<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>
<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>
<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>
<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>
<short_desc>Integral gain for vertical velocity error</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>
<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>