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Consistent capital use
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@@ -64,7 +64,7 @@
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PARAM_DEFINE_FLOAT(FW_R_TC, 0.4f);
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PARAM_DEFINE_FLOAT(FW_R_TC, 0.4f);
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/**
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/**
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* Attitude Pitch Time Constant
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* Attitude pitch time constant
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*
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*
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* This defines the latency between a pitch step input and the achieved setpoint
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* This defines the latency between a pitch step input and the achieved setpoint
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* (inverse to a P gain). Half a second is a good start value and fits for
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* (inverse to a P gain). Half a second is a good start value and fits for
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@@ -186,7 +186,7 @@ PARAM_DEFINE_FLOAT(FW_RR_P, 0.05f);
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PARAM_DEFINE_FLOAT(FW_RR_I, 0.01f);
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PARAM_DEFINE_FLOAT(FW_RR_I, 0.01f);
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/**
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/**
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* Roll Integrator Anti-Windup
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* Roll integrator anti-windup
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*
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*
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* The portion of the integrator part in the control surface deflection is limited to this value.
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* The portion of the integrator part in the control surface deflection is limited to this value.
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*
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*
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@@ -199,7 +199,7 @@ PARAM_DEFINE_FLOAT(FW_RR_I, 0.01f);
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PARAM_DEFINE_FLOAT(FW_RR_IMAX, 0.2f);
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PARAM_DEFINE_FLOAT(FW_RR_IMAX, 0.2f);
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/**
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/**
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* Maximum Roll Rate
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* Maximum roll rate
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*
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*
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* This limits the maximum roll rate the controller will output (in degrees per
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* This limits the maximum roll rate the controller will output (in degrees per
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* second). Setting a value of zero disables the limit.
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* second). Setting a value of zero disables the limit.
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@@ -258,7 +258,7 @@ PARAM_DEFINE_FLOAT(FW_YR_I, 0.0f);
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PARAM_DEFINE_FLOAT(FW_YR_IMAX, 0.2f);
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PARAM_DEFINE_FLOAT(FW_YR_IMAX, 0.2f);
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/**
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/**
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* Maximum Yaw Rate
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* Maximum yaw rate
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*
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*
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* This limits the maximum yaw rate the controller will output (in degrees per
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* This limits the maximum yaw rate the controller will output (in degrees per
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* second). Setting a value of zero disables the limit.
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* second). Setting a value of zero disables the limit.
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@@ -444,7 +444,7 @@ PARAM_DEFINE_FLOAT(FW_YCO_VMIN, 1000.0f);
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PARAM_DEFINE_INT32(FW_YCO_METHOD, 0);
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PARAM_DEFINE_INT32(FW_YCO_METHOD, 0);
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/**
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/**
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* Roll Setpoint Offset
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* Roll setpoint offset
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*
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*
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* An airframe specific offset of the roll setpoint in degrees, the value is
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* An airframe specific offset of the roll setpoint in degrees, the value is
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* added to the roll setpoint and should correspond to the typical cruise speed
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* added to the roll setpoint and should correspond to the typical cruise speed
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@@ -460,7 +460,7 @@ PARAM_DEFINE_INT32(FW_YCO_METHOD, 0);
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PARAM_DEFINE_FLOAT(FW_RSP_OFF, 0.0f);
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PARAM_DEFINE_FLOAT(FW_RSP_OFF, 0.0f);
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/**
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/**
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* Pitch Setpoint Offset
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* Pitch setpoint offset
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*
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*
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* An airframe specific offset of the pitch setpoint in degrees, the value is
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* An airframe specific offset of the pitch setpoint in degrees, the value is
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* added to the pitch setpoint and should correspond to the typical cruise
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* added to the pitch setpoint and should correspond to the typical cruise
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@@ -476,7 +476,7 @@ PARAM_DEFINE_FLOAT(FW_RSP_OFF, 0.0f);
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PARAM_DEFINE_FLOAT(FW_PSP_OFF, 0.0f);
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PARAM_DEFINE_FLOAT(FW_PSP_OFF, 0.0f);
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/**
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/**
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* Max Manual Roll
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* Max manual roll
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*
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*
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* Max roll for manual control in attitude stabilized mode
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* Max roll for manual control in attitude stabilized mode
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*
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*
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@@ -490,7 +490,7 @@ PARAM_DEFINE_FLOAT(FW_PSP_OFF, 0.0f);
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PARAM_DEFINE_FLOAT(FW_MAN_R_MAX, 45.0f);
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PARAM_DEFINE_FLOAT(FW_MAN_R_MAX, 45.0f);
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/**
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/**
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* Max Manual Pitch
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* Max manual pitch
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*
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*
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* Max pitch for manual control in attitude stabilized mode
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* Max pitch for manual control in attitude stabilized mode
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*
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*
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