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 |