CentralBodyCollisionAltitudePadding | Gets or sets the minimum altitude below which the Lambert algorithm will consider the spacecraft to have hit the central body. |
CoordSystemName | Gets or sets the coordinate system. |
DisableFirstPropagateNonLambertStopConditions | Set this to true to disable all non-LambertDuration stopping conditions in the first propagate segment. |
DisableSecondPropagateNonLambertStopConditions | Set this to true to disable all non-LambertDuration stopping conditions in the second propagate segment. This is visible when you select Write Flight Duration to Second Propagate. |
EarliestArrivalTime | Gets or sets the earliest time from the start of the target sequence that the satellite should arrive at its destination. |
EnableSecondManeuver | Enable to calculate second maneuver at destination. |
EnableTargetMatchPhase | Set this to true if the satellite should match the phase of the orbit at the target. |
EnableWriteDepartureDelayToFirstPropagate | Set this to true to write the departure delay duration before the Lambert transfer to the 'LambertDuration' stopping condition in the first linked propagate segment. |
EnableWriteDurationToSecondPropagate | Set this to true to write the Lambert duration of transfer to the 'LambertDuration' stopping condition in the second linked propagate segment. |
EnableWriteToFirstManeuver | Set this to true to write the Delta-V solution from Lambert at the start of the transfer to the linked maneuver. |
EnableWriteToSecondManeuver | Set this to true to write the Delta-V solution from Lambert at the end of the transfer to the linked maneuver. It is visible when you select Calculate Second Maneuver At Destination . |
FirstManeuverSegment | Gets or sets the first maneuver segment to manipulate that occurs at the start of the transfer. It is visible when you select Write Initial Inertial Delta-V to Maneuver. |
FirstPropagateSegment | Gets or sets the propagate segment to manipulate that contains the departure delay. |
GridSearchTimeStep | Gets or sets the time step between Lambert evaluations for searching over both the departure window and arrival window of time. |
LatestArrivalTime | Gets or sets the latest time from the start of the target sequence that the satellite should arrive at its destination. |
LatestDepartureTime | Gets or sets the latest time from the start of the target sequence for the first Lambert maneuver to occur. |
MaxRevolutions | Gets or sets the maximum number of revolutions for the Lambert solution. |
SecondManeuverSegment | Gets or sets the second maneuver segment to manipulate that occurs at the end of the transfer. It is visible when you select Write Final Inertial Delta-V to Maneuver. |
SecondPropagateSegment | Gets or sets the propagate segment to manipulate that contains the transfer duration. It is visible when you select Write Flight Duration to Second Propagate. |
TargetArgumentOfPeriapsis | Gets or sets the target argument of periapsis for the end of the Lambert transfer. |
TargetCoordType | Get the target coordinate type. |
TargetEccentricity | Gets or sets the target eccentricity for the end of the Lambert transfer. |
TargetInclination | Gets or sets the target inclination for the end of the Lambert transfer. |
TargetPositionX | Gets or sets the X component of the target position for the end of the Lambert transfer. |
TargetPositionY | Gets or sets the Y component of the target position for the end of the Lambert transfer. |
TargetPositionZ | Gets or sets the Z component of the target position for the end of the Lambert transfer. |
TargetRightAscensionOfAscendingNode | Gets or sets the target right ascension of the ascending node for the end of the Lambert transfer. |
TargetSemimajorAxis | Gets or sets the target semimajor axis for the end of the Lambert transfer. |
TargetTrueAnomaly | Gets or sets the target true anomaly for the end of the Lambert transfer. |
TargetVelocityX | Gets or sets the X component of the target velocity for the end of the Lambert transfer. |
TargetVelocityY | Gets or sets the Y component of the target velocity for the end of the Lambert transfer. |
TargetVelocityZ | Gets or sets the Z component of the target velocity for the end of the Lambert transfer. |