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fix thrust coefs in airframe files

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This commit is contained in:
Felix Ruess
2009-09-10 08:33:03 +00:00
parent 907115e772
commit 934999ccd4
4 changed files with 26 additions and 24 deletions
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conf/airframes/booz2_flixr.xml
+11 -9
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@@ -20,15 +20,17 @@
</section>
<section name="SUPERVISION" prefix="SUPERVISION_">
<define name="MIN_MOTOR" value="2" />
<define name="MAX_MOTOR" value="210" />
<define name="TRIM_A" value="0" />
<define name="TRIM_E" value="0" />
<define name="TRIM_R" value="0" />
<define name="NB_MOTOR" value="4" />
<define name="ROLL_COEF" value="{ 0, 0, -256, 256}" />
<define name="PITCH_COEF" value="{ 256, -256, 0, 0}" />
<define name="YAW_COEF" value="{ 256, 256, -256, -256}" />
<define name="MIN_MOTOR" value="2" />
<define name="MAX_MOTOR" value="210" />
<define name="TRIM_A" value="0" />
<define name="TRIM_E" value="0" />
<define name="TRIM_R" value="0" />
<define name="NB_MOTOR" value="4" />
<define name="SCALE" value="256"/>
<define name="ROLL_COEF" value="{ 0, 0, -256, 256}" />
<define name="PITCH_COEF" value="{ 256, -256, 0, 0}" />
<define name="YAW_COEF" value="{ 256, 256, -256, -256}" />
<define name="THRUST_COEF" value="{ 256, 256, 256, 256}"/>
</section>
<section name="IMU" prefix="IMU_">