Description

SimpleAscent Propagator.

Public Methods

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

Public Properties

EphemerisInterval	Get the propagator's ephemeris interval.
InitialState	Get the initial state.
Step	Step size. Uses Time Dimension.

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