diff --git a/tests/CMakeLists.txt b/tests/CMakeLists.txt
index 176527de02..1d60653d28 100644
--- a/tests/CMakeLists.txt
+++ b/tests/CMakeLists.txt
@@ -50,7 +50,8 @@ set(PYTHON_TESTS ResetOutputFiles
                  TestLinearActuator
                  TestPlanet
                  TestLighterThanAir
-                 TestUnusableFuel)
+                 TestUnusableFuel
+                 TestPQRdot)
 
 foreach(test ${PYTHON_TESTS})
   add_test(NAME ${test}
diff --git a/tests/TestPQRdot.py b/tests/TestPQRdot.py
new file mode 100644
index 0000000000..bd33e000e5
--- /dev/null
+++ b/tests/TestPQRdot.py
@@ -0,0 +1,74 @@
+# TestPQRdot.py
+#
+# Regression test for the GitHub issue #1034
+#
+# Copyright (c) 2024 Bertrand Coconnier
+#
+# This program is free software; you can redistribute it and/or modify it under
+# the terms of the GNU General Public License as published by the Free Software
+# Foundation; either version 3 of the License, or (at your option) any later
+# version.
+#
+# This program is distributed in the hope that it will be useful, but WITHOUT
+# ANY WARRANTY; without even the implied warranty of MERCHANTABILITY or FITNESS
+# FOR A PARTICULAR PURPOSE.  See the GNU General Public License for more
+# details.
+#
+# You should have received a copy of the GNU General Public License along with
+# this program; if not, see <http://www.gnu.org/licenses/>
+#
+
+import math
+from JSBSim_utils import JSBSimTestCase, RunTest
+
+
+class TestPQRdot(JSBSimTestCase):
+    def test_pqrdot(self):
+        script_name = "ball_orbit.xml"
+        script_path = self.sandbox.path_to_jsbsim_file("scripts", script_name)
+        fdm = self.create_fdm()
+        fdm.load_script(script_path)
+
+        omega = 0.00007292115
+        p0 = math.radians(15.0)
+        T0 = 2.0 * math.pi / p0
+
+        fdm["ic/p-rad_sec"] = p0
+        fdm.run_ic()
+
+        pm = fdm.get_property_manager()
+
+        sim_time = pm.get_node("simulation/sim-time-sec")
+        p = pm.get_node("velocities/p-rad_sec")
+        q = pm.get_node("velocities/q-rad_sec")
+        r = pm.get_node("velocities/r-rad_sec")
+        pdot = pm.get_node("accelerations/pdot-rad_sec2")
+        qdot = pm.get_node("accelerations/qdot-rad_sec2")
+        rdot = pm.get_node("accelerations/rdot-rad_sec2")
+        pi = pm.get_node("velocities/pi-rad_sec")
+        qi = pm.get_node("velocities/qi-rad_sec")
+        ri = pm.get_node("velocities/ri-rad_sec")
+
+        while sim_time.get_double_value() < 10.0 * T0:
+            fdm.run()
+            t = sim_time.get_double_value()
+            self.assertAlmostEqual(p.get_double_value(), p0, delta=1e-8)
+            self.assertAlmostEqual(
+                q.get_double_value(), omega * math.cos(p0 * t), delta=2e-8
+            )
+            self.assertAlmostEqual(
+                r.get_double_value(), -omega * math.sin(p0 * t), delta=2e-8
+            )
+            self.assertAlmostEqual(pdot.get_double_value(), 0.0, delta=1e-8)
+            self.assertAlmostEqual(
+                qdot.get_double_value(), -omega * p0 * math.sin(p0 * t), delta=1e-8
+            )
+            self.assertAlmostEqual(
+                rdot.get_double_value(), -omega * p0 * math.cos(p0 * t), delta=1e-8
+            )
+            self.assertAlmostEqual(pi.get_double_value(), p0, delta=1e-8)
+            self.assertAlmostEqual(qi.get_double_value(), 0.0, delta=1e-8)
+            self.assertAlmostEqual(ri.get_double_value(), 0.0, delta=1e-8)
+
+
+RunTest(TestPQRdot)