From 273a72c45246db45fed8c26410a26e290d1c70b5 Mon Sep 17 00:00:00 2001
From: breadoven <56191411+breadoven@users.noreply.github.com>
Date: Sun, 10 Mar 2024 13:37:16 +0000
Subject: [PATCH] Update Settings.md

---
 docs/Settings.md | 42 ++++++++++++++++++++++++++++++++++++------
 1 file changed, 36 insertions(+), 6 deletions(-)

diff --git a/docs/Settings.md b/docs/Settings.md
index 79278af68f3..61e3fdfe4ab 100644
--- a/docs/Settings.md
+++ b/docs/Settings.md
@@ -2018,7 +2018,7 @@ Calculated 1G of Acc axis Z to use in INS
 
 | Default | Min | Max |
 | --- | --- | --- |
-| 0.0 | 0 | 2000 |
+| 0 | 0 | 2000 |
 
 ---
 
@@ -2744,7 +2744,7 @@ Protocol that is used to send motor updates to ESCs. Possible values - STANDARD,
 
 ### motor_pwm_rate
 
-Output frequency (in Hz) for motor pins.  Applies only to brushed motors. 
+Output frequency (in Hz) for motor pins.  Applies only to brushed motors.
 
 | Default | Min | Max |
 | --- | --- | --- |
@@ -2852,6 +2852,26 @@ Enable the possibility to manually increase the throttle in auto throttle contro
 
 ---
 
+### nav_fw_alt_control_response
+
+Adjusts the deceleration response of fixed wing altitude control as the target altitude is approached. Decrease value to help avoid overshooting the target altitude.
+
+| Default | Min | Max |
+| --- | --- | --- |
+| 20 | 5 | 100 |
+
+---
+
+### nav_fw_auto_climb_rate
+
+Maximum climb/descent rate that UAV is allowed to reach during navigation modes. [cm/s]
+
+| Default | Min | Max |
+| --- | --- | --- |
+| 500 | 10 | 2000 |
+
+---
+
 ### nav_fw_bank_angle
 
 Max roll angle when rolling / turning in GPS assisted modes, is also restrained by global max_angle_inclination_rll
@@ -3012,6 +3032,16 @@ Forward acceleration threshold for bungee launch of throw launch [cm/s/s], 1G =
 
 ---
 
+### nav_fw_launch_allow_throttle_low
+
+Allow launch sequence with throttle maintained low throughout. When main launch sequence completes control is maintained with Nav cruise throttle until sticks moved/throttle raised or control switches to other Nav mode if preselected
+
+| Default | Min | Max |
+| --- | --- | --- |
+| OFF | OFF | ON |
+
+---
+
 ### nav_fw_launch_climb_angle
 
 Climb angle (attitude of model, not climb slope) for launch sequence (degrees), is also restrained by global max_angle_inclination_pit
@@ -3694,21 +3724,21 @@ Maximum D-term attenution percentage for horizontal velocity PID controller (Mul
 
 ### nav_mc_vel_xy_dterm_attenuation_end
 
-A point (in percent of both target and current horizontal velocity) where nav_mc_vel_xy_dterm_attenuation reaches maximum
+Horizontal velocity where nav_mc_vel_xy_dterm_attenuation reaches maximum [m/s]
 
 | Default | Min | Max |
 | --- | --- | --- |
-| 60 | 0 | 100 |
+| 10 | 0 | 100 |
 
 ---
 
 ### nav_mc_vel_xy_dterm_attenuation_start
 
-A point (in percent of both target and current horizontal velocity) where nav_mc_vel_xy_dterm_attenuation begins
+Horizontal velocity where nav_mc_vel_xy_dterm_attenuation begins [m/s]
 
 | Default | Min | Max |
 | --- | --- | --- |
-| 10 | 0 | 100 |
+| 5 | 0 | 100 |
 
 ---