaternion) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setEulerFrameAString(String) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setEulerFrameBString(String) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setEulerDirection(String) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setEulerRotSeq(String) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setRateFrameString(String) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setRotationAngles(Vector3D) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setRotationRates(Vector3D) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setSpinFrameAString(String) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setSpinFrameBString(String) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setSpinDirection(String) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setSpinAlpha(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setSpinDelta(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setSpinAngle(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setSpinAngleVel(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setNutation(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setNutationPeriod(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setNutationPhase(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setInertiaRefFrameString(String) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setI11(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setI22(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setI33(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setI12(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setI13(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setI23(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getEpochComment() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getEulerComment() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getSpinComment() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getSpacecraftComment() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getNbManeuvers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getManeuvers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getMetaDataComment() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getMetaData() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getEpoch() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getQuaternionFrameAString() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getQuaternionFrameBString() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getAttitudeQuaternionDirection() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getQuaternion() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getQuaternionDot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getEulerFrameAString() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getEulerFrameBString() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getEulerDirection() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getEulerRotSeq() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getRateFrameString() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getRotationAngles() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getRotationRates() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getSpinFrameAString() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getSpinFrameBString() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getSpinDirection() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getSpinAlpha() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getSpinDelta() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getSpinAngle() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getSpinAngleVel() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getNutation() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getNutationPeriod() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getNutationPhase() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getInertiaRefFrameString() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getI11() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getI22() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getI33() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getI12() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getI13() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getI23() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |