Aero.satellitescenario.CentralBodyOptions

Central body options used by numerical orbit propagator

Since R2025a

Description

Central body options used by numerical orbit propagator in satellite scenario.

Creation

You can create Aero.satellitescenario.CentralBodyOptions objects using the centralBodyOptions function of a satelliteScenario object.

Properties

CentralBody — Name of central body

Earth (default) | string scalar

Name of the central body, specified a string scalar. This property is read-only.

Data Types: string

UseEarthOrientationParameters — Option to use Earth orientation parameters

false (default) | true

Option to use Earth orientation parameters for the transformation between the Geocentric Celestial Reference Frame (GCRF) and International Terrestrial Reference Frame (ITRF), specified as a logical scalar.

Data Types: logical

EarthOrientationParameterFile — Earth orientation data file

aeroiersdata.mat (default) | MAT-file

Custom list of Earth orientation data, specified in a MAT-file. To create the file, use the aeroReadIERSData function.

Data Types: string

Version History

Introduced in R2025a