Made corrections to unit tests based on issue #226

Tudat · Aug 28, 2017 · 992cd78 · 992cd78
1 parent 27f9881
commit 992cd78
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Showing 4 changed files with 5 additions and 5 deletions.
diff --git a/Tudat/Astrodynamics/GroundStations/UnitTests/unitTestPointingAnglesCalculator.cpp b/Tudat/Astrodynamics/GroundStations/UnitTests/unitTestPointingAnglesCalculator.cpp
@@ -168,7 +168,7 @@ BOOST_AUTO_TEST_CASE( test_PointingAnglesCalculator )
                 stationState->getRotationFromBodyFixedToTopocentricFrame( 0.0 ) * inertialToBodyFixedFrame *
                 testCartesianPoint ;
         TUDAT_CHECK_MATRIX_CLOSE_FRACTION(
-                    testPointInLocalFrame, expectedTestPointInLocalFrame, std::numeric_limits< double >::epsilon( ) );
+                    testPointInLocalFrame, expectedTestPointInLocalFrame, ( 10.0 * std::numeric_limits< double >::epsilon( ) ) );
     }
 
 }

diff --git a/...namics/OrbitDetermination/AccelerationPartials/UnitTests/unitTestAccelerationPartials.cpp b/...namics/OrbitDetermination/AccelerationPartials/UnitTests/unitTestAccelerationPartials.cpp
@@ -598,8 +598,8 @@ BOOST_AUTO_TEST_CASE( testRelativisticAccelerationPartial )
 
     // Load spice kernel.
     std::string kernelsPath = input_output::getSpiceKernelPath( );
-    spice_interface::loadSpiceKernelInTudat( kernelsPath + "de-403-masses.tpc");
     spice_interface::loadSpiceKernelInTudat( kernelsPath + "pck00009.tpc");
+    spice_interface::loadSpiceKernelInTudat( kernelsPath + "de-403-masses.tpc");
     spice_interface::loadSpiceKernelInTudat( kernelsPath + "de421.bsp");
 
     // Set vehicle and earth state.
@@ -728,8 +728,8 @@ BOOST_AUTO_TEST_CASE( testEmpiricalAccelerationPartial )
 
     // Load spice kernel.
     std::string kernelsPath = input_output::getSpiceKernelPath( );
-    spice_interface::loadSpiceKernelInTudat( kernelsPath + "de-403-masses.tpc");
     spice_interface::loadSpiceKernelInTudat( kernelsPath + "pck00009.tpc");
+    spice_interface::loadSpiceKernelInTudat( kernelsPath + "de-403-masses.tpc");
     spice_interface::loadSpiceKernelInTudat( kernelsPath + "de421.bsp");
 
     // Set vehicle and earth state.

diff --git a/...trodynamics/OrbitDetermination/ObservationPartials/UnitTests/unitTestPositionPartials.cpp b/...trodynamics/OrbitDetermination/ObservationPartials/UnitTests/unitTestPositionPartials.cpp
@@ -59,10 +59,10 @@ BOOST_AUTO_TEST_CASE( testCartesianStatePartials )
 {
     //Load spice kernels.
     std::string kernelsPath = input_output::getSpiceKernelPath( );
+    loadSpiceKernelInTudat( kernelsPath + "pck00009.tpc");
     loadSpiceKernelInTudat( kernelsPath + "de-403-masses.tpc");
     loadSpiceKernelInTudat( kernelsPath + "de421.bsp");
     loadSpiceKernelInTudat( kernelsPath + "naif0009.tls");
-    loadSpiceKernelInTudat( kernelsPath + "pck00009.tpc");
 
     // Specify initial time
     double initialEphemerisTime = 1.0E7;

diff --git a/...strodynamics/OrbitDetermination/UnitTests/unitTestEstimationFromIdealDataDoubleDouble.cpp b/...strodynamics/OrbitDetermination/UnitTests/unitTestEstimationFromIdealDataDoubleDouble.cpp
@@ -67,7 +67,7 @@ BOOST_AUTO_TEST_CASE( test_EstimationFromPosition )
     {
         BOOST_CHECK_SMALL( std::fabs( estimationError( i ) ), 5.0E-3 );
         BOOST_CHECK_SMALL( std::fabs( estimationError( i + 3 ) ), 5.0E-7 );
-        BOOST_CHECK_SMALL( std::fabs( estimationError( i + 18 ) ), 2.0E-4 );
+        BOOST_CHECK_SMALL( std::fabs( estimationError( i + 18 ) ), 5.0E-4 );
     }
 
     BOOST_CHECK_SMALL( std::fabs( estimationError( 6 ) ), 5.0E-6 );