Updated unit test data

rdoddanavar · Dec 8, 2024 · 53b402e · 53b402e
1 parent c051868
commit 53b402e
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Showing 16 changed files with 173 additions and 173 deletions.
diff --git a/tools/unit_test/windows/run1/input.yml b/tools/unit_test/windows/run1/input.yml
@@ -1,12 +1,12 @@
-# 2024-12-07 10:40:32
+# 2024-12-07 18:43:34
 # hpr-sim v0.0.0
 # Run: 1/5
 ---
 exec:
     mcMode:
         value: nominal
     seed:
-        value: 0
+        value: 129745503399974868
     numMC:
         value: 1
     procMode:
@@ -29,7 +29,7 @@ engine:
         value: input/AeroTech_J450DM.eng
 mass:
     massBody:
-        value: 4.897012985685388
+        value: 5.443846838408149
         unit: lbm
         dist:
             name: normal

diff --git a/tools/unit_test/windows/run1/stats.yml b/tools/unit_test/windows/run1/stats.yml
@@ -1,11 +1,11 @@
-# 2024-12-07 10:40:32
+# 2024-12-07 18:43:34
 # hpr-sim v0.0.0
 # Run: 1/5
 ---
 time:
     unit: s
     min: 0.000
-    max: 67.081
+    max: 62.129
 thrust:
     unit: N
     min: 0.000
@@ -16,64 +16,64 @@ massEng:
     max: 1.223
 mass:
     unit: kg
-    min: 2.934
-    max: 3.444
+    min: 3.182
+    max: 3.692
 gravity:
     unit: m/s^2
-    min: 9.779
+    min: 9.781
     max: 9.795
 temperature:
     unit: K
-    min: 253.641
+    min: 258.620
     max: 288.150
 pressure:
     unit: Pa
-    min: 51866.551
+    min: 57439.543
     max: 101325.000
 density:
     unit: kg/m^3
-    min: 0.712
+    min: 0.774
     max: 1.225
 dynamicPressure:
     unit: Pa
     min: 0.000
-    max: 63702.160
+    max: 54504.680
 mach:
     unit: null
     min: 0.000
-    max: 0.948
+    max: 0.877
 alphaT:
     unit: rad
     min: 0.000
     max: 0.000
 dragCoeff:
     unit: null
     min: 0.455
-    max: 0.600
+    max: 0.522
 dragForce:
     unit: N
     min: 0.000
-    max: 309.725
+    max: 230.512
 liftForce:
     unit: N
     min: 0.000
     max: 0.000
 forceZ:
     unit: N
-    min: -28.741
-    max: 509.855
+    min: -31.171
+    max: 507.425
 linAccZ:
     unit: m/s^2
     min: -9.795
-    max: 161.351
+    max: 148.825
 linVelZ:
     unit: m/s
-    min: -322.499
-    max: 311.390
+    min: -298.327
+    max: 287.230
 linPosZ:
     unit: m
     min: 0.000
-    max: 5313.541
+    max: 4546.312
 isBurnout:
     unit: null
     min: 0.000

diff --git a/tools/unit_test/windows/run1/telem.npy b/tools/unit_test/windows/run1/telem.npy
diff --git a/tools/unit_test/windows/run2/input.yml b/tools/unit_test/windows/run2/input.yml
@@ -1,12 +1,12 @@
-# 2024-12-07 10:40:32
+# 2024-12-07 18:43:34
 # hpr-sim v0.0.0
 # Run: 2/5
 ---
 exec:
     mcMode:
         value: nominal
     seed:
-        value: 1
+        value: 2377483205311176162
     numMC:
         value: 1
     procMode:
@@ -29,7 +29,7 @@ engine:
         value: input/AeroTech_J450DM.eng
 mass:
     massBody:
-        value: 5.280727605592823
+        value: 5.439992288858991
         unit: lbm
         dist:
             name: normal

diff --git a/tools/unit_test/windows/run2/stats.yml b/tools/unit_test/windows/run2/stats.yml
@@ -1,11 +1,11 @@
-# 2024-12-07 10:40:32
+# 2024-12-07 18:43:34
 # hpr-sim v0.0.0
 # Run: 2/5
 ---
 time:
     unit: s
     min: 0.000
-    max: 63.529
+    max: 62.161
 thrust:
     unit: N
     min: 0.000
@@ -16,64 +16,64 @@ massEng:
     max: 1.223
 mass:
     unit: kg
-    min: 3.108
-    max: 3.618
+    min: 3.181
+    max: 3.691
 gravity:
     unit: m/s^2
-    min: 9.780
+    min: 9.781
     max: 9.795
 temperature:
     unit: K
-    min: 257.252
+    min: 258.589
     max: 288.150
 pressure:
     unit: Pa
-    min: 55861.797
+    min: 57403.797
     max: 101325.000
 density:
     unit: kg/m^3
-    min: 0.756
+    min: 0.773
     max: 1.225
 dynamicPressure:
     unit: Pa
     min: 0.000
-    max: 57030.645
+    max: 54567.008
 mach:
     unit: null
     min: 0.000
-    max: 0.897
+    max: 0.877
 alphaT:
     unit: rad
     min: 0.000
     max: 0.000
 dragCoeff:
     unit: null
-    min: 0.454
-    max: 0.524
+    min: 0.455
+    max: 0.522
 dragForce:
     unit: N
     min: 0.000
-    max: 242.123
+    max: 230.795
 liftForce:
     unit: N
     min: 0.000
     max: 0.000
 forceZ:
     unit: N
-    min: -30.446
-    max: 508.150
+    min: -31.154
+    max: 507.442
 linAccZ:
     unit: m/s^2
     min: -9.795
-    max: 152.365
+    max: 148.906
 linVelZ:
     unit: m/s
-    min: -305.161
-    max: 294.060
+    min: -298.482
+    max: 287.384
 linPosZ:
     unit: m
     min: 0.000
-    max: 4757.155
+    max: 4551.037
 isBurnout:
     unit: null
     min: 0.000

diff --git a/tools/unit_test/windows/run2/telem.npy b/tools/unit_test/windows/run2/telem.npy
diff --git a/tools/unit_test/windows/run3/input.yml b/tools/unit_test/windows/run3/input.yml
@@ -1,12 +1,12 @@
-# 2024-12-07 10:40:32
+# 2024-12-07 18:43:34
 # hpr-sim v0.0.0
 # Run: 3/5
 ---
 exec:
     mcMode:
         value: nominal
     seed:
-        value: 2
+        value: 4349422948805191298
     numMC:
         value: 1
     procMode:
@@ -29,7 +29,7 @@ engine:
         value: input/AeroTech_J450DM.eng
 mass:
     massBody:
-        value: 4.466468913532913
+        value: 4.516166478011944
         unit: lbm
         dist:
             name: normal

diff --git a/tools/unit_test/windows/run3/stats.yml b/tools/unit_test/windows/run3/stats.yml
@@ -1,11 +1,11 @@
-# 2024-12-07 10:40:32
+# 2024-12-07 18:43:34
 # hpr-sim v0.0.0
 # Run: 3/5
 ---
 time:
     unit: s
     min: 0.000
-    max: 71.563
+    max: 71.015
 thrust:
     unit: N
     min: 0.000
@@ -16,64 +16,64 @@ massEng:
     max: 1.223
 mass:
     unit: kg
-    min: 2.739
-    max: 3.249
+    min: 2.761
+    max: 3.271
 gravity:
     unit: m/s^2
-    min: 9.776
+    min: 9.777
     max: 9.795
 temperature:
     unit: K
-    min: 248.802
+    min: 249.410
     max: 288.150
 pressure:
     unit: Pa
-    min: 46878.434
+    min: 47482.652
     max: 101325.000
 density:
     unit: kg/m^3
-    min: 0.656
+    min: 0.663
     max: 1.225
 dynamicPressure:
     unit: Pa
     min: 0.000
-    max: 72631.234
+    max: 71507.781
 mach:
     unit: null
     min: 0.000
-    max: 1.012
+    max: 1.004
 alphaT:
     unit: rad
     min: 0.000
     max: 0.000
 dragCoeff:
     unit: null
     min: 0.455
-    max: 0.751
+    max: 0.732
 dragForce:
     unit: N
     min: 0.000
-    max: 441.944
+    max: 424.312
 liftForce:
     unit: N
     min: 0.000
     max: 0.000
 forceZ:
     unit: N
-    min: -26.828
-    max: 511.767
+    min: -27.049
+    max: 511.547
 linAccZ:
     unit: m/s^2
     min: -9.795
-    max: 172.699
+    max: 171.313
 linVelZ:
     unit: m/s
-    min: -344.368
-    max: 333.255
+    min: -341.698
+    max: 330.586
 linPosZ:
     unit: m
     min: 0.000
-    max: 6059.293
+    max: 5965.625
 isBurnout:
     unit: null
     min: 0.000

diff --git a/tools/unit_test/windows/run3/telem.npy b/tools/unit_test/windows/run3/telem.npy
diff --git a/tools/unit_test/windows/run4/input.yml b/tools/unit_test/windows/run4/input.yml
@@ -1,12 +1,12 @@
-# 2024-12-07 10:40:32
+# 2024-12-07 18:43:34
 # hpr-sim v0.0.0
 # Run: 4/5
 ---
 exec:
     mcMode:
         value: nominal
     seed:
-        value: 3
+        value: 843197638110165454
     numMC:
         value: 1
     procMode:
@@ -29,7 +29,7 @@ engine:
         value: input/AeroTech_J450DM.eng
 mass:
     massBody:
-        value: 5.3774548339920685
+        value: 5.030482508422596
         unit: lbm
         dist:
             name: normal