Description
Fixed time of flight interface for missile flight parameters.
Public Properties
 TimeOfFlight | Fixed time of flight: duration of the vehicle's flight. Uses Time Dimension. |
Interfaces
CoClasses that Implement IAgVeLaunchControlFixedTimeOfFlight
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 = -20.0;
impact.Lon = -20.0;
impact.Alt = 0.0;
// Propagate Missile
trajectory.Propagate();
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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 = -20
impact.Lon = -20
impact.Alt = 0
' Propagate Missile
trajectory.Propagate()
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