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)

Example

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

SetStateIgnoreCB */Satellite/ERS1 Cartesian J4Perturbation "1 Nov 2000 00:00:00.00" "1 Nov 2000 08:00:00.00" 60 J2000 "1 Nov 2000 00:00:00.00" -5465000.513055 4630000.194365 0.0 712.713627 841.292034 7377.687805

ReturnMessage

If activated, Connect returns an acknowledgement message.

Group Membership

This command belongs to the following group(s):

Vehicles

Version

6.2

STK Programming Interface 11.0.1