@ -5100,10 +5100,10 @@
@@ -5100,10 +5100,10 @@
<unit > s</unit>
<decimal > 2</decimal>
</parameter>
<parameter name= "MPC_ACC_DOWN_MAX" default= "3.0 " type= "FLOAT" >
<parameter name= "MPC_ACC_DOWN_MAX" default= "3." type= "FLOAT" >
<short_desc > Maximum downwards acceleration in climb rate controlled modes</short_desc>
<min > 2.0 </min>
<max > 15.0 </max>
<min > 2</min>
<max > 15</max>
<unit > m/s^2</unit>
<decimal > 1</decimal>
<increment > 1</increment>
@ -5126,10 +5126,10 @@
@@ -5126,10 +5126,10 @@
<decimal > 2</decimal>
<increment > 1</increment>
</parameter>
<parameter name= "MPC_ACC_UP_MAX" default= "4.0 " type= "FLOAT" >
<parameter name= "MPC_ACC_UP_MAX" default= "4." type= "FLOAT" >
<short_desc > Maximum upwards acceleration in climb rate controlled modes</short_desc>
<min > 2.0 </min>
<max > 15.0 </max>
<min > 2</min>
<max > 15</max>
<unit > m/s^2</unit>
<decimal > 1</decimal>
<increment > 1</increment>
@ -5245,8 +5245,8 @@
@@ -5245,8 +5245,8 @@
<parameter name= "MPC_MANTHR_MIN" default= "0.08" type= "FLOAT" >
<short_desc > Minimum collective thrust in Stabilized mode</short_desc>
<long_desc > The value is mapped to the lowest throttle stick position in Stabilized mode. Too low collective thrust leads to loss of roll/pitch/yaw torque control authority. Airmode is used to keep torque authority with zero thrust (see MC_AIRMODE).</long_desc>
<min > 0.0 </min>
<max > 1.0 </max>
<min > 0</min>
<max > 1</max>
<unit > norm</unit>
<decimal > 2</decimal>
<increment > 0.01</increment>
@ -5270,8 +5270,8 @@
@@ -5270,8 +5270,8 @@
<parameter name= "MPC_MAN_Y_TAU" default= "0.08" type= "FLOAT" >
<short_desc > Manual yaw rate input filter time constant</short_desc>
<long_desc > Not used in Stabilized mode Setting this parameter to 0 disables the filter</long_desc>
<min > 0.0 </min>
<max > 5.0 </max>
<min > 0</min>
<max > 5</max>
<unit > s</unit>
<decimal > 2</decimal>
<increment > 0.01</increment>
@ -5323,7 +5323,7 @@
@@ -5323,7 +5323,7 @@
<parameter name= "MPC_THR_XY_MARG" default= "0.3" type= "FLOAT" >
<short_desc > Horizontal thrust margin</short_desc>
<long_desc > Margin that is kept for horizontal control when higher priority vertical thrust is saturated. To avoid completely starving horizontal control with high vertical error.</long_desc>
<min > 0.0 </min>
<min > 0</min>
<max > 0.5</max>
<unit > norm</unit>
<decimal > 2</decimal>
@ -5367,7 +5367,7 @@
@@ -5367,7 +5367,7 @@
</parameter>
<parameter name= "MPC_VELD_LP" default= "5.0" type= "FLOAT" >
<short_desc > Numerical velocity derivative low pass cutoff frequency</short_desc>
<min > 0.0 </min>
<min > 0</min>
<max > 10</max>
<unit > Hz</unit>
<decimal > 1</decimal>