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mc_pos_control_params: remove forgotten trailing zeroes
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@@ -35,25 +35,25 @@
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* Maximum upwards acceleration in climb rate controlled modes
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* Maximum upwards acceleration in climb rate controlled modes
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*
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*
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* @unit m/s^2
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* @unit m/s^2
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* @min 2.0
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* @min 2
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* @max 15.0
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* @max 15
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* @decimal 1
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* @decimal 1
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* @increment 1
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* @increment 1
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* @group Multicopter Position Control
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* @group Multicopter Position Control
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*/
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*/
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PARAM_DEFINE_FLOAT(MPC_ACC_UP_MAX, 4.0f);
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PARAM_DEFINE_FLOAT(MPC_ACC_UP_MAX, 4.f);
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/**
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/**
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* Maximum downwards acceleration in climb rate controlled modes
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* Maximum downwards acceleration in climb rate controlled modes
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*
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*
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* @unit m/s^2
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* @unit m/s^2
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* @min 2.0
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* @min 2
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* @max 15.0
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* @max 15
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* @decimal 1
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* @decimal 1
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* @increment 1
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* @increment 1
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* @group Multicopter Position Control
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* @group Multicopter Position Control
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*/
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*/
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PARAM_DEFINE_FLOAT(MPC_ACC_DOWN_MAX, 3.0f);
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PARAM_DEFINE_FLOAT(MPC_ACC_DOWN_MAX, 3.f);
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/**
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/**
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* Manual yaw rate input filter time constant
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* Manual yaw rate input filter time constant
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@@ -62,8 +62,8 @@ PARAM_DEFINE_FLOAT(MPC_ACC_DOWN_MAX, 3.0f);
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* Setting this parameter to 0 disables the filter
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* Setting this parameter to 0 disables the filter
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*
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*
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* @unit s
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* @unit s
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* @min 0.0
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* @min 0
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* @max 5.0
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* @max 5
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* @decimal 2
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* @decimal 2
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* @increment 0.01
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* @increment 0.01
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* @group Multicopter Position Control
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* @group Multicopter Position Control
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@@ -66,7 +66,7 @@ PARAM_DEFINE_INT32(MPC_USE_HTE, 1);
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* To avoid completely starving horizontal control with high vertical error.
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* To avoid completely starving horizontal control with high vertical error.
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*
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*
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* @unit norm
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* @unit norm
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* @min 0.0
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* @min 0
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* @max 0.5
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* @max 0.5
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* @decimal 2
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* @decimal 2
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* @increment 0.01
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* @increment 0.01
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@@ -78,7 +78,7 @@ PARAM_DEFINE_FLOAT(MPC_THR_XY_MARG, 0.3f);
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* Numerical velocity derivative low pass cutoff frequency
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* Numerical velocity derivative low pass cutoff frequency
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*
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*
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* @unit Hz
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* @unit Hz
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* @min 0.0
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* @min 0
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* @max 10
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* @max 10
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* @decimal 1
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* @decimal 1
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* @increment 0.5
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* @increment 0.5
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@@ -64,8 +64,8 @@ PARAM_DEFINE_FLOAT(MPC_MAN_Y_MAX, 150.f);
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* Airmode is used to keep torque authority with zero thrust (see MC_AIRMODE).
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* Airmode is used to keep torque authority with zero thrust (see MC_AIRMODE).
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*
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*
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* @unit norm
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* @unit norm
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* @min 0.0
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* @min 0
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* @max 1.0
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* @max 1
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* @decimal 2
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* @decimal 2
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* @increment 0.01
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* @increment 0.01
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* @group Multicopter Position Control
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* @group Multicopter Position Control
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