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[doc] clarify commment
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Felix Ruess
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@@ -5,7 +5,7 @@
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<description>
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Adaptive attitude and lateral (heading) control for fixedwing aircraft.
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Mostly based on PID and optional reference generators and feedforward gains.
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Adaptive parameters should not be used for normal operation at the moment.
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An experimental adaptive filter is also included to estimate some parameters, but should not be used for normal operation at the moment.
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</description>
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<section name="HORIZONTAL CONTROL" prefix="H_CTL_">
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<define name="COURSE_PGAIN" value="1.0" description="feedback heading P gain"/>
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