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Current compensation code is removed so these defines don't do anything anymore. (#3496)
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This commit is contained in:
Christophe De Wagter
2025-07-03 22:43:58 +02:00
committed by GitHub
parent 8511252b9b
commit 834a420e9c
71 changed files with 3 additions and 386 deletions
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conf/airframes/examples/ardrone2.xml
-5
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@@ -84,11 +84,6 @@
<define name="MAG_Y_SENS" value="16." integer="16"/>
<define name="MAG_Z_SENS" value="16." integer="16"/>
<!-- Magneto current calibration -->
<define name="MAG_X_CURRENT_COEF" value="0.0"/>
<define name="MAG_Y_CURRENT_COEF" value="0.0"/>
<define name="MAG_Z_CURRENT_COEF" value="0.0"/>
<define name="BODY_TO_IMU_PHI" value="0." unit="deg"/>
<define name="BODY_TO_IMU_THETA" value="0." unit="deg"/>
<define name="BODY_TO_IMU_PSI" value="0." unit="deg"/>
conf/airframes/examples/ardrone2_gazebo.xml
-5
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@@ -96,11 +96,6 @@
<define name="MAG_Y_SENS" value="16." integer="16"/>
<define name="MAG_Z_SENS" value="16." integer="16"/>
<!-- Magneto current calibration -->
<define name="MAG_X_CURRENT_COEF" value="0.0"/>
<define name="MAG_Y_CURRENT_COEF" value="0.0"/>
<define name="MAG_Z_CURRENT_COEF" value="0.0"/>
<define name="BODY_TO_IMU_PHI" value="0." unit="deg"/>
<define name="BODY_TO_IMU_THETA" value="0." unit="deg"/>
<define name="BODY_TO_IMU_PSI" value="0." unit="deg"/>
conf/airframes/examples/ardrone2_opticflow_hover.xml
-5
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@@ -99,11 +99,6 @@
<define name="MAG_Y_SENS" value="16." integer="16"/>
<define name="MAG_Z_SENS" value="16." integer="16"/>
<!-- Magneto current calibration -->
<define name="MAG_X_CURRENT_COEF" value="0.0"/>
<define name="MAG_Y_CURRENT_COEF" value="0.0"/>
<define name="MAG_Z_CURRENT_COEF" value="0.0"/>
<define name="BODY_TO_IMU_PHI" value="0." unit="deg"/>
<define name="BODY_TO_IMU_THETA" value="0." unit="deg"/>
<define name="BODY_TO_IMU_PSI" value="0." unit="deg"/>
conf/airframes/examples/bebop.xml
-5
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@@ -91,11 +91,6 @@
<define name="MAG_Y_SENS" value="11.1147400462" integer="16"/>
<define name="MAG_Z_SENS" value="11.6479371722" integer="16"/>
<!-- Magneto current calibration -->
<define name="MAG_X_CURRENT_COEF" value="0.0"/>
<define name="MAG_Y_CURRENT_COEF" value="0.0"/>
<define name="MAG_Z_CURRENT_COEF" value="0.0"/>
<define name="BODY_TO_IMU_PHI" value="0." unit="deg"/>
<define name="BODY_TO_IMU_THETA" value="0." unit="deg"/>
<define name="BODY_TO_IMU_PSI" value="0." unit="deg"/>
conf/airframes/examples/ladybird_lisa_s.xml
-4
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@@ -84,10 +84,6 @@
<define name="MAG_Y_SENS" value="4.14629702271" integer="16"/>
<define name="MAG_Z_SENS" value="4.54518768636" integer="16"/>
<!-- MAGNETO CURRENT CALIBRATION -->
<define name="MAG_X_CURRENT_COEF" value="0.0103422023767"/>
<define name="MAG_Y_CURRENT_COEF" value="0.0084568317783"/>
<define name="MAG_Z_CURRENT_COEF" value="-0.01935617335"/>
</section>
<section name="AUTOPILOT">
conf/airframes/examples/ladybird_lisa_s_bluegiga.xml
-5
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@@ -83,11 +83,6 @@
<define name="MAG_X_SENS" value="3.94431833863" integer="16"/>
<define name="MAG_Y_SENS" value="4.14629702271" integer="16"/>
<define name="MAG_Z_SENS" value="4.54518768636" integer="16"/>
<!-- MAGNETO CURRENT CALIBRATION -->
<define name="MAG_X_CURRENT_COEF" value="0.0103422023767"/>
<define name="MAG_Y_CURRENT_COEF" value="0.0084568317783"/>
<define name="MAG_Z_CURRENT_COEF" value="-0.01935617335"/>
</section>
<section name="AUTOPILOT">
conf/airframes/examples/matek_h7_rotorcraft_hitl.xml
-4
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@@ -105,10 +105,6 @@
<define name="MAG_Y_SENS" value="15.9334896814" integer="16"/>
<define name="MAG_Z_SENS" value="15.9429325263" integer="16"/>
<!--define name= "MAG_X_CURRENT_COEF" value="0.0350248861409"/>
<define name= "MAG_Y_CURRENT_COEF" value="-0.0118884242797"/>
<define name= "MAG_Z_CURRENT_COEF" value="0.0176235525201"/-->
<define name="BODY_TO_IMU_PHI" value="0." unit="deg"/>
<define name="BODY_TO_IMU_THETA" value="0." unit="deg"/>
<define name="BODY_TO_IMU_PSI" value="0." unit="deg"/>
conf/airframes/examples/quadrotor_lisa_s.xml
-4
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@@ -83,10 +83,6 @@
<define name="MAG_Y_SENS" value="4.14629702271" integer="16"/>
<define name="MAG_Z_SENS" value="4.54518768636" integer="16"/>
<!-- MAGNETO CURRENT CALIBRATION -->
<define name="MAG_X_CURRENT_COEF" value="0.0103422023767"/>
<define name="MAG_Y_CURRENT_COEF" value="0.0084568317783"/>
<define name="MAG_Z_CURRENT_COEF" value="-0.01935617335"/>
</section>
<section name="AUTOPILOT">