2013-04-28 19:38:37 +02:00
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<xml>
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2013-06-22 19:58:54 +02:00
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<object name="EKFStateVariance" singleinstance="true" settings="false" category="State">
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2013-04-28 19:38:37 +02:00
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<description>Extended Kalman Filter state covariance</description>
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2013-05-01 19:16:29 +02:00
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<field name="P" units="1^2" type="float">
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<elementnames>
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<elementname>PositionNorth</elementname>
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<elementname>PositionEast</elementname>
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<elementname>PositionDown</elementname>
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<elementname>VelocityNorth</elementname>
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<elementname>VelocityEast</elementname>
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<elementname>VelocityDown</elementname>
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<elementname>AttitudeQ1</elementname>
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<elementname>AttitudeQ2</elementname>
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<elementname>AttitudeQ3</elementname>
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<elementname>AttitudeQ4</elementname>
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<elementname>GyroDriftX</elementname>
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<elementname>GyroDriftY</elementname>
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<elementname>GyroDriftZ</elementname>
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</elementnames>
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</field>
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2013-04-28 19:38:37 +02:00
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<access gcs="readwrite" flight="readwrite"/>
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<telemetrygcs acked="false" updatemode="manual" period="0"/>
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2013-04-28 21:17:51 +02:00
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<telemetryflight acked="false" updatemode="periodic" period="10000"/>
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2013-04-28 19:38:37 +02:00
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<logging updatemode="manual" period="0"/>
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</object>
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</xml>
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