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moved old booz airframe file to obsolte dir

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This commit is contained in:
Felix Ruess
2011-01-06 19:42:40 +01:00
parent ba36c61694
commit 570685e969
6 changed files with 106 additions and 106 deletions
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conf/airframes/booz2_Aron.xml → conf/airframes/obsolete/booz2_Aron.xml
+36 -36
View File
@@ -1,37 +1,37 @@
<airframe name="BOOZ2_A2">
<servos min="0" neutral="0" max="0xff">
<servo name="FRONT" no="0" min="0" neutral="0" max="255" />
<servo name="BACK" no="1" min="0" neutral="0" max="255" />
<servo name="RIGHT" no="2" min="0" neutral="0" max="255" />
<servo name="LEFT" no="3" min="0" neutral="0" max="255" />
</servos>
<commands>
<axis name="PITCH" failsafe_value="0" />
<axis name="ROLL" failsafe_value="0" />
<axis name="YAW" failsafe_value="0" />
<axis name="THRUST" failsafe_value="0" />
</commands>
<section name="ACTUATORS_MKK" prefix="ACTUATORS_MKK_">
<define name="NB" value="4" />
<define name="ADDR" value="{ 0x52, 0x54, 0x56, 0x58 }" />
</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="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>
<servos min="0" neutral="0" max="0xff">
<servo name="FRONT" no="0" min="0" neutral="0" max="255" />
<servo name="BACK" no="1" min="0" neutral="0" max="255" />
<servo name="RIGHT" no="2" min="0" neutral="0" max="255" />
<servo name="LEFT" no="3" min="0" neutral="0" max="255" />
</servos>
<commands>
<axis name="PITCH" failsafe_value="0" />
<axis name="ROLL" failsafe_value="0" />
<axis name="YAW" failsafe_value="0" />
<axis name="THRUST" failsafe_value="0" />
</commands>
<section name="ACTUATORS_MKK" prefix="ACTUATORS_MKK_">
<define name="NB" value="4" />
<define name="ADDR" value="{ 0x52, 0x54, 0x56, 0x58 }" />
</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="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_">
@@ -46,10 +46,10 @@
<define name="GYRO_P_SENS" value=" -0.85" integer="16"/>
<define name="GYRO_Q_SENS" value=" -0.85" integer="16"/>
<define name="GYRO_R_SENS" value=" 0.85" integer="16"/>
<define name="ACCEL_X_CHAN" value="5"/>
<define name="ACCEL_Y_CHAN" value="2"/>
<define name="ACCEL_Z_CHAN" value="6"/>
<define name="ACCEL_Z_CHAN" value="6"/>
<define name="ACCEL_X_SENS" value="6.23079413" integer="16"/>
<define name="ACCEL_Y_SENS" value="-6.38411981" integer="16"/>
@@ -62,9 +62,9 @@
<define name="MAG_X_CHAN" value="0"/>
<define name="MAG_Y_CHAN" value="4"/>
<define name="MAG_Z_CHAN" value="2"/>
<define name="MAG_X_NEUTRAL" value="2339"/>
<define name="MAG_Y_NEUTRAL" value="2106"/>
<define name="MAG_Y_NEUTRAL" value="2106"/>
<define name="MAG_Z_NEUTRAL" value="1902"/>
<define name="MAG_X_SENS" value="-4.4039655" integer="16"/>
conf/airframes/booz2_NoVa.xml → conf/airframes/obsolete/booz2_NoVa.xml
+22 -22
View File
@@ -70,18 +70,18 @@
<section name="STABILIZATION_RATE" prefix="STABILIZATION_RATE_">
<!-- setpoints -->
<define name="SP_MAX_P" value="10000" />
<define name="SP_MAX_Q" value="10000" />
<define name="SP_MAX_R" value="10000" />
<define name="SP_MAX_P" value="10000" />
<define name="SP_MAX_Q" value="10000" />
<define name="SP_MAX_R" value="10000" />
<define name="DEADBAND_P" value="0" />
<define name="DEADBAND_Q" value="0" />
<define name="DEADBAND_R" value="200" />
<define name="REF_TAU" value="4" />
<!-- feedback -->
<define name="GAIN_P" value="-400" />
<define name="GAIN_Q" value="-400" />
<define name="GAIN_R" value="-350" />
<define name="GAIN_P" value="-400" />
<define name="GAIN_Q" value="-400" />
<define name="GAIN_R" value="-350" />
<define name="IGAIN_P" value="-75" />
<define name="IGAIN_Q" value="-75" />
@@ -91,7 +91,7 @@
<define name="DDGAIN_P" value="300" />
<define name="DDGAIN_Q" value="300" />
<define name="DDGAIN_R" value="300" />
</section>
</section>
<section name="STABILIZATION_ATTITUDE" prefix="STABILIZATION_ATTITUDE_">
@@ -152,23 +152,23 @@
</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="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>
<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="ACTUATORS_MKK" prefix="ACTUATORS_MKK_">
<define name="NB" value="4" />
<define name="ADDR" value="{ 0x52, 0x56, 0x54, 0x58 }" />
</section>
<define name="NB" value="4" />
<define name="ADDR" value="{ 0x52, 0x56, 0x54, 0x58 }" />
</section>
<section name="INS" prefix="INS_">
<define name="BARO_SENS" value="14.9" integer="16"/>
conf/airframes/booz2_NoVa_001.xml → conf/airframes/obsolete/booz2_NoVa_001.xml
+22 -22
View File
@@ -70,18 +70,18 @@
<section name="STABILIZATION_RATE" prefix="STABILIZATION_RATE_">
<!-- setpoints -->
<define name="SP_MAX_P" value="10000" />
<define name="SP_MAX_Q" value="10000" />
<define name="SP_MAX_R" value="10000" />
<define name="SP_MAX_P" value="10000" />
<define name="SP_MAX_Q" value="10000" />
<define name="SP_MAX_R" value="10000" />
<define name="DEADBAND_P" value="0" />
<define name="DEADBAND_Q" value="0" />
<define name="DEADBAND_R" value="200" />
<define name="REF_TAU" value="4" />
<!-- feedback -->
<define name="GAIN_P" value="-400" />
<define name="GAIN_Q" value="-400" />
<define name="GAIN_R" value="-350" />
<define name="GAIN_P" value="-400" />
<define name="GAIN_Q" value="-400" />
<define name="GAIN_R" value="-350" />
<define name="IGAIN_P" value="-75" />
<define name="IGAIN_Q" value="-75" />
@@ -91,7 +91,7 @@
<define name="DDGAIN_P" value="300" />
<define name="DDGAIN_Q" value="300" />
<define name="DDGAIN_R" value="300" />
</section>
</section>
<section name="STABILIZATION_ATTITUDE" prefix="STABILIZATION_ATTITUDE_">
@@ -152,23 +152,23 @@
</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="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>
<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="ACTUATORS_MKK" prefix="ACTUATORS_MKK_">
<define name="NB" value="4" />
<define name="ADDR" value="{ 0x52, 0x58, 0x54, 0x56 }" />
</section>
<define name="NB" value="4" />
<define name="ADDR" value="{ 0x52, 0x58, 0x54, 0x56 }" />
</section>
<section name="INS" prefix="INS_">
<define name="BARO_SENS" value="14.9" integer="16"/>
conf/airframes/booz2_NoVa_002.xml → conf/airframes/obsolete/booz2_NoVa_002.xml
+22 -22
View File
@@ -70,18 +70,18 @@
<section name="STABILIZATION_RATE" prefix="STABILIZATION_RATE_">
<!-- setpoints -->
<define name="SP_MAX_P" value="10000" />
<define name="SP_MAX_Q" value="10000" />
<define name="SP_MAX_R" value="10000" />
<define name="SP_MAX_P" value="10000" />
<define name="SP_MAX_Q" value="10000" />
<define name="SP_MAX_R" value="10000" />
<define name="DEADBAND_P" value="0" />
<define name="DEADBAND_Q" value="0" />
<define name="DEADBAND_R" value="200" />
<define name="REF_TAU" value="4" />
<!-- feedback -->
<define name="GAIN_P" value="-400" />
<define name="GAIN_Q" value="-400" />
<define name="GAIN_R" value="-350" />
<define name="GAIN_P" value="-400" />
<define name="GAIN_Q" value="-400" />
<define name="GAIN_R" value="-350" />
<define name="IGAIN_P" value="-75" />
<define name="IGAIN_Q" value="-75" />
@@ -91,7 +91,7 @@
<define name="DDGAIN_P" value="300" />
<define name="DDGAIN_Q" value="300" />
<define name="DDGAIN_R" value="300" />
</section>
</section>
<section name="STABILIZATION_ATTITUDE" prefix="STABILIZATION_ATTITUDE_">
@@ -152,23 +152,23 @@
</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="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>
<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="ACTUATORS_MKK" prefix="ACTUATORS_MKK_">
<define name="NB" value="4" />
<define name="ADDR" value="{ 0x54, 0x58, 0x56, 0x52 }" />
</section>
<define name="NB" value="4" />
<define name="ADDR" value="{ 0x54, 0x58, 0x56, 0x52 }" />
</section>
<section name="INS" prefix="INS_">
<define name="BARO_SENS" value="14.9" integer="16"/>
conf/airframes/booz2_s1.xml → conf/airframes/obsolete/booz2_s1.xml
+4 -4
View File
@@ -39,10 +39,10 @@
<define name="GYRO_P_SENS" value=" 1.01" integer="16"/>
<define name="GYRO_Q_SENS" value="-1.01" integer="16"/>
<define name="GYRO_R_SENS" value="-1.01" integer="16"/>
<define name="ACCEL_X_CHAN" value="5"/>
<define name="ACCEL_Y_CHAN" value="3"/>
<define name="ACCEL_Z_CHAN" value="4"/>
<define name="ACCEL_Z_CHAN" value="4"/>
<define name="ACCEL_X_SENS" value="-3.60757190" integer="16"/>
<define name="ACCEL_Y_SENS" value="-3.54533328" integer="16"/>
@@ -55,7 +55,7 @@
<define name="MAG_X_CHAN" value="0"/>
<define name="MAG_Y_CHAN" value="1"/>
<define name="MAG_Z_CHAN" value="2"/>
<define name="MAG_X_NEUTRAL" value="-54"/>
<define name="MAG_Y_NEUTRAL" value="28"/>
@@ -160,7 +160,7 @@
<define name="MILLIAMP_PER_PERCENT" value="0.86"/>
<define name="CATASTROPHIC_BAT_LEVEL" value="9.3" unit="V"/>
<define name="BATTERY_SENS" value="0.245" integer="16"/>
</section>
<section name="AUTOPILOT">
conf/airframes/booz2_x1.xml → conf/airframes/obsolete/booz2_x1.xml
View File