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	<id>https://patrius.cnes.fr/index.php?action=history&amp;feed=atom&amp;title=LOFOffsetAttitudeLaw</id>
	<title>LOFOffsetAttitudeLaw - Historique des versions</title>
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	<updated>2026-04-07T05:35:31Z</updated>
	<subtitle>Historique des versions pour cette page sur le wiki</subtitle>
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	<entry>
		<id>https://patrius.cnes.fr/index.php?title=LOFOffsetAttitudeLaw&amp;diff=45&amp;oldid=prev</id>
		<title>Admin : Page créée avec « &lt;syntaxhighlight lang=&quot;java&quot;&gt; public class LOFOffsetAttitudeLaw {      public static void main(String[] args) throws PatriusException {                  // Patrius Dataset... »</title>
		<link rel="alternate" type="text/html" href="https://patrius.cnes.fr/index.php?title=LOFOffsetAttitudeLaw&amp;diff=45&amp;oldid=prev"/>
		<updated>2018-02-13T10:34:25Z</updated>

		<summary type="html">&lt;p&gt;Page créée avec « &amp;lt;syntaxhighlight lang=&amp;quot;java&amp;quot;&amp;gt; public class LOFOffsetAttitudeLaw {      public static void main(String[] args) throws PatriusException {                  // Patrius Dataset... »&lt;/p&gt;
&lt;p&gt;&lt;b&gt;Nouvelle page&lt;/b&gt;&lt;/p&gt;&lt;div&gt;&amp;lt;syntaxhighlight lang=&amp;quot;java&amp;quot;&amp;gt;&lt;br /&gt;
public class LOFOffsetAttitudeLaw {&lt;br /&gt;
&lt;br /&gt;
    public static void main(String[] args) throws PatriusException {&lt;br /&gt;
        &lt;br /&gt;
        // Patrius Dataset initialization (needed for example to get the UTC time&lt;br /&gt;
        PatriusDataset.addResourcesFromPatriusDataset() ;&lt;br /&gt;
&lt;br /&gt;
        // Recovery of the UTC time scale using a &amp;quot;factory&amp;quot; (not to duplicate such unique object)&lt;br /&gt;
        final TimeScale TUC = TimeScalesFactory.getUTC();&lt;br /&gt;
        &lt;br /&gt;
        // Date of the orbit given in UTC time scale)&lt;br /&gt;
        final AbsoluteDate date = new AbsoluteDate(&amp;quot;2010-01-01T12:00:00.000&amp;quot;, TUC);&lt;br /&gt;
        &lt;br /&gt;
        // Getting the frame with wich will defined the orbit parameters&lt;br /&gt;
        // As for time scale, we will use also a &amp;quot;factory&amp;quot;.&lt;br /&gt;
        final Frame GCRF = FramesFactory.getGCRF();&lt;br /&gt;
&lt;br /&gt;
        // Initial orbit&lt;br /&gt;
        final double sma = 7200.e+3;&lt;br /&gt;
        final double exc = 0.01;&lt;br /&gt;
        final double inc = FastMath.toRadians(98.);&lt;br /&gt;
        final double pa = FastMath.toRadians(0.);&lt;br /&gt;
        final double raan = FastMath.toRadians(0.);&lt;br /&gt;
        final double anm = FastMath.toRadians(0.);&lt;br /&gt;
        final double MU = Constants.WGS84_EARTH_MU;&lt;br /&gt;
        &lt;br /&gt;
        final KeplerianParameters par = new KeplerianParameters(sma, exc, inc, pa, raan, anm, PositionAngle.MEAN, MU);&lt;br /&gt;
        final Orbit iniOrbit = new KeplerianOrbit(par, GCRF, date);&lt;br /&gt;
        &lt;br /&gt;
        // Building a first attitude law&lt;br /&gt;
        final AttitudeLaw attitudeLaw0= new LofOffset(LOFType.TNW);&lt;br /&gt;
        final Attitude att0 = attitudeLaw0.getAttitude(iniOrbit);&lt;br /&gt;
        &lt;br /&gt;
        // Building a second attitude law with a 45 deg rotation on Z axis&lt;br /&gt;
        final double psi  = FastMath.toRadians(45.);&lt;br /&gt;
        final double teta = 0.;&lt;br /&gt;
        final double phi  = 0.;&lt;br /&gt;
        final AttitudeLaw attitudeLaw = new LofOffset(LOFType.TNW, RotationOrder.ZYX, psi, teta, phi);&lt;br /&gt;
        final Attitude att = attitudeLaw.getAttitude(iniOrbit);&lt;br /&gt;
        &lt;br /&gt;
        // Rotation of the X axis&lt;br /&gt;
        Vector3D vec0 = att0.getRotation().applyTo(Vector3D.PLUS_I);&lt;br /&gt;
        Vector3D vec  = att.getRotation().applyTo(Vector3D.PLUS_I);&lt;br /&gt;
        double cos = vec.dotProduct(vec0);&lt;br /&gt;
        double ang = FastMath.acos(cos);&lt;br /&gt;
        System.out.println(FastMath.toDegrees(ang));&lt;br /&gt;
        &lt;br /&gt;
        // Rotation of the Y axis&lt;br /&gt;
        vec0 = att0.getRotation().applyTo(Vector3D.PLUS_J);&lt;br /&gt;
        vec  = att.getRotation().applyTo(Vector3D.PLUS_J);&lt;br /&gt;
        cos = vec.dotProduct(vec0);&lt;br /&gt;
        ang = FastMath.acos(cos);&lt;br /&gt;
        System.out.println(FastMath.toDegrees(ang));&lt;br /&gt;
        &lt;br /&gt;
        // Z axis comparison&lt;br /&gt;
        vec0 = att0.getRotation().applyTo(Vector3D.PLUS_K);&lt;br /&gt;
        vec  = att.getRotation().applyTo(Vector3D.PLUS_K);&lt;br /&gt;
        final Vector3D dVec = vec.subtract(vec0);&lt;br /&gt;
        final double norm = dVec.getNorm();&lt;br /&gt;
        System.out.println(norm);&lt;br /&gt;
        &lt;br /&gt;
    }&lt;br /&gt;
&lt;br /&gt;
}&lt;br /&gt;
&amp;lt;/syntaxhighlight&amp;gt;&lt;/div&gt;</summary>
		<author><name>Admin</name></author>
	</entry>
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