@ -4885,17 +4885,18 @@ the setpoint will be capped to MPC_XY_VEL_MAX</short_desc>
@@ -4885,17 +4885,18 @@ the setpoint will be capped to MPC_XY_VEL_MAX</short_desc>
<short_desc>Differential gain for horizontal velocity error. Small values help reduce fast oscillations. If value is too big oscillations will appear again</short_desc>
<min>0.005</min>
<max>0.1</max>
<long_desc>defined as correction acceleration in m/s^2 per m/s^2 velocity derivative</long_desc>
<short_desc>Integral gain for horizontal velocity error</short_desc>
<long_desc>Non-zero value allows to eliminate steady state errors in the presence of disturbances like wind.</long_desc>
<long_desc>defined as correction acceleration in m/s^2 per m velocity integral Non-zero value allows to eliminate steady state errors in the presence of disturbances like wind.</long_desc>
@ -4907,10 +4908,11 @@ the setpoint will be capped to MPC_XY_VEL_MAX</short_desc>
@@ -4907,10 +4908,11 @@ the setpoint will be capped to MPC_XY_VEL_MAX</short_desc>
@ -4933,17 +4935,18 @@ the setpoint will be capped to MPC_XY_VEL_MAX</short_desc>
@@ -4933,17 +4935,18 @@ the setpoint will be capped to MPC_XY_VEL_MAX</short_desc>
<short_desc>Integral gain for vertical velocity error</short_desc>
<long_desc>Non zero value allows hovering thrust estimation on stabilized or autonomous takeoff.</long_desc>
<min>0.01</min>
<max>0.1</max>
<long_desc>defined as correction acceleration in m/s^2 per m velocity integral Non zero value allows hovering thrust estimation on stabilized or autonomous takeoff.</long_desc>
@ -4961,10 +4964,11 @@ the setpoint will be capped to MPC_XY_VEL_MAX</short_desc>
@@ -4961,10 +4964,11 @@ the setpoint will be capped to MPC_XY_VEL_MAX</short_desc>