feat: fix tests

bindings/python/test/access/test_visibility_criterion.py

@@ -136,11 +136,15 @@ def test_aer_interval_is_satisfied(
         aer_interval = VisibilityCriterion.AERInterval(
             azimuth_interval, elevation_interval, range_interval
         )
-        aer = AER(azimuth=np.pi / 4, elevation=np.pi / 8, range=5e6)
-        assert aer_interval.is_satisfied(aer) is True
+        assert (
+            aer_interval.is_satisfied(azimuth=np.pi / 4, elevation=np.pi / 8, range=5e6)
+            is True
+        )
 
-        aer_invalid = AER(azimuth=np.pi, elevation=np.pi / 2, range=1e8)
-        assert aer_interval.is_satisfied(aer_invalid) is False
+        assert (
+            aer_interval.is_satisfied(azimuth=np.pi, elevation=np.pi / 2, range=1e8)
+            is False
+        )
 
     def test_elevation_interval_is_satisfied(
         self,
@@ -159,8 +163,10 @@ def test_line_of_sight_is_satisfied(
     ):
         line_of_sight = VisibilityCriterion.LineOfSight(environment)
         instant = Instant.now()
-        from_position = np.array([7000e3, 0.0, 0.0])  # 7000 km altitude
-        to_position = np.array([0.0, 7000e3, 0.0])  # 7000 km altitude
+
+        from_position = np.array([7000e3, 0.0, 0.0])
+        to_position = np.array([7005e3, 0.0, 0.0])
+
         assert line_of_sight.is_satisfied(instant, from_position, to_position) is True
 
     def test_visibility_criterion_type_checks(

bindings/python/test/solvers/test_temporal_condition_solver.py

@@ -16,6 +16,8 @@
 from ostk.astrodynamics.trajectory.orbit.model.kepler import COE
 from ostk.astrodynamics.access import Generator
 from ostk.astrodynamics.solver import TemporalConditionSolver
+from ostk.astrodynamics.access import AccessTarget
+from ostk.astrodynamics.access import VisibilityCriterion
 
 
 @pytest.fixture
@@ -141,9 +143,15 @@ def test_solve_success_using_access_generator(
             celestial_object=earth,
         )
 
+        visibility_criterion: VisibilityCriterion = (
+            VisibilityCriterion.from_line_of_sight(environment)
+        )
+
+        access_target = AccessTarget.from_trajectory(visibility_criterion, trajectory)
+
         solution: list[Interval] = temporal_condition_solver.solve(
             condition=generator.get_condition_function(
-                from_trajectory=trajectory,
+                access_target=access_target,
                 to_trajectory=trajectory,
             ),
             interval=interval,

bindings/python/test/test_display.py

@@ -15,12 +15,13 @@
 from ostk.physics.unit import Length
 from ostk.physics.unit import Angle
 
-from ostk.astrodynamics import Trajectory
 from ostk.astrodynamics import display
 from ostk.astrodynamics.access import Generator as AccessGenerator
 from ostk.astrodynamics.trajectory import Orbit
 from ostk.astrodynamics.trajectory.orbit.model import SGP4
 from ostk.astrodynamics.trajectory.orbit.model.sgp4 import TLE
+from ostk.astrodynamics.access import AccessTarget
+from ostk.astrodynamics.access import VisibilityCriterion
 
 
 class TestDisplay:
@@ -52,7 +53,12 @@ def test_accesses_plot(self):
         environment: Environment = Environment.default()
         earth: Celestial = environment.access_celestial_object_with_name("Earth")
 
-        ground_station_trajectory: Trajectory = Trajectory.position(
+        visibility_criterion: VisibilityCriterion = (
+            VisibilityCriterion.from_line_of_sight(environment)
+        )
+
+        access_target: AccessTarget = AccessTarget.from_position(
+            visibility_criterion,
             Position.meters(
                 ground_station_lla.to_cartesian(
                     earth.get_equatorial_radius(),
@@ -76,15 +82,15 @@ def test_accesses_plot(self):
 
         accesses_1 = generator.compute_accesses(
             interval=search_interval,
-            from_trajectory=ground_station_trajectory,
+            access_target=access_target,
             to_trajectory=orbit_1,
         )
 
         assert len(accesses_1) > 0
 
         accesses_2 = generator.compute_accesses(
             interval=search_interval,
-            from_trajectory=ground_station_trajectory,
+            access_target=access_target,
             to_trajectory=orbit_2,
         )