RK78 Object

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Description

The Runge Kutta 7(8) propagator uses 7th order Runge-Kutta propagation with 8th order error control to propagate the Spacecraft orbit. See expanded description.

 

 

Inheritance Hierarchy: Object->Propagator->Integrator->RK78

 

Available In Editions:

Engineer

Mission

 

Timing Precision Mode

This page describes functionality in nanosecond timing precision mode.

Click here to see the documentation for this object in millisecond timing precision mode.

 

Constructors

 

Properties

 

Methods

 

 

See also

Spacecraft Propagators

Setting up an Integrator