RK89 Object

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Description

The Runge Kutta 8(9) propagator uses 8th order Runge-Kutta propagation with 9th order error control to propagate the spacecraft orbit. See expanded description.

 

 

Inheritance Hierarchy: Object->Propagator->Integrator->RK89

 

Available In Editions:

Engineer

Mission

 

Timing Precision Mode

This page describes functionality in millisecond timing precision mode. Millisecond timing precision mode is deprecated and will be removed in a future release. We recommend that you migrate your Mission Plans to nanosecond timing precision mode.

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

 

Constructors

 

Properties

 

Methods

 

 

See also

Spacecraft Propagators

Setting up an Integrator