Description

SimpleAscent Propagator.

Public Methods

Propagates the launch vehicle's path using the specified time interval.

Public Properties

EphemerisInterval	The propagator's ephemeris interval.
InitialState	Get the initial state.
StartTime	This property is deprecated. Use EphemerisInterval to configure the propagation interval. Start time. Uses DateFormat Dimension.
Step	Step size. Uses Time Dimension.
StopTime	This property is deprecated. Use EphemerisInterval to configure the propagation interval. Stop time. Uses DateFormat Dimension.
UseScenarioAnalysisTime	This property is deprecated. Use the new Timeline API components to configure the propagator's analysis time. Whether the scenario analysis start/stop times shall be used.

Interfaces

Implemented Interface
IAgVePropagator

CoClasses that Implement IAgVePropagatorSimpleAscent

Name
AgVePropagatorSimpleAscent

Example

Configure the Simple Ascent propagator

[C#]

// Configure time period
propagator.EphemerisInterval.SetExplicitInterval("1 Jan 2012 12:00:00.000", "2 Jan 2012 12:00:00.000");
propagator.Step = 60.0;

// Set the initial state
propagator.InitialState.Launch.AssignGeodetic(38.3721, -77.6402, 25.0);
propagator.InitialState.Burnout.AssignGeodetic(48.1395, -82.5145, 25.0);
propagator.InitialState.BurnoutVel = 7.7258;

// Propagate
propagator.Propagate();

Configure the Simple Ascent propagator

[Visual Basic .NET]

' Configure time period
propagator.EphemerisInterval.SetExplicitInterval("1 Jan 2012 12:00:00.000", "2 Jan 2012 12:00:00.000")
propagator.[Step] = 60

' Set the initial state
propagator.InitialState.Launch.AssignGeodetic(38.3721, -77.6402, 25)
propagator.InitialState.Burnout.AssignGeodetic(48.1395, -82.5145, 25)
propagator.InitialState.BurnoutVel = 7.7258

' Propagate
propagator.Propagate()

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IAgVePropagatorSimpleAscent Interface