Description

Public Properties

TimeOfFlight

Fixed time of flight: duration of the vehicle's flight. Uses Time Dimension.

Example

Define missile trajectory

[C#]

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// Set missile trajectory type  missile.SetTrajectoryType(AgEVePropagatorType.ePropagatorBallistic);    // Retrieve the Propagator interface  IAgVePropagatorBallistic trajectory = missile.Trajectory as IAgVePropagatorBallistic;    // Set propagator settings if they should be other than defaults  trajectory.EphemerisInterval.SetExplicitInterval("1 Jan 2012 12:00:00.000", "2 Jan 2012 12:00:00.000");  trajectory.Step = 60.0;    // Set flight parameters  trajectory.SetLaunchType(AgEVeLaunch.eLaunchLLA);  IAgVeLaunchLLA launch = trajectory.Launch as IAgVeLaunchLLA;  launch.Lat = 0.0;  launch.Lon = 0.0;  launch.Alt = 0.0;    // Set impact location type  trajectory.SetImpactLocationType(AgEVeImpactLocation.eImpactLocationPoint);    // Retrieve the impact point interface  IAgVeImpactLocationPoint impactLocation = trajectory.ImpactLocation as IAgVeImpactLocationPoint;  impactLocation.SetLaunchControlType(AgEVeLaunchControl.eLaunchControlFixedTimeOfFlight);    // Retrieve the launch flight interface  IAgVeLaunchControlFixedTimeOfFlight launchControl = impactLocation.LaunchControl as IAgVeLaunchControlFixedTimeOfFlight;  launchControl.TimeOfFlight = 9000.0;    // Configure missile Impact parameters  impactLocation.SetImpactType(AgEVeImpact.eImpactLLA);  IAgVeImpactLLA impact = impactLocation.Impact as IAgVeImpactLLA;  impact.Lat = 12.0;  impact.Lon = 5.0;  impact.Alt = 0.0;    // Propagate Missile  trajectory.Propagate();

Define missile trajectory

[Visual Basic .NET]

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' Set missile trajectory type missile.SetTrajectoryType(AgEVePropagatorType.ePropagatorBallistic) ' Retrieve the Propagator interface Dim trajectory As IAgVePropagatorBallistic = TryCast(missile.Trajectory, IAgVePropagatorBallistic) ' Set propagator settings if they should be other than defaults trajectory.EphemerisInterval.SetExplicitInterval("1 Jan 2012 12:00:00.000", "2 Jan 2012 12:00:00.000") trajectory.[Step] = 60 ' Set flight parameters trajectory.SetLaunchType(AgEVeLaunch.eLaunchLLA) Dim launch As IAgVeLaunchLLA = TryCast(trajectory.Launch, IAgVeLaunchLLA) launch.Lat = 0 launch.Lon = 0 launch.Alt = 0 ' Set impact location type trajectory.SetImpactLocationType(AgEVeImpactLocation.eImpactLocationPoint) ' Retrieve the impact point interface Dim impactLocation As IAgVeImpactLocationPoint = TryCast(trajectory.ImpactLocation, IAgVeImpactLocationPoint) impactLocation.SetLaunchControlType(AgEVeLaunchControl.eLaunchControlFixedTimeOfFlight) ' Retrieve the launch flight interface Dim launchControl As IAgVeLaunchControlFixedTimeOfFlight = TryCast(impactLocation.LaunchControl, IAgVeLaunchControlFixedTimeOfFlight) launchControl.TimeOfFlight = 9000 ' Configure missile Impact parameters impactLocation.SetImpactType(AgEVeImpact.eImpactLLA) Dim impact As IAgVeImpactLLA = TryCast(impactLocation.Impact, IAgVeImpactLLA) impact.Lat = 12 impact.Lon = 5 impact.Alt = 0 ' Propagate Missile trajectory.Propagate()

CoClasses that Implement IAgVeLaunchControlFixedTimeOfFlight