Description

Public Methods

SetTargetCoordType

Selects a target coordinate type.

Public Properties

CentralBodyCollisionAltitudePadding	The minimum altitude below which the Lambert algorithm will consider the spacecraft to have hit the central body.
CoordSystemName	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	This is 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	et 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	This is 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	This is the propagate segment to manipulate that contains the departure delay.
GridSearchTimeStep	This is the time step between Lambert evaluations for searching over both the departure window and arrival window of time.
LatestArrivalTime	This is the latest time from the start of the target sequence that the satellite should arrive at its destination.
LatestDepartureTime	This is the latest time from the start of the target sequence for the first Lambert maneuver to occur.
MaxRevolutions	This is the maximum number of revolutions for the Lambert solution.
SecondManeuverSegment	This is 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	This is the propagate segment to manipulate that contains the transfer duration. It is visible when you select Write Flight Duration to Second Propagate.
TargetArgumentOfPeriapsis	The target argument of periapsis for the end of the Lambert transfer.
TargetCoordType	The target coordinate type.
TargetEccentricity	The target eccentricity for the end of the Lambert transfer.
TargetInclination	The target inclination for the end of the Lambert transfer.
TargetPositionX	The X component of the target position for the end of the Lambert transfer.
TargetPositionY	The Y component of the target position for the end of the Lambert transfer.
TargetPositionZ	The Z component of the target position for the end of the Lambert transfer.
TargetRightAscensionOfAscendingNode	The target right ascension of the ascending node for the end of the Lambert transfer.
TargetSemimajorAxis	The target semimajor axis for the end of the Lambert transfer.
TargetTrueAnomaly	The target true anomaly for the end of the Lambert transfer.
TargetVelocityX	The X component of the target velocity for the end of the Lambert transfer.
TargetVelocityY	The Y component of the target velocity for the end of the Lambert transfer.
TargetVelocityZ	The Z component of the target velocity for the end of the Lambert transfer.

Interfaces

CoClasses that Implement IAgVAProfileLambertSearchProfile