SetStateIgnoreCB

Set the orbit state of a vehicle, ignoring propagation intersections with the central body.

Syntax

SetStateIgnoreCB <SatObjectPath> {ElementSetType} {Parameters}

Description

Set the orbit state of a satellite or the trajectory of a launch vehicle using the {ElementSetType} coordinates. The SetStateIgnoreCB command will set the vehicle's state while ignoring any propagation intersections with the central body.

The format for these commands is the same as the format for the SetState command. Valid values for {ElementSetType} are listed below.

• Cartesian : For format see SetState Cartesian
• Classical : For format see SetState Classical
• Equi : For format see SetState Equi
• Spherical : For format see SetState Spherical
• MixedSpherical : For format see SetState MixedSpherical
• SGP4 : For format see SetState SGP4 (Satellites)
• File : For format see SetState File
• SimpleAscent : For format see SetState SimpleAscent (Launch Vehicle)
• TLE : For format see SetState TLE (Satellites)

Examples

To set the orbit for ERS1 using Cartesian coordinates, while ignoring propagation intersections with the central body:

Return message

Group membership

This command belongs to the following group(s):

Vehicles

Version

11.1.1