with the latest version of numpy this error appears

Conversion of an array with ndim > 0 to a scalar is deprecated, and will error in future. These fixes correct this issue and pytest runs again without lots of depreciation warnings.
AVSLab · Oct 8, 2023 · 6a76711 · 6a76711
1 parent 46e7266
commit 6a76711
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Showing 7 changed files with 14 additions and 13 deletions.
diff --git a/examples/scenarioAttLocPoint.py b/examples/scenarioAttLocPoint.py
@@ -296,7 +296,7 @@ def run(show_plots):
                                                   )
         vizSupport.addLocation(viz, stationName="Boulder Station"
                                , parentBodyName=earth.displayName
-                               , r_GP_P=groundStation.r_LP_P_Init
+                               , r_GP_P=unitTestSupport.EigenVector3d2list(groundStation.r_LP_P_Init)
                                , fieldOfView=np.radians(160.)
                                , color='pink'
                                , range=2000.0*1000  # meters

diff --git a/examples/scenarioGroundDownlink.py b/examples/scenarioGroundDownlink.py
@@ -70,6 +70,7 @@
 from Basilisk.simulation import simpleInstrument, simpleStorageUnit, partitionedStorageUnit, spaceToGroundTransmitter
 from Basilisk.simulation import groundLocation
 from Basilisk.utilities import vizSupport
+from Basilisk.utilities import unitTestSupport
 
 from Basilisk.simulation import spacecraft
 from Basilisk.utilities import macros
@@ -221,7 +222,7 @@ def run(show_plots):
                                                   )
         vizSupport.addLocation(viz, stationName="Boulder Station"
                                , parentBodyName=planet.planetName
-                               , r_GP_P=groundStation.r_LP_P_Init
+                               , r_GP_P=unitTestSupport.EigenVector3d2list(groundStation.r_LP_P_Init)
                                , fieldOfView=np.radians(160.)
                                , color='pink'
                                , range=1000.0*1000  # meters

diff --git a/examples/scenarioGroundLocationImaging.py b/examples/scenarioGroundLocationImaging.py
@@ -450,7 +450,7 @@ def run(show_plots):
             viz,
             stationName="Boulder Target",
             parentBodyName=earth.displayName,
-            r_GP_P=imagingTarget.r_LP_P_Init,
+            r_GP_P=unitTestSupport.EigenVector3d2list(imagingTarget.r_LP_P_Init),
             fieldOfView=np.radians(160.0),
             color="pink",
             range=2000.0 * 1000,  # meters
@@ -464,7 +464,7 @@ def run(show_plots):
             viz,
             stationName="Santiago Target",
             parentBodyName=earth.displayName,
-            r_GP_P=[[1761771.6422437236], [-5022201.882030934], [-3515898.6046771165]],
+            r_GP_P=[1761771.6422437236, -5022201.882030934, -3515898.6046771165],
             fieldOfView=np.radians(160.0),
             color="pink",
             range=2000.0 * 1000,  # meters
@@ -475,7 +475,7 @@ def run(show_plots):
             viz,
             stationName="Singapore Station",
             parentBodyName=earth.displayName,
-            r_GP_P=singaporeStation.r_LP_P_Init,
+            r_GP_P=unitTestSupport.EigenVector3d2list(singaporeStation.r_LP_P_Init),
             fieldOfView=np.radians(160.0),
             color="green",
             range=2000.0 * 1000,  # meters

diff --git a/src/fswAlgorithms/sensorInterfaces/TAMSensorData/_UnitTest/test_tamComm.py b/src/fswAlgorithms/sensorInterfaces/TAMSensorData/_UnitTest/test_tamComm.py
@@ -92,7 +92,7 @@ def tamCommTestFunction(show_plots):
 
     # Initialize the test module configuration data
     dcm3, _ = np.linalg.qr(np.random.normal(0, 1, (3, 3)))
-    module.dcm_BS = dcm3.reshape(9, 1)
+    module.dcm_BS = unitTestSupport.flattenList(dcm3.reshape(9, 1).tolist())
 
     # Create input message and size it because the regular creator of that message
     # is not part of the test.

diff --git a/src/simulation/environment/planetEphemeris/_UnitTest/test_planetEphemeris.py b/src/simulation/environment/planetEphemeris/_UnitTest/test_planetEphemeris.py
@@ -184,7 +184,7 @@ def planetEphemerisTest(show_plots, setRAN, setDEC, setLST, setRate):
             testMessages.append("FAILED: planetEphemeris() didn't set the desired plane name " + planet)
 
         # check that the time information is correct
-        timeTrue = [[0.0], [0.5], [1.0]]
+        timeTrue = [0.0, 0.5, 1.0]
         testFailCount, testMessages = unitTestSupport.compareDoubleArray(
             timeTrue, J2000Current, accuracy, "J2000Current", testFailCount, testMessages)
 
@@ -199,7 +199,7 @@ def planetEphemerisTest(show_plots, setRAN, setDEC, setLST, setRate):
         rTrue = []
         vTrue = []
         for time in timeTrue:
-            Mt = M0 + np.sqrt(mu/oe.a/oe.a/oe.a)*time[0]
+            Mt = M0 + np.sqrt(mu/oe.a/oe.a/oe.a)*time
             Et = orbitalMotion.M2E(Mt, oe.e)
             oe.f = orbitalMotion.E2f(Et, oe.e)
 
@@ -223,7 +223,7 @@ def planetEphemerisTest(show_plots, setRAN, setDEC, setLST, setRate):
             omega_NP_P = np.array([0.0, 0.0, -omegaList[c]])
             tilde = rbk.v3Tilde(omega_NP_P)
             for time in timeTrue:
-                lst = lst0 + omegaList[c]*time[0]
+                lst = lst0 + omegaList[c]*time
                 DCM = rbk.euler3232C([RAN, np.pi/2.0 - DEC, lst])
                 dcmTrue.append(DCM)
                 dDCMdt = np.matmul(tilde, DCM)

diff --git a/src/simulation/sensors/coarseSunSensor/_UnitTest/test_CSSConfig.py b/src/simulation/sensors/coarseSunSensor/_UnitTest/test_CSSConfig.py
@@ -129,7 +129,7 @@ def run(show_plots, accuracy):
     testFailCount, testMessages = unitTestSupport.compareArray([[0., 0., 0.]], dataCSS1pos,
                                                                accuracy, "CSS1 pos",
                                                                testFailCount, testMessages)
-    testFailCount, testMessages = unitTestSupport.compareArray([CSS1.nHat_B], dataCSS1nHat,
+    testFailCount, testMessages = unitTestSupport.compareArray([unitTestSupport.EigenVector3d2np(CSS1.nHat_B)], dataCSS1nHat,
                                                                accuracy, "CSS1 nHat_B",
                                                                testFailCount, testMessages)
     testFailCount, testMessages = unitTestSupport.compareDoubleArray([CSS1.fov], dataCSS1fov,
@@ -149,10 +149,10 @@ def run(show_plots, accuracy):
                                                                      testFailCount, testMessages)
 
     # check CSS 2 output
-    testFailCount, testMessages = unitTestSupport.compareArray([CSS2.r_B], dataCSS2pos,
+    testFailCount, testMessages = unitTestSupport.compareArray([unitTestSupport.EigenVector3d2np(CSS2.r_B)], dataCSS2pos,
                                                                accuracy, "CSS2 pos",
                                                                testFailCount, testMessages)
-    testFailCount, testMessages = unitTestSupport.compareArray([CSS2.nHat_B], dataCSS2nHat,
+    testFailCount, testMessages = unitTestSupport.compareArray([unitTestSupport.EigenVector3d2np(CSS2.nHat_B)], dataCSS2nHat,
                                                                accuracy, "CSS2 nHat_B",
                                                                testFailCount, testMessages)
     testFailCount, testMessages = unitTestSupport.compareDoubleArray([CSS2.fov], dataCSS2fov,

diff --git a/src/simulation/sensors/simpleMassProps/_UnitTest/test_simpleMassProps.py b/src/simulation/sensors/simpleMassProps/_UnitTest/test_simpleMassProps.py
@@ -139,7 +139,7 @@ def simpleMassPropsTestFunction(show_plots, accuracy):
     unitTestSim.TotalSim.SingleStepProcesses()
 
     # set the filtered output truth states
-    trueMass = [[100], [500]]
+    trueMass = [100, 500]
     trueInertia = [[40, 0, 0, 0, 50, 0, 0, 0, 60],
                    [200, 0, 0, 0, 300, 0, 0, 0, 400]]
     trueCoM = [[0.0, 0.0, 0.0],