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| Line 1: |
Line 1: |
| − |
| |
| − | {{PropertiesStart}}
| |
| − | {{Property
| |
| − | |type=double
| |
| − | |name=ApA
| |
| − | |hasget=1
| |
| − | |desc=Actual Apoapsis.
| |
| − | }}
| |
| − | {{Property
| |
| − | |type=double
| |
| − | |name=ApR
| |
| − | |hasget=1
| |
| − | |desc=Apoapsis, including the radius of the planet.
| |
| − | }}
| |
| − | {{Property
| |
| − | |type=double
| |
| − | |name=PeA
| |
| − | |hasget=1
| |
| − | |desc=Actual Periapsis.
| |
| − | }}
| |
| − | {{Property|type=double
| |
| − | |name=PeR
| |
| − | |hasget=1
| |
| − | |desc=Periapsis, including the radius of the planet.
| |
| − | }}
| |
| − | {{Property
| |
| − | |type=double
| |
| − | |name=semiLatusRectum
| |
| − | |hasget=1
| |
| − | |desc=Semi-latus Rectum, half the length of the chord parallel to the directrix through one of the orbit's foci.
| |
| − | }}
| |
| − | {{Property
| |
| − | |type=double
| |
| − | |name=semiMinorAxis
| |
| − | |hasget=1
| |
| − | |desc=Semi-minor Axis, half the length of the shorter axis through the center of the orbit.
| |
| − | }}
| |
| − | {{PropertiesEnd}}
| |
| − |
| |
| − | {{FieldsStart}}
| |
| − | {{Field
| |
| − | |type=bool
| |
| − | |name=activePatch
| |
| − | }}
| |
| − | {{Field
| |
| − | |type=double
| |
| − | |name=altitude
| |
| − | |desc=Height above the surface of the reference body, including liquid bodies.
| |
| − | }}
| |
| − | {{Field
| |
| − | |type=Vector3d
| |
| − | |name=an
| |
| − | }}
| |
| − | {{Field
| |
| − | |type=double
| |
| − | |name=argumentOfPeriapsis
| |
| − | }}
| |
| − | {{Field
| |
| − | |type=double
| |
| − | |name=ClAppr
| |
| − | |desc=Presumably the distance to the target at closest approach agnostic of encounters, in meters).
| |
| − | }}
| |
| − |
| |
| − | {{Field
| |
| − | |type=double
| |
| − | |name=ClEctr1
| |
| − | |desc= presumably as distance to target during the next closest encounter, in meters.
| |
| − | }}
| |
| − |
| |
| − | {{Field
| |
| − | |type=double
| |
| − | |name=ClEctr2
| |
| − | |desc=Second closest encounter, as an unknown quantity (presumably distance to target, in meters).
| |
| − | }}
| |
| − |
| |
| − | {{Field
| |
| − | |type=CelestialBody
| |
| − | |name=closestEncounterBody
| |
| − | |desc=The next celestial body to be encountered.
| |
| − | }}
| |
| − |
| |
| − | {{Field
| |
| − | |type=EncounterSolutionLevel
| |
| − | |name=closestEncounterLevel
| |
| − | |desc=The type of the next closest encounter, constrained to the values enumerated in EncounterSolutionLevel.
| |
| − | }}
| |
| − |
| |
| − | {{Field
| |
| − | |type=Orbit
| |
| − | |name=closestEncounterPath
| |
| − | |desc=The Orbit around the next celestial body to be encountered.
| |
| − | }}
| |
| − |
| |
| − | {{Field
| |
| − | |type=double
| |
| − | |name=closestTgtApprUT
| |
| − | |desc=The time of the next closest approach, in Universal Time.
| |
| − | }}
| |
| − |
| |
| − | {{Field
| |
| − | |type=double
| |
| − | |name=crAppr
| |
| − | |desc=Unknown type of approach type, presumably distance in meters.
| |
| − | }}
| |
| − |
| |
| − | {{Field
| |
| − | |type=bool
| |
| − | |name=debug_returnFullEllipseTrajectory
| |
| − | }}
| |
| − |
| |
| − | {{Field
| |
| − | |type=Vector3
| |
| − | |name=debugAN
| |
| − | }}
| |
| − |
| |
| − | {{Field
| |
| − | |type=Vector3
| |
| − | |name=debugEccVec
| |
| − | }}
| |
| − |
| |
| − | {{Field
| |
| − | |type=Vector3
| |
| − | |name=debugH
| |
| − | }}
| |
| − |
| |
| − | {{Field
| |
| − | |type=Vector3
| |
| − | |name=debugPos
| |
| − | }}
| |
| − |
| |
| − | {{Field
| |
| − | |type=Vector3
| |
| − | |name=debugVel
| |
| − | }}
| |
| − |
| |
| − | {{Field
| |
| − | |type=double
| |
| − | |name=E
| |
| − | }}
| |
| − |
| |
| − | {{Field
| |
| − | |type=double
| |
| − | |name=eccentricAnomaly
| |
| − | |desc=The eccentric anomaly of the orbit, corresponding to the angle between the periapsis and the current projected position on a circle of radius equal to the semimajor axis.
| |
| − | }}
| |
| − |
| |
| − | {{Field
| |
| − | |type=double
| |
| − | |name=eccentricity
| |
| − | |desc=The eccentricity of the orbit, describing the deviation of the orbit from a perfect circle, from 0 to 1 exclusive for elliptical and 1 to infinity exclusive for hyperbolic (0 being circular and 1 being parabolic)
| |
| − | }}
| |
| − |
| |
| − | {{Field
| |
| − | |type=Vector3d
| |
| − | |name=eccVec
| |
| − | |desc=The eccentricity vector of the orbit, whose magnitude is the eccentricity.
| |
| − | }}
| |
| − |
| |
| − | {{Field
| |
| − | |type=double
| |
| − | |name=EndUT
| |
| − | }}
| |
| − |
| |
| − | {{Field
| |
| − | |type=double
| |
| − | |name=epoch
| |
| − | |desc=The reference time of the orbit, presumably in Universal Time.
| |
| − | }}
| |
| − |
| |
| − | {{Field
| |
| − | |type=double
| |
| − | |name=FEVp
| |
| − | }}
| |
| − |
| |
| − | {{Field
| |
| − | |type=double
| |
| − | |name=FEVs
| |
| − | }}
| |
| − |
| |
| − | {{Field
| |
| − | |type=double
| |
| − | |name=fromE
| |
| − | }}
| |
| − |
| |
| − | {{Field
| |
| − | |type=double
| |
| − | |name=fromV
| |
| − | }}
| |
| − |
| |
| − | {{Field
| |
| − | |type=Vector3d
| |
| − | |name=h
| |
| − | |desc=The specific relative angular momentum vector of the orbit in meters squared per second, being specifically relative to the celestial body around which the orbit exists.
| |
| − | }}
| |
| − |
| |
| − | {{Field
| |
| − | |type=double
| |
| − | |name=inclination
| |
| − | |desc=The inclination of the orbit above the reference plane, presumably in degrees.
| |
| − | }}
| |
| − |
| |
| − | {{Field
| |
| − | |type=double
| |
| − | |name=LAN
| |
| − | }}
| |
| − |
| |
| − | {{Field
| |
| − | |type=double
| |
| − | |name=mag
| |
| − | }}
| |
| − |
| |
| − | {{Field
| |
| − | |type=double
| |
| − | |name=meanAnomaly
| |
| − | }}
| |
| − |
| |
| − | {{Field
| |
| − | |type=double
| |
| − | |name=meanAnomalyAtEpoch
| |
| − | }}
| |
| − |
| |
| − | {{Field
| |
| − | |type=double
| |
| − | |name=nearestTT
| |
| − | |desc=Obsolete, Use VesselType or CelestialBodyType instead.
| |
| − | }}
| |
| − |
| |
| − | {{Field
| |
| − | |type=double
| |
| − | |name=ObT
| |
| − | }}
| |
| − |
| |
| − | {{Field
| |
| − | |type=double
| |
| − | |name=ObTAtEpoch
| |
| − | }}
| |
| − |
| |
| − | {{Field
| |
| − | |type=double
| |
| − | |name=orbitalEnergy
| |
| − | }}
| |
| − |
| |
| − | {{Field
| |
| − | |type=double
| |
| − | |name=orbitalSpeed
| |
| − | }}
| |
| − |
| |
| − | {{Field
| |
| − | |type=double
| |
| − | |name=orbitalPercent
| |
| − | }}
| |
| − |
| |
| − | {{Field
| |
| − | |type=PatchTransitionType
| |
| − | |name=patchEndTransition
| |
| − | }}
| |
| − |
| |
| − | {{Field
| |
| − | |type=PatchTransitionType
| |
| − | |name=patchStartTransition
| |
| − | }}
| |
| − |
| |
| − | {{Field
| |
| − | |type=double
| |
| − | |name=period
| |
| − | }}
| |
| − |
| |
| − | {{Field
| |
| − | |type=Vector3d
| |
| − | |name=pos
| |
| − | }}
| |
| − |
| |
| − | {{Field
| |
| − | |type=Orbit
| |
| − | |name=previousPatch
| |
| − | }}
| |
| − |
| |
| − | {{Field
| |
| − | |type=double
| |
| − | |name=radius
| |
| − | }}
| |
| − |
| |
| − | {{Field
| |
| − | |type=CelestialBody
| |
| − | |name=referenceBody
| |
| − | }}
| |
| − |
| |
| − | {{Field
| |
| − | |type=double
| |
| − | |name=sampleInterval
| |
| − | }}
| |
| − |
| |
| − | {{Field
| |
| − | |type=Vector3d
| |
| − | |name=secondaryPosAtTransition1
| |
| − | }}
| |
| − |
| |
| − | {{Field
| |
| − | |type=Vector3d
| |
| − | |name=secondaryPosAtTransition2
| |
| − | }}
| |
| − |
| |
| − | {{Field
| |
| − | |type=double
| |
| − | |name=semiMajorAxis
| |
| − | }}
| |
| − |
| |
| − | {{Field
| |
| − | |type=double
| |
| − | |name=SEVp
| |
| − | }}
| |
| − |
| |
| − | {{Field
| |
| − | |type=double
| |
| − | |name=SEVs
| |
| − | }}
| |
| − |
| |
| − | {{Field
| |
| − | |type=double
| |
| − | |name=StartUT
| |
| − | }}
| |
| − |
| |
| − | {{Field
| |
| − | |type=double
| |
| − | |name=timeToAp
| |
| − | |desc=Time in seconde before reach the actual Apoapsis.
| |
| − | }}
| |
| − |
| |
| − | {{Field
| |
| − | |type=double
| |
| − | |name=timeToPe
| |
| − | |desc=Time in seconde before reach the actual Periapsis.
| |
| − | }}
| |
| − |
| |
| − | {{Field
| |
| − | |type=double
| |
| − | |name=timeToTransition1
| |
| − | }}
| |
| − |
| |
| − | {{Field
| |
| − | |type=double
| |
| − | |name=timeToTransition2
| |
| − | }}
| |
| − |
| |
| − | {{Field
| |
| − | |type=double
| |
| − | |name=toE
| |
| − | }}
| |
| − |
| |
| − | {{Field
| |
| − | |type=double
| |
| − | |name=toV
| |
| − | }}
| |
| − |
| |
| − | {{Field
| |
| − | |type=double
| |
| − | |name=trueAnomaly
| |
| − | }}
| |
| − |
| |
| − | {{Field
| |
| − | |type=double
| |
| − | |name=UTappr
| |
| − | }}
| |
| − |
| |
| − | {{Field
| |
| − | |type=double
| |
| − | |name=UTsoi
| |
| − | }}
| |
| − |
| |
| − | {{Field
| |
| − | |type=double
| |
| − | |name=V
| |
| − | }}
| |
| − |
| |
| − | {{Field
| |
| − | |type=Vector3d
| |
| − | |name=vel
| |
| − | }}
| |
| − | {{FieldsEnd}}
| |
| − |
| |
| − | {{MethodsStart}}
| |
| − |
| |
| − | {{Method
| |
| − | |returntype=static
| |
| − | |name=Orbit
| |
| − | |args=
| |
| − | }}
| |
| − | {{Method
| |
| − | |returntype=public
| |
| − | |name=Orbit
| |
| − | |args={{arg|double|inc}},{{arg|double|e}},{{arg|double|sma}},{{arg|double|lan}},{{arg|double|w}},{{arg|double|mEp}},{{arg|double|t}},{{arg|CelestialBody|body}}
| |
| − | }}
| |
| − |
| |
| − | {{Method
| |
| − | |returntype=void
| |
| − | |name=DrawOrbit
| |
| − | |args=
| |
| − | }}
| |
| − |
| |
| − | {{Method
| |
| − | |returntype=static void
| |
| − | |name=FindClosestPoints
| |
| − | |args={{arg|Orbit|p}},{{arg|Orbit|s}},{{arg|ref double|CD}},{{arg|ref double CCD}},{{arg|ref double|FFp}},{{arg|ref double|FFs}},{{arg|ref double|SFp}},{{arg|ref double SFs}},{{arg|double|epsilon}},{{arg|int|maxIterations}},{{arg|ref int|iterationCount}}
| |
| − | }}
| |
| − |
| |
| − | {{Method
| |
| − | |returntype=Vector3d
| |
| − | |name=GetANVector
| |
| − | |args=
| |
| − | }}
| |
| − |
| |
| − | {{Method
| |
| − | |returntype=double
| |
| − | |name=GetDTforTrueAnomaly
| |
| − | |args={{arg|double|tA}},{{arg|double|wrapAfterSeconds}}
| |
| − | }}
| |
| − |
| |
| − | {{Method
| |
| − | |returntype=double
| |
| − | |name=GetEccentricAnomaly
| |
| − | |args={{arg|double|tA}}
| |
| − | }}
| |
| − |
| |
| − | {{Method
| |
| − | |returntype=Vector3d
| |
| − | |name=GetEccVector
| |
| − | |args=
| |
| − | }}
| |
| − |
| |
| − | {{Method
| |
| − | |returntype=Vector3d
| |
| − | |name=GetFrameVel
| |
| − | |args=
| |
| − | }}
| |
| − |
| |
| − | {{Method
| |
| − | |returntype=Vector3d
| |
| − | |name=GetFrameVelAtUT
| |
| − | |args={{arg|double|UT}}
| |
| − | }}
| |
| − |
| |
| − | {{Method
| |
| − | |returntype=double
| |
| − | |name=GetMeanAnomaly
| |
| − | |args={{arg|double|E}},{{arg|double|tA}}
| |
| − | }}
| |
| − |
| |
| − | {{Method
| |
| − | |returntype=double
| |
| − | |name=getObTAtMeanAnomaly
| |
| − | |args={{arg|double|M}}
| |
| − | }}
| |
| − |
| |
| − | {{Method
| |
| − | |returntype=double
| |
| − | |name=getObtAtUT
| |
| − | |args={{arg|double|UT}}
| |
| − | }}
| |
| − |
| |
| − | {{Method
| |
| − | |returntype=double
| |
| − | |name=getOrbitalSpeedAt
| |
| − | |args={{arg|double|time}}
| |
| − | }}
| |
| − |
| |
| − | {{Method
| |
| − | |returntype=double
| |
| − | |name=getOrbitalSpeedAtDistance
| |
| − | |args={{arg|double|d}}
| |
| − | }}
| |
| − |
| |
| − | {{Method
| |
| − | |returntype=double
| |
| − | |name=getOrbitalSpeedAtPos
| |
| − | |args={{arg|Vector3d|pos}}
| |
| − | }}
| |
| − |
| |
| − | {{Method
| |
| − | |returntype=double
| |
| − | |name=getOrbitalSpeedAtRelativePos
| |
| − | |args={{arg|Vector3d|relPos}}
| |
| − | }}
| |
| − |
| |
| − | {{Method
| |
| − | |returntype=Vector3d
| |
| − | |name=getOrbitalVelocityAtObT
| |
| − | |args={{arg|double|ObT}}
| |
| − | }}
| |
| − |
| |
| − | {{Method
| |
| − | |returntype=Vector3d
| |
| − | |name=getOrbitalVelocityAtUT
| |
| − | |args={{arg|double|UT}}
| |
| − | }}
| |
| − |
| |
| − | {{Method
| |
| − | |returntype=Vector3d
| |
| − | |name=GetOrbitNormal()
| |
| − | |args=
| |
| − | }}
| |
| − |
| |
| − | {{Method
| |
| − | |returntype=Trajectory
| |
| − | |name=GetPatchTrajectory
| |
| − | |args={{arg|int|sampleCount}}
| |
| − | }}
| |
| − |
| |
| − | {{Method
| |
| − | |returntype=Vector3d
| |
| − | |name=getPositionAtT
| |
| − | |args={{arg|double|T}}
| |
| − | }}
| |
| − |
| |
| − | {{Method
| |
| − | |returntype=Vector3d
| |
| − | |name=getPositionAtUT
| |
| − | |args={{arg|double|UT}}
| |
| − | }}
| |
| − |
| |
| − | {{Method
| |
| − | |returntype=Vector3d
| |
| − | |name=getPositionFromEccAnomaly
| |
| − | |args={{arg|double|E}}
| |
| − | }}
| |
| − |
| |
| − | {{Method
| |
| − | |returntype=Vector3d
| |
| − | |name=getPositionFromMeanAnomaly
| |
| − | |args={{arg|double|M}}
| |
| − | }}
| |
| − |
| |
| − | {{Method
| |
| − | |returntype=Vector3d
| |
| − | |name=getPositionFromTrueAnomaly
| |
| − | |args={{arg|double|tA}}
| |
| − |
| |
| − | }}
| |
| − |
| |
| − | {{Method
| |
| − | |returntype=Vector3d
| |
| − | |name=getRelativePositionAtT
| |
| − | |args={{arg|double|T}}
| |
| − |
| |
| − | }}
| |
| − |
| |
| − |
| |
| − |
| |
| − | {{Method
| |
| − | |returntype=Vector3d
| |
| − | |name=getRelativePositionAtUT
| |
| − | |args={{arg|double|UT}}
| |
| − |
| |
| − | }}
| |
| − |
| |
| − |
| |
| − | {{Method
| |
| − | |returntype=Vector3d
| |
| − | |name=getRelativePositionFromEccAnomaly
| |
| − | |args={{arg|double|E}}
| |
| − |
| |
| − | }}
| |
| − |
| |
| − |
| |
| − | {{Method
| |
| − | |returntype=Vector3d
| |
| − | |name=getRelativePositionFromMeanAnomaly
| |
| − | |args={{arg|double|m}}
| |
| − |
| |
| − | }}
| |
| − |
| |
| − |
| |
| − | {{Method
| |
| − | |returntype=Vector3d
| |
| − | |name=getRelativePositionFromTrueAnomaly
| |
| − | |args={{arg|double|tA}}
| |
| − |
| |
| − | }}
| |
| − |
| |
| − |
| |
| − | {{Method
| |
| − | |returntype=Vector3d
| |
| − | |name=GetRelativeVel
| |
| − | |args=
| |
| − |
| |
| − | }}
| |
| − |
| |
| − |
| |
| − | {{Method
| |
| − | |returntype=Vector3d
| |
| − | |name=GetRotFrameVel
| |
| − | |args={{arg|CelestialBody|refBody}}
| |
| − |
| |
| − | }}
| |
| − |
| |
| − |
| |
| − | {{Method
| |
| − | |returntype=double
| |
| − | |name=getTrueAnomaly
| |
| − | |args={{arg|double|E}}
| |
| − |
| |
| − | }}
| |
| − |
| |
| − |
| |
| − | {{Method
| |
| − | |returntype=double
| |
| − | |name=GetTrueAnomalyOfZupVector
| |
| − | |args={{arg|Vector3d|vector}}
| |
| − |
| |
| − | }}
| |
| − |
| |
| − | {{Method
| |
| − | |returntype=Vector3d
| |
| − | |name=getTruePositionAtUT
| |
| − | |args={{arg|double|UT}}
| |
| − |
| |
| − | }}
| |
| − |
| |
| − | {{Method
| |
| − | |returntype=double
| |
| − | |name=GetUTforTrueAnomaly
| |
| − | |args={{arg|double|tA}},{{arg|double|wrapAfterSeconds}}
| |
| − |
| |
| − | }}
| |
| − |
| |
| − | {{Method
| |
| − | |returntype=Vector3d
| |
| − | |name=GetVel
| |
| − | |args=
| |
| − |
| |
| − | }}
| |
| − |
| |
| − | {{Method
| |
| − | |returntype=Vector3d
| |
| − | |name=GetWorldSpaceVel
| |
| − | |args=
| |
| − |
| |
| − | }}
| |
| − |
| |
| − | {{Method
| |
| − | |returntype=static bool
| |
| − | |name=PeApIntersects
| |
| − | |args={{arg|Orbit|primary}},{{arg|Orbit|secondary}},{{arg|double|threshold}}
| |
| − |
| |
| − | }}
| |
| − |
| |
| − | {{Method
| |
| − | |returntype=double
| |
| − | |name=RadiusAtTrueAnomaly
| |
| − | |args={{arg|double|tA}}
| |
| − |
| |
| − | }}
| |
| − |
| |
| − | {{Method
| |
| − | |returntype=static double
| |
| − | |name=SolveClosestApproach
| |
| − | |args={{arg|Orbit|p}},{{arg|Orbit|s}},{{arg|ref double|UT}},{{arg|double|dT}},{{arg|double|threshold}},{{arg|double|MinUT}},{{arg|double|MaxUT}},{{arg|double|epsilon}},{{arg|int|maxIterations}},{{arg|ref int|iterationCount}}
| |
| − |
| |
| − | }}
| |
| − |
| |
| − | {{Method
| |
| − | |returntype=static double
| |
| − | |name=SolveClosestBSP
| |
| − | |args={{arg|ref double|Fp}},{{arg|ref double|Fs}},{{arg|double|Ir}},{{arg|double|dF}},{{arg|Orbit|p}},{{arg|orbit|s}},{{arg|double|epsilon}},{{arg|int|maxIterations}},{{arg|ref int|iterationCount}}
| |
| − |
| |
| − | }}
| |
| − |
| |
| − | {{Method
| |
| − | |returntype=double
| |
| − | |name=solveEccentricAnomaly
| |
| − | |args={{arg|double|M}},{{arg|double|ecc}},{{arg|double|maxError}},{{arg|int|maxIterations}}
| |
| − |
| |
| − | }}
| |
| − |
| |
| − | {{Method
| |
| − | |returntype=static bool
| |
| − | |name=SolveSOI_BSP
| |
| − | |args={{arg|Orbit|p}},{{arg|Orbit|s}},{{arg|ref double|UT}},{{arg|double|dT}},{{arg|double|Rsoi}},{{arg|double|MinUT}},{{arg|double|MaxUT}},{{arg|double|epsilon}},{{arg|int|maxIterations}},{{arg|ref int|iterationCount}}
| |
| − |
| |
| − | }}
| |
| − |
| |
| − | {{Method
| |
| − | |returntype=double
| |
| − | |name=TrueAnomalyAtRadius
| |
| − | |args={{arg|double|R}}
| |
| − |
| |
| − | }}
| |
| − |
| |
| − | {{Method
| |
| − | |returntype=double
| |
| − | |name=TrueAnomalyAtT
| |
| − | |args={{arg|double|T}}
| |
| − |
| |
| − | }}
| |
| − |
| |
| − | {{Method
| |
| − | |returntype=double
| |
| − | |name=TrueAnomalyAtUT
| |
| − | |args={{arg|double|UT}}
| |
| − |
| |
| − | }}
| |
| − |
| |
| − | {{Method
| |
| − | |returntype=void
| |
| − | |name=UpdateFromOrbitAtUT
| |
| − | |args={{arg|Orbit|orbit}},{{arg|double|UT}},{{arg|CelestialBody|toBody}}
| |
| − |
| |
| − | }}
| |
| − |
| |
| − | {{Method
| |
| − | |returntype=void
| |
| − | |name=UpdateFromStateVectors
| |
| − | |args={{arg|Vector3d|pos}},{{arg|Vector3d|vel}},{{arg|CelestialBody|refBody}},{{arg|double|UT}}
| |
| − |
| |
| − | }}
| |
| − |
| |
| − | {{Method
| |
| − | |returntype=void
| |
| − | |name=UpdateFromUT
| |
| − | |args={{arg|double|UT}}
| |
| − |
| |
| − | }}
| |
| − |
| |
| − | {{MethodsEnd}}
| |
| − |
| |
| − | == Enumerations ==
| |
| − | public enum EncounterSolutionLevel
| |
| − | {
| |
| − | :NONE,
| |
| − | :ESCAPE,
| |
| − | :ORBIT_INTERSECT,
| |
| − | :SOI_INTERSECT_2,
| |
| − | :SOI_INTERSECT_1
| |
| − | }
| |
| − |
| |
| − | public enum ObjectType
| |
| − | {
| |
| − | :VESSEL,
| |
| − | :SPACE_DEBRIS,
| |
| − | :CELESTIAL_BODIES,
| |
| − | :UNKOWN_MISC,
| |
| − | :KERBAL
| |
| − | }
| |
| − |
| |
| − | public enum PatchTransitionType{
| |
| − | :INITIAL,
| |
| − | :FINAL,
| |
| − | :ENCOUNTER,
| |
| − | :ESCAPE,
| |
| − | :MANEUVER
| |
| − | }
| |
| − | == Tips ==
| |
| − | -Use '''[[API:FlightGlobals|FlightGlobals]].[[API:FlightGlobals|ActiveVessel]].orbit.ApA''' to get the actual Apoapsis of the vessel controlled by the player.
| |
| − | [[Category:Community API Documentation]]
| |
| | | | |
| | {{PropertiesStart}} | | {{PropertiesStart}} |
The following is a list of publically-accessible fields in Orbit. This includes protected items, which can be accessed by subclasses.
| Signature
|
Description
|
| bool activePatch
|
?
|
| double altitude
|
Height above the surface of the reference body, including liquid bodies.
|
| Vector3d an
|
?
|
| double argumentOfPeriapsis
|
?
|
| double ClAppr
|
Presumably the distance to the target at closest approach agnostic of encounters, in meters).
|
| double ClEctr1
|
presumably as distance to target during the next closest encounter, in meters.
|
| double ClEctr2
|
Second closest encounter, as an unknown quantity (presumably distance to target, in meters).
|
| CelestialBody closestEncounterBody
|
The next celestial body to be encountered.
|
| EncounterSolutionLevel closestEncounterLevel
|
The type of the next closest encounter, constrained to the values enumerated in EncounterSolutionLevel.
|
| Orbit closestEncounterPath
|
The Orbit around the next celestial body to be encountered.
|
| double closestTgtApprUT
|
The time of the next closest approach, in Universal Time.
|
| double crAppr
|
Unknown type of approach type, presumably distance in meters.
|
| bool debug_returnFullEllipseTrajectory
|
?
|
| Vector3 debugAN
|
?
|
| Vector3 debugEccVec
|
?
|
| Vector3 debugH
|
?
|
| Vector3 debugPos
|
?
|
| Vector3 debugVel
|
?
|
| double E
|
?
|
| double eccentricAnomaly
|
The eccentric anomaly of the orbit, corresponding to the angle between the periapsis and the current projected position on a circle of radius equal to the semimajor axis.
|
| double eccentricity
|
The eccentricity of the orbit, describing the deviation of the orbit from a perfect circle, from 0 to 1 exclusive for elliptical and 1 to infinity exclusive for hyperbolic (0 being circular and 1 being parabolic)
|
| Vector3d eccVec
|
The eccentricity vector of the orbit, whose magnitude is the eccentricity.
|
| double EndUT
|
?
|
| double epoch
|
The reference time of the orbit, presumably in Universal Time.
|
| double FEVp
|
?
|
| double FEVs
|
?
|
| double fromE
|
?
|
| double fromV
|
?
|
| Vector3d h
|
The specific relative angular momentum vector of the orbit in meters squared per second, being specifically relative to the celestial body around which the orbit exists.
|
| double inclination
|
The inclination of the orbit above the reference plane, presumably in degrees.
|
| double LAN
|
?
|
| double mag
|
?
|
| double meanAnomaly
|
?
|
| double meanAnomalyAtEpoch
|
?
|
| double nearestTT
|
Obsolete, Use VesselType or CelestialBodyType instead.
|
| double ObT
|
?
|
| double ObTAtEpoch
|
?
|
| double orbitalEnergy
|
?
|
| double orbitalSpeed
|
?
|
| double orbitalPercent
|
?
|
| PatchTransitionType patchEndTransition
|
?
|
| PatchTransitionType patchStartTransition
|
?
|
| double period
|
?
|
| Vector3d pos
|
?
|
| Orbit previousPatch
|
?
|
| double radius
|
?
|
| CelestialBody referenceBody
|
?
|
| double sampleInterval
|
?
|
| Vector3d secondaryPosAtTransition1
|
?
|
| Vector3d secondaryPosAtTransition2
|
?
|
| double semiMajorAxis
|
?
|
| double SEVp
|
?
|
| double SEVs
|
?
|
| double StartUT
|
?
|
| double timeToAp
|
Time in seconde before reach the actual Apoapsis.
|
| double timeToPe
|
Time in seconde before reach the actual Periapsis.
|
| double timeToTransition1
|
?
|
| double timeToTransition2
|
?
|
| double toE
|
?
|
| double toV
|
?
|
| double trueAnomaly
|
?
|
| double UTappr
|
?
|
| double UTsoi
|
?
|
| double V
|
?
|
| Vector3d vel
|
?
|
| Signature |
Description
|
| static Orbit()
|
?
|
| public Orbit(double inc,double e,double sma,double lan,double w,double mEp,double t,CelestialBody body)
|
?
|
| void DrawOrbit()
|
?
|
| static void FindClosestPoints(Orbit p,Orbit s,ref double CD,ref double CCD ,ref double FFp,ref double FFs,ref double SFp,ref double SFs ,double epsilon,int maxIterations,ref int iterationCount)
|
?
|
| Vector3d GetANVector()
|
?
|
| double GetDTforTrueAnomaly(double tA,double wrapAfterSeconds)
|
?
|
| double GetEccentricAnomaly(double tA)
|
?
|
| Vector3d GetEccVector()
|
?
|
| Vector3d GetFrameVel()
|
?
|
| Vector3d GetFrameVelAtUT(double UT)
|
?
|
| double GetMeanAnomaly(double E,double tA)
|
?
|
| double getObTAtMeanAnomaly(double M)
|
?
|
| double getObtAtUT(double UT)
|
?
|
| double getOrbitalSpeedAt(double time)
|
?
|
| double getOrbitalSpeedAtDistance(double d)
|
?
|
| double getOrbitalSpeedAtPos(Vector3d pos)
|
?
|
| double getOrbitalSpeedAtRelativePos(Vector3d relPos)
|
?
|
| Vector3d getOrbitalVelocityAtObT(double ObT)
|
?
|
| Vector3d getOrbitalVelocityAtUT(double UT)
|
?
|
| Vector3d GetOrbitNormal()()
|
?
|
| Trajectory GetPatchTrajectory(int sampleCount)
|
?
|
| Vector3d getPositionAtT(double T)
|
?
|
| Vector3d getPositionAtUT(double UT)
|
?
|
| Vector3d getPositionFromEccAnomaly(double E)
|
?
|
| Vector3d getPositionFromMeanAnomaly(double M)
|
?
|
| Vector3d getPositionFromTrueAnomaly(double tA)
|
?
|
| Vector3d getRelativePositionAtT(double T)
|
?
|
| Vector3d getRelativePositionAtUT(double UT)
|
?
|
| Vector3d getRelativePositionFromEccAnomaly(double E)
|
?
|
| Vector3d getRelativePositionFromMeanAnomaly(double m)
|
?
|
| Vector3d getRelativePositionFromTrueAnomaly(double tA)
|
?
|
| Vector3d GetRelativeVel()
|
?
|
| Vector3d GetRotFrameVel(CelestialBody refBody)
|
?
|
| double getTrueAnomaly(double E)
|
?
|
| double GetTrueAnomalyOfZupVector(Vector3d vector)
|
?
|
| Vector3d getTruePositionAtUT(double UT)
|
?
|
| double GetUTforTrueAnomaly(double tA,double wrapAfterSeconds)
|
?
|
| Vector3d GetVel()
|
?
|
| Vector3d GetWorldSpaceVel()
|
?
|
| static bool PeApIntersects(Orbit primary,Orbit secondary,double threshold)
|
?
|
| double RadiusAtTrueAnomaly(double tA)
|
?
|
| static double SolveClosestApproach(Orbit p,Orbit s,ref double UT,double dT,double threshold,double MinUT,double MaxUT,double epsilon,int maxIterations,ref int iterationCount)
|
?
|
| static double SolveClosestBSP(ref double Fp,ref double Fs,double Ir,double dF,Orbit p,orbit s,double epsilon,int maxIterations,ref int iterationCount)
|
?
|
| double solveEccentricAnomaly(double M,double ecc,double maxError,int maxIterations)
|
?
|
| static bool SolveSOI_BSP(Orbit p,Orbit s,ref double UT,double dT,double Rsoi,double MinUT,double MaxUT,double epsilon,int maxIterations,ref int iterationCount)
|
?
|
| double TrueAnomalyAtRadius(double R)
|
?
|
| double TrueAnomalyAtT(double T)
|
?
|
| double TrueAnomalyAtUT(double UT)
|
?
|
| void UpdateFromOrbitAtUT(Orbit orbit,double UT,CelestialBody toBody)
|
?
|
| void UpdateFromStateVectors(Vector3d pos,Vector3d vel,CelestialBody refBody,double UT)
|
?
|
| void UpdateFromUT(double UT)
|
?
|
