From: bcoconni <bcoconni@users.sourceforge.net>
Date: Sun, 9 Aug 2015 17:59:29 +0000 (+0200)
Subject: Fixed the accelerometer that now reports correctly 0g in orbit and 1g when steady... 
X-Git-Url: https://git.mxchange.org/?a=commitdiff_plain;h=adb926eefc5616142b575cdd08db5106d2b23de5;p=flightgear.git

Fixed the accelerometer that now reports correctly 0g in orbit and 1g when steady on ground. Bug report by Thorsten Renk.
---

diff --git a/src/FDM/JSBSim/models/flight_control/FGAccelerometer.cpp b/src/FDM/JSBSim/models/flight_control/FGAccelerometer.cpp
index 11f39835f..2b9b4c5b4 100644
--- a/src/FDM/JSBSim/models/flight_control/FGAccelerometer.cpp
+++ b/src/FDM/JSBSim/models/flight_control/FGAccelerometer.cpp
@@ -92,9 +92,8 @@ bool FGAccelerometer::Run(void )
     
   //aircraft forces
   vAccel = (Accelerations->GetBodyAccel()
-              + Propagate->GetTi2b() * Accelerations->GetGravAccel()
-              + Accelerations->GetPQRdot() * vRadius
-              + Propagate->GetPQR() * (Propagate->GetPQR() * vRadius));
+              + Accelerations->GetPQRidot() * vRadius
+              + Propagate->GetPQRi() * (Propagate->GetPQRi() * vRadius));
 
   // transform to the specified orientation
   vAccel = mT * vAccel;