From adb926eefc5616142b575cdd08db5106d2b23de5 Mon Sep 17 00:00:00 2001
From: bcoconni <bcoconni@users.sourceforge.net>
Date: Sun, 9 Aug 2015 19:59:29 +0200
Subject: [PATCH] Fixed the accelerometer that now reports correctly 0g in
 orbit and 1g when steady on ground. Bug report by Thorsten Renk.

---
 src/FDM/JSBSim/models/flight_control/FGAccelerometer.cpp | 5 ++---
 1 file changed, 2 insertions(+), 3 deletions(-)

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;