PX4 parameter group: FW Rate Control

This page lists named parameter set commands in the PX4 FW Rate Control group. All commands use PARAM_SET and are governed by PX4_COMMAND_MODE, operator guard, and PX4_PARAMETER_WRITE_ALLOWLIST.
MetricCount
Parameters36
FLOAT29
INT327
Standard36
System0
Developer0
Reboot required0
volatile0

Parameters

PX4 ParameterCommand typeCategoryTypeDefaultRangeUnitShapeRebootVolatilePX4 short description
FW_ACRO_X_MAXpx4.parameter.fw_acro_x_max.setStandardFloat90.010.0..720.0deg-nonoAcro body roll max rate setpoint
FW_ACRO_YAW_ENpx4.parameter.fw_acro_yaw_en.setStandardInt320--enum 2nonoEnable yaw rate controller in Acro
FW_ACRO_Y_MAXpx4.parameter.fw_acro_y_max.setStandardFloat90.010.0..720.0deg-nonoAcro body pitch max rate setpoint
FW_ACRO_Z_MAXpx4.parameter.fw_acro_z_max.setStandardFloat45.010.0..720.0deg-nonoAcro body yaw max rate setpoint
FW_ARSP_SCALE_ENpx4.parameter.fw_arsp_scale_en.setStandardInt321--enum 2nonoEnable airspeed scaling
FW_BAT_SCALE_ENpx4.parameter.fw_bat_scale_en.setStandardInt320--enum 2nonoEnable throttle scale by battery level
FW_DTRIM_P_VMAXpx4.parameter.fw_dtrim_p_vmax.setStandardFloat0.0-0.5..0.5--nonoPitch trim increment at maximum airspeed
FW_DTRIM_P_VMINpx4.parameter.fw_dtrim_p_vmin.setStandardFloat0.0-0.5..0.5--nonoPitch trim increment at minimum airspeed
FW_DTRIM_R_VMAXpx4.parameter.fw_dtrim_r_vmax.setStandardFloat0.0-0.5..0.5--nonoRoll trim increment at maximum airspeed
FW_DTRIM_R_VMINpx4.parameter.fw_dtrim_r_vmin.setStandardFloat0.0-0.5..0.5--nonoRoll trim increment at minimum airspeed
FW_DTRIM_Y_VMAXpx4.parameter.fw_dtrim_y_vmax.setStandardFloat0.0-0.5..0.5--nonoYaw trim increment at maximum airspeed
FW_DTRIM_Y_VMINpx4.parameter.fw_dtrim_y_vmin.setStandardFloat0.0-0.5..0.5--nonoYaw trim increment at minimum airspeed
FW_FLAPS_MANpx4.parameter.fw_flaps_man.setStandardInt320--enum 7nonoFlap input in manual flight
FW_GC_ENpx4.parameter.fw_gc_en.setStandardInt321--enum 2nonoEnable rate gain compression
FW_GC_GAIN_MINpx4.parameter.fw_gc_gain_min.setStandardFloat0.30.0..1.0--nonoCompression gain lower limit
FW_MAN_P_SCpx4.parameter.fw_man_p_sc.setStandardFloat1.0>= 0.0norm-nonoManual pitch scale
FW_MAN_R_SCpx4.parameter.fw_man_r_sc.setStandardFloat1.00.0..1.0norm-nonoManual roll scale
FW_MAN_Y_SCpx4.parameter.fw_man_y_sc.setStandardFloat1.0>= 0.0norm-nonoManual yaw scale
FW_PR_Dpx4.parameter.fw_pr_d.setStandardFloat0.00.0..10.0%/rad/s-nonoPitch rate derivative gain
FW_PR_FFpx4.parameter.fw_pr_ff.setStandardFloat0.50.0..10.0%/rad/s-nonoPitch rate feed forward
FW_PR_Ipx4.parameter.fw_pr_i.setStandardFloat0.10.0..10.0%/rad-nonoPitch rate integrator gain
FW_PR_IMAXpx4.parameter.fw_pr_imax.setStandardFloat0.40.0..1.0--nonoPitch rate integrator limit
FW_PR_Ppx4.parameter.fw_pr_p.setStandardFloat0.080.0..10.0%/rad/s-nonoPitch rate proportional gain
FW_RLL_TO_YAW_FFpx4.parameter.fw_rll_to_yaw_ff.setStandardFloat0.0>= 0.0--nonoRoll control to yaw control feedforward gain
FW_RR_Dpx4.parameter.fw_rr_d.setStandardFloat0.00.0..10.0%/rad/s-nonoRoll rate derivative gain
FW_RR_FFpx4.parameter.fw_rr_ff.setStandardFloat0.50.0..10.0%/rad/s-nonoRoll rate feed forward
FW_RR_Ipx4.parameter.fw_rr_i.setStandardFloat0.10.0..10.0%/rad-nonoRoll rate integrator gain
FW_RR_IMAXpx4.parameter.fw_rr_imax.setStandardFloat0.20.0..1.0--nonoRoll integrator limit
FW_RR_Ppx4.parameter.fw_rr_p.setStandardFloat0.050.0..10.0%/rad/s-nonoRoll rate proportional gain
FW_SPOILERS_MANpx4.parameter.fw_spoilers_man.setStandardInt320--enum 7nonoSpoiler input in manual flight
FW_USE_AIRSPDpx4.parameter.fw_use_airspd.setStandardInt321--enum 2nonoUse airspeed for control
FW_YR_Dpx4.parameter.fw_yr_d.setStandardFloat0.00.0..10.0%/rad/s-nonoYaw rate derivative gain
FW_YR_FFpx4.parameter.fw_yr_ff.setStandardFloat0.30.0..10.0%/rad/s-nonoYaw rate feed forward
FW_YR_Ipx4.parameter.fw_yr_i.setStandardFloat0.10.0..10.0%/rad-nonoYaw rate integrator gain
FW_YR_IMAXpx4.parameter.fw_yr_imax.setStandardFloat0.20.0..1.0--nonoYaw rate integrator limit
FW_YR_Ppx4.parameter.fw_yr_p.setStandardFloat0.050.0..10.0%/rad/s-nonoYaw rate proportional gain