OrbitManeuver() | | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
getAcceleration() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
setAcceleration(int, double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getDv() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
setDv(int, double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getThrust() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
setThrust(int, double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getDeployDv() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
setDeployDv(int, double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setDate(AbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setDuration(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setDeltaMass(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setAccelerationInterpolation(OnOff) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setAccelerationMagnitudeSigma(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setAccelerationDirectionSigma(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setDvMagSigma(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setDvDirSigma(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setThrustEfficiency(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setThrustInterpolation(OnOff) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setThrustIsp(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setThrustMagnitudeSigma(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setThrustDirectionSigma(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setDeployId(String) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setDeployMass(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setDeployDvSigma(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setDeployDirSigma(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setDeployDvRatio(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setDeployDvCda(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getDate() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getDuration() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getDeltaMass() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getAccelerationInterpolation() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getAccelerationMagnitudeSigma() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getAccelerationDirectionSigma() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getDvMagSigma() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getDvDirSigma() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getThrustEfficiency() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getThrustInterpolation() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getThrustIsp() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getThrustMagnitudeSigma() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getThrustDirectionSigma() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getDeployId() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getDeployMass() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getDeployDvSigma() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getDeployDirSigma() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getDeployDvRatio() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getDeployDvCda() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |