From 05992691eaba0d365cafb6aa38c6bb0d55322560 Mon Sep 17 00:00:00 2001 From: PX4 Jenkins Date: Thu, 8 Mar 2018 22:37:37 -0600 Subject: [PATCH] Update PX4 Firmware metadata Thu Mar 8 22:37:37 CST 2018 --- .../PX4/PX4ParameterFactMetaData.xml | 42 +++++++++++----------- 1 file changed, 22 insertions(+), 20 deletions(-) diff --git a/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml b/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml index 397f1e3..cd61fcb 100644 --- a/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml +++ b/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml @@ -9336,9 +9336,10 @@ Airbrakes need to be enables for your selected model/mixer modules/vtol_att_control - Thottle output during back transition -For ESCs and mixers that support reverse thrust on low PWM values set this to a negative value to apply active breaking -For ESCs that support thrust reversal with a control channel please set VT_B_REV_OUT and set this to a positive value to apply active breaking + Target throttle value for the transition to hover flight. +standard vtol: pusher +tailsitter, tiltrotor: main throttle + Note for standard vtol: For ESCs and mixers that support reverse thrust on low PWM values set this to a negative value to apply active breaking For ESCs that support thrust reversal with a control channel please set VT_B_REV_OUT and set this to a positive value to apply active breaking -1 1 2 @@ -9411,15 +9412,6 @@ to accelerate forward if necessary modules/vtol_att_control - - Fixed wing pitch trim - This parameter allows to adjust the neutral elevon position in fixed wing mode. - -1.0 - 1.0 - 2 - 0.01 - modules/vtol_att_control - QuadChute Max Pitch Maximum pitch angle before QuadChute engages Above this the vehicle will transition back to MC mode and enter failsafe RTL @@ -9444,6 +9436,16 @@ to accelerate forward if necessary 1 modules/vtol_att_control + + Target throttle value for the transition to fixed wing flight. +standard vtol: pusher +tailsitter, tiltrotor: main throttle + 0.0 + 1.0 + 3 + 0.01 + modules/vtol_att_control + Airspeed less front transition time (open loop) The duration of the front transition when there is no airspeed feedback available. @@ -9474,6 +9476,14 @@ to accelerate forward if necessary modules/vtol_att_control + + Defines the time window during which the pusher throttle will be ramped up linearly to VT_F_TRANS_THR during a transition +to fixed wing mode. Zero or negative values will produce an instant throttle rise to VT_F_TRANS_THR + 20 + 2 + 0.01 + modules/vtol_att_control + Position of tilt servo in fw mode 0.0 @@ -9516,14 +9526,6 @@ to accelerate forward if necessary 0.01 modules/vtol_att_control - - Target throttle value for pusher/puller motor during the transition to fw mode - 0.0 - 1.0 - 3 - 0.01 - modules/vtol_att_control - Front transition timeout Time in seconds after which transition will be cancelled. Disabled if set to 0.