Merge pull request #6403 from nmaggioni/nm_settings_md_update

Trigger docs CI on PRs

.github/workflows/docs.yml

@@ -1,5 +1,9 @@
 name: Make sure docs are updated
 on:
+  pull_request:
+    paths:
+      - src/main/fc/settings.yaml
+      - docs/Settings.md
   push:
     paths:
       - src/main/fc/settings.yaml

docs/Settings.md

@@ -277,8 +277,8 @@
 | nav_fw_max_thr | 1700 | Maximum throttle for flying wing in GPS assisted modes |
 | nav_fw_min_thr | 1200 | Minimum throttle for flying wing in GPS assisted modes |
 | nav_fw_pitch2thr | 10 | Amount of throttle applied related to pitch attitude in GPS assisted modes. Throttle = nav_fw_cruise_throttle - (nav_fw_pitch2thr * pitch_angle). (notice that pitch_angle is in degrees and is negative when climbing and positive when diving, and throttle value is constrained between nav_fw_min_thr and nav_fw_max_thr) |
-| nav_fw_pitch2thr_smoothing | 0 | How smoothly the autopilot makes pitch to throttle correction inside a deadband defined by pitch_to_throttle_thresh. |
-| nav_fw_pitch2thr_threshold | 0 | Threshold from average pitch where momentary pitch_to_throttle correction kicks in. [decidegrees] |
+| nav_fw_pitch2thr_smoothing | 6 | How smoothly the autopilot makes pitch to throttle correction inside a deadband defined by pitch_to_throttle_thresh. |
+| nav_fw_pitch2thr_threshold | 50 | Threshold from average pitch where momentary pitch_to_throttle correction kicks in. [decidegrees] |
 | nav_fw_pos_hdg_d | 0 | D gain of heading trajectory PID controller. (Fixedwing, rovers, boats) |
 | nav_fw_pos_hdg_i | 0 | I gain of heading trajectory PID controller. (Fixedwing, rovers, boats) |
 | nav_fw_pos_hdg_p | 60 | P gain of heading PID controller. (Fixedwing, rovers, boats) |
@@ -324,7 +324,7 @@
 | nav_mc_vel_z_i | 50 | I gain of velocity PID controller |
 | nav_mc_vel_z_p | 100 | P gain of velocity PID controller |
 | nav_min_rth_distance | 500 | Minimum distance from homepoint when RTH full procedure will be activated [cm]. Below this distance, the mode will activate at the current location and the final phase is executed (loiter / land). Above this distance, the full procedure is activated, which may include initial climb and flying directly to the homepoint before entering the loiter / land phase. |
-| nav_overrides_motor_stop | ALL_NAV | When set OFF_ALWAYS the navigation system will not take over the control of the motor if the throttle is low (motor will stop). When set to OFF always the navigation system will not take over the control of the motor if the throttle was low even when failsafe is triggered. When set to AUTO_ONLY the navigation system will only take over the control of the throttle in autonomous navigation modes (NAV WP and NAV RTH). When set to ALL_NAV (default) the navigation system will take over the control of the motor completely and never allow the motor to stop even when the throttle is low. This setting only has an effect combined with MOTOR_STOP and is likely to cause a stall if fw_min_throttle_down_pitch isn't set correctly or the pitch estimation is wrong for fixed wing models when not set to ALL_NAV |
+| nav_overrides_motor_stop | ALL_NAV | When set OFF_ALWAYS the navigation system will not take over the control of the motor if the throttle is low (motor will stop). When set to OFF always the navigation system will not take over the control of the motor if the throttle was low even when failsafe is triggered. When set to AUTO_ONLY the navigation system will only take over the control of the throttle in autonomous navigation modes (NAV WP and NAV RTH). When set to ALL_NAV (default) the navigation system will take over the control of the motor completely and never allow the motor to stop even when the throttle is low. This setting only has an effect on NAV modes which take control of the throttle when combined with MOTOR_STOP and is likely to cause a stall if fw_min_throttle_down_pitch isn't set correctly or the pitch estimation is wrong for fixed wing models when not set to ALL_NAV |
 | nav_position_timeout | 5 | If GPS fails wait for this much seconds before switching to emergency landing mode (0 - disable) |
 | nav_rth_abort_threshold | 50000 | RTH sanity checking feature will notice if distance to home is increasing during RTH and once amount of increase exceeds the threshold defined by this parameter, instead of continuing RTH machine will enter emergency landing, self-level and go down safely. Default is 500m which is safe enough for both multirotor machines and airplanes. [cm] |
 | nav_rth_allow_landing | ALWAYS | If set to ON drone will land as a last phase of RTH. |