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- :ref:`ATC_ACCEL_R_MAX <ATC_ACCEL_R_MAX>` : Roll rate acceleration
@@ -23,7 +23,7 @@ For aircraft designed to carry large directly mounted payloads, the maximum valu
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- :ref:`ATC_ACCEL_R_MAX <ATC_ACCEL_R_MAX>` x (min_TOW / max_TOW)
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- :ref:`ATC_ACCEL_Y_MAX <ATC_ACCEL_Y_MAX>` x (min_TOW / max_TOW)
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:ref:`ACRO_YAW_P <ACRO_YAW_P>` should be set to be approximately 0.5 x :ref:`ATC_ACCEL_Y_MAX <ATC_ACCEL_Y_MAX>` / 4500 to ensure that the aircraft can achieve full yaw rate in approximately half a second.
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:ref:`ACRO_Y_RATE<ACRO_Y_RATE>` should be set to be approximately 0.5 x :ref:`ATC_ACCEL_Y_MAX <ATC_ACCEL_Y_MAX>` / 4500 to ensure that the aircraft can achieve full yaw rate in approximately half a second.
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:ref:`ATC_ANG_LIM_TC <ATC_ANG_LIM_TC>` may be increased to provide a very smooth feeling on the sticks at the expense of a slower reaction time.
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@@ -32,22 +32,22 @@ Aerobatic aircraft should keep the :ref:`ATC_ACCEL_P_MAX <ATC_ACCEL_P_MAX>`, :re
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