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Mise à jour de AttitudePointing authored by Julien LEBLOND's avatar Julien LEBLOND
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AttitudePointing.md
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---
title: AttitudePointing
---
This page describes the content of a CZML document. Please read [Get Started](Get-Started) for an explanation of how a CZML document is put together.
# Attitude Pointing
......@@ -45,7 +44,7 @@ This page describes the content of a CZML document. Please read [Get Started](Ge
**name** - String : Name of the attitude pointing, _default_ : "Attitude pointing of : {name of the satellite}".
**availability** - [TimeInterval](https://cesium.com/learn/cesiumjs/ref-doc/TimeInterval.html) : Time interval when the attitude pointing is displayed, *default* : the time interval of the clock of the header
**availability** - [TimeInterval](https://cesium.com/learn/cesiumjs/ref-doc/TimeInterval.html) : Time interval when the attitude pointing is displayed, _default_ : the time interval of the clock of the header
## Intrinsinc arguments
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**julianDates** - [List of JulianDate](https://cesium.com/learn/cesiumjs/ref-doc/JulianDate.html) : The list of all the JulianDate objects, they represents the julian dates of all instants computed for the attitude pointing.
**pointOnBody** - \[AbstractPointOnBody\](AbstractPointOnBody\] : This represents the Czml object that will create the point at the surface of the body to use it as a reference for the polyline.
**pointOnBody** - [AbstractPointOnBody](AbstractPointOnBody) : This represents the Czml object that will create the point at the surface of the body to use it as a reference for the polyline.
**satelliteAttitudes** - [List of Attitude](https://www.orekit.org/site-orekit-development/apidocs/org/orekit/attitudes/Attitude.html) : This list contains all the attitudes object of the satellite computed during the propagation.
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# Functions
* displayPointingPath() - void : This function allows to display the path of the point in the surface of the body.
* displayPeriodPointingPath - void : The function must be used always after `displayPointingPath()`, it allows to displays the path for a duration of one period of the orbit to not overload the scene.
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