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zero gravity heuristic for vibrating heli
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@@ -107,12 +107,33 @@
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</section>
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</section>
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<section name="AHRS" prefix="AHRS_">
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<section name="AHRS" prefix="AHRS_">
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<!--This airframe vibrates a lot, which causes accel measurements in excess of 1g continuously-->
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<define name="GRAVITY_HEURISTIC_FACTOR" value="0"/>
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<!-- values used if no GPS fix, on 3D fix is update by geo_mag module -->
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<!-- values used if no GPS fix, on 3D fix is update by geo_mag module -->
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<define name="H_X" value="0.3770441"/>
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<define name="H_X" value="0.3770441"/>
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<define name="H_Y" value="0.0193986"/>
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<define name="H_Y" value="0.0193986"/>
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<define name="H_Z" value="0.9259921"/>
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<define name="H_Z" value="0.9259921"/>
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</section>
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</section>
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<section name="STABILIZATION_RATE" prefix="STABILIZATION_RATE_">
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<!-- setpoints -->
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<define name="SP_MAX_P" unit="deg/s" value="280"/>
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<define name="SP_MAX_Q" unit="deg/s" value="280"/>
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<define name="SP_MAX_R" unit="deg/s" value="140"/>
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<define name="DEADBAND_P" value="20"/>
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<define name="DEADBAND_Q" value="20"/>
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<define name="DEADBAND_R" value="200"/>
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<!-- feedback -->
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<define name="GAIN_P" value="400"/>
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<define name="GAIN_Q" value="400"/>
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<define name="GAIN_R" value="350"/>
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<define name="IGAIN_P" value="75"/>
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<define name="IGAIN_Q" value="75"/>
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<define name="IGAIN_R" value="50"/>
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</section>
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<section name="STABILIZATION_ATTITUDE" prefix="STABILIZATION_ATTITUDE_">
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<section name="STABILIZATION_ATTITUDE" prefix="STABILIZATION_ATTITUDE_">
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