From 2986192a6e4e786e5ca21a283b85929723cbec14 Mon Sep 17 00:00:00 2001
From: PX4BuildBot <bot@px4.io>
Date: Sun, 15 Mar 2020 17:25:16 +0000
Subject: [PATCH] Update PX4 Firmware metadata Sun Mar 15 17:25:16 UTC 2020

---
 src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml | 8 ++++++++
 1 file changed, 8 insertions(+)

diff --git a/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml b/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml
index 94c10f034..900e3bdd1 100644
--- a/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml
+++ b/src/FirmwarePlugin/PX4/PX4ParameterFactMetaData.xml
@@ -1804,6 +1804,14 @@ Sets the number of standard deviations used by the innovation consistency test</
       <unit>m/s</unit>
       <decimal>2</decimal>
     </parameter>
+    <parameter default="15.0" name="EKF2_GSF_TAS" type="FLOAT">
+      <short_desc>Default value of true airspeed used in EKF-GSF AHRS calculation.
+If no airspeed measurements are avalable, the EKF-GSF AHRS calculation will assume this value of true airspeed when compensating for centripetal acceleration during turns. Set to zero to disable centripetal acceleration compensation during fixed wing flight modes</short_desc>
+      <min>0.0</min>
+      <max>100.0</max>
+      <unit>m/s</unit>
+      <decimal>1</decimal>
+    </parameter>
     <parameter default="1.0e-3" name="EKF2_GYR_B_NOISE" type="FLOAT">
       <short_desc>Process noise for IMU rate gyro bias prediction</short_desc>
       <min>0.0</min>
-- 
2.22.0