AGI STK Objects 11 Send comments on this topic.
IAgMissile Interface





Description

Interface for a missile object.

Object Model












Public Methods

Public Method IsAttitudeTypeSupported Gets a value indicating whether the specified type can be used.
Public Method IsTrajectoryTypeSupported Gets a value indicating whether the specified type can be used.
Public Method SetAttitudeType Method to set the type of attitude profile used by the missile.
Public Method SetTrajectoryType Method to set the propagator type.

Public Properties

Public Property AccessConstraints Get the constraints imposed on the missile.
Public Property Atmosphere The local atmosphere.
Public Property Attitude Get the missile's attitude profile.
Public Property AttitudeSupportedTypes Returns an array of valid choices.
Public Property AttitudeType Get the type of attitude profile used by the missile.
Public Property ExportTools Returns the IAgMsExportTools interface.
Public Property Graphics Get the missile's 2D Graphics properties.
Public Property GroundEllipses Get the missile's ground ellipses properties.
Public Property RadarClutterMap Returns the radar clutter map.
Public Property RadarCrossSection Returns the radar cross sectoin.
Public Property SpaceEnvironment Returns the missile's SpaceEnvironment properties.
Public Property Trajectory Get the missile's trajectory properties.
Public Property TrajectorySupportedTypes Returns an array of valid choices.
Public Property TrajectoryType Get the propagator type used by the missile.
Public Property VO Get the missile's 3D Graphics properties.

Example

Define missile trajectory
[C#] Copy Code
// 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] Copy Code
' 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()

Create a New Missile (on the current scenario central body)
[MATLAB] Copy Code
% IAgScenario scenario: Scenario object 
missile = scenario.Children.New('eMissile','MyMissile'); 
missile.SetTrajectoryType('ePropagatorBallistic'); 
trajectory = missile.Trajectory; 
trajectory.StartTime = 0; 
trajectory.Launch.Lat = 29; 
trajectory.Launch.Lon = -81; 
trajectory.ImpactLocation.Impact.Lat = 27; 
trajectory.ImpactLocation.Impact.Lon = -43; 
trajectory.ImpactLocation.SetLaunchControlType('eLaunchControlFixedApogeeAlt'); 
trajectory.impactLocation.LaunchControl.ApogeeAlt = 1200;   % km 
trajectory.Propagate; 
 
 

CoClasses that Implement IAgMissile

Name
AgMissile
© 2016 Analytical Graphics, Inc. All Rights Reserved.

STK Programming Interface 11.0.1