From 0bcabd9eb6f955ec7606d34693bde24f616783b5 Mon Sep 17 00:00:00 2001 From: shota Date: Wed, 20 Sep 2023 01:12:48 +0900 Subject: [PATCH] revert changes of pid controller --- docs/Settings.md | 12 +----------- 1 file changed, 1 insertion(+), 11 deletions(-) diff --git a/docs/Settings.md b/docs/Settings.md index 508108e97ee..0ec4bd8a69b 100644 --- a/docs/Settings.md +++ b/docs/Settings.md @@ -5672,19 +5672,9 @@ See tpa_rate. --- -### tpa_on_yaw - -Throttle PID attenuation also reduces influence on YAW for multi-rotor, Should be set to ON for tilting rotors. - -| Default | Min | Max | -| --- | --- | --- | -| OFF | OFF | ON | - ---- - ### tpa_rate -Throttle PID attenuation reduces influence of PDFF on ROLL and PITCH of multi-rotor, PIDFF on ROLL,PITCH,YAW OF fixed_wing as throttle increases. For every 1% throttle after the TPA breakpoint, P is reduced by the TPA rate. +Throttle PID attenuation reduces influence of P on ROLL and PITCH as throttle increases. For every 1% throttle after the TPA breakpoint, P is reduced by the TPA rate. | Default | Min | Max | | --- | --- | --- |