FW_ACRO_X_MAX | px4.parameter.fw_acro_x_max.set | Standard | Float | 90.0 | 10.0..720.0 | deg | - | no | no | Acro body roll max rate setpoint |
FW_ACRO_YAW_EN | px4.parameter.fw_acro_yaw_en.set | Standard | Int32 | 0 | - | - | enum 2 | no | no | Enable yaw rate controller in Acro |
FW_ACRO_Y_MAX | px4.parameter.fw_acro_y_max.set | Standard | Float | 90.0 | 10.0..720.0 | deg | - | no | no | Acro body pitch max rate setpoint |
FW_ACRO_Z_MAX | px4.parameter.fw_acro_z_max.set | Standard | Float | 45.0 | 10.0..720.0 | deg | - | no | no | Acro body yaw max rate setpoint |
FW_ARSP_SCALE_EN | px4.parameter.fw_arsp_scale_en.set | Standard | Int32 | 1 | - | - | enum 2 | no | no | Enable airspeed scaling |
FW_BAT_SCALE_EN | px4.parameter.fw_bat_scale_en.set | Standard | Int32 | 0 | - | - | enum 2 | no | no | Enable throttle scale by battery level |
FW_DTRIM_P_VMAX | px4.parameter.fw_dtrim_p_vmax.set | Standard | Float | 0.0 | -0.5..0.5 | - | - | no | no | Pitch trim increment at maximum airspeed |
FW_DTRIM_P_VMIN | px4.parameter.fw_dtrim_p_vmin.set | Standard | Float | 0.0 | -0.5..0.5 | - | - | no | no | Pitch trim increment at minimum airspeed |
FW_DTRIM_R_VMAX | px4.parameter.fw_dtrim_r_vmax.set | Standard | Float | 0.0 | -0.5..0.5 | - | - | no | no | Roll trim increment at maximum airspeed |
FW_DTRIM_R_VMIN | px4.parameter.fw_dtrim_r_vmin.set | Standard | Float | 0.0 | -0.5..0.5 | - | - | no | no | Roll trim increment at minimum airspeed |
FW_DTRIM_Y_VMAX | px4.parameter.fw_dtrim_y_vmax.set | Standard | Float | 0.0 | -0.5..0.5 | - | - | no | no | Yaw trim increment at maximum airspeed |
FW_DTRIM_Y_VMIN | px4.parameter.fw_dtrim_y_vmin.set | Standard | Float | 0.0 | -0.5..0.5 | - | - | no | no | Yaw trim increment at minimum airspeed |
FW_FLAPS_MAN | px4.parameter.fw_flaps_man.set | Standard | Int32 | 0 | - | - | enum 7 | no | no | Flap input in manual flight |
FW_GC_EN | px4.parameter.fw_gc_en.set | Standard | Int32 | 1 | - | - | enum 2 | no | no | Enable rate gain compression |
FW_GC_GAIN_MIN | px4.parameter.fw_gc_gain_min.set | Standard | Float | 0.3 | 0.0..1.0 | - | - | no | no | Compression gain lower limit |
FW_MAN_P_SC | px4.parameter.fw_man_p_sc.set | Standard | Float | 1.0 | >= 0.0 | norm | - | no | no | Manual pitch scale |
FW_MAN_R_SC | px4.parameter.fw_man_r_sc.set | Standard | Float | 1.0 | 0.0..1.0 | norm | - | no | no | Manual roll scale |
FW_MAN_Y_SC | px4.parameter.fw_man_y_sc.set | Standard | Float | 1.0 | >= 0.0 | norm | - | no | no | Manual yaw scale |
FW_PR_D | px4.parameter.fw_pr_d.set | Standard | Float | 0.0 | 0.0..10.0 | %/rad/s | - | no | no | Pitch rate derivative gain |
FW_PR_FF | px4.parameter.fw_pr_ff.set | Standard | Float | 0.5 | 0.0..10.0 | %/rad/s | - | no | no | Pitch rate feed forward |
FW_PR_I | px4.parameter.fw_pr_i.set | Standard | Float | 0.1 | 0.0..10.0 | %/rad | - | no | no | Pitch rate integrator gain |
FW_PR_IMAX | px4.parameter.fw_pr_imax.set | Standard | Float | 0.4 | 0.0..1.0 | - | - | no | no | Pitch rate integrator limit |
FW_PR_P | px4.parameter.fw_pr_p.set | Standard | Float | 0.08 | 0.0..10.0 | %/rad/s | - | no | no | Pitch rate proportional gain |
FW_RLL_TO_YAW_FF | px4.parameter.fw_rll_to_yaw_ff.set | Standard | Float | 0.0 | >= 0.0 | - | - | no | no | Roll control to yaw control feedforward gain |
FW_RR_D | px4.parameter.fw_rr_d.set | Standard | Float | 0.0 | 0.0..10.0 | %/rad/s | - | no | no | Roll rate derivative gain |
FW_RR_FF | px4.parameter.fw_rr_ff.set | Standard | Float | 0.5 | 0.0..10.0 | %/rad/s | - | no | no | Roll rate feed forward |
FW_RR_I | px4.parameter.fw_rr_i.set | Standard | Float | 0.1 | 0.0..10.0 | %/rad | - | no | no | Roll rate integrator gain |
FW_RR_IMAX | px4.parameter.fw_rr_imax.set | Standard | Float | 0.2 | 0.0..1.0 | - | - | no | no | Roll integrator limit |
FW_RR_P | px4.parameter.fw_rr_p.set | Standard | Float | 0.05 | 0.0..10.0 | %/rad/s | - | no | no | Roll rate proportional gain |
FW_SPOILERS_MAN | px4.parameter.fw_spoilers_man.set | Standard | Int32 | 0 | - | - | enum 7 | no | no | Spoiler input in manual flight |
FW_USE_AIRSPD | px4.parameter.fw_use_airspd.set | Standard | Int32 | 1 | - | - | enum 2 | no | no | Use airspeed for control |
FW_YR_D | px4.parameter.fw_yr_d.set | Standard | Float | 0.0 | 0.0..10.0 | %/rad/s | - | no | no | Yaw rate derivative gain |
FW_YR_FF | px4.parameter.fw_yr_ff.set | Standard | Float | 0.3 | 0.0..10.0 | %/rad/s | - | no | no | Yaw rate feed forward |
FW_YR_I | px4.parameter.fw_yr_i.set | Standard | Float | 0.1 | 0.0..10.0 | %/rad | - | no | no | Yaw rate integrator gain |
FW_YR_IMAX | px4.parameter.fw_yr_imax.set | Standard | Float | 0.2 | 0.0..1.0 | - | - | no | no | Yaw rate integrator limit |
FW_YR_P | px4.parameter.fw_yr_p.set | Standard | Float | 0.05 | 0.0..10.0 | %/rad/s | - | no | no | Yaw rate proportional gain |