implements flight route tests; bring common fixturest o toplevel conf…

…test

README.md

@@ -99,12 +99,6 @@ $ touch .env && echo MONGODB_CONNECTION_STRING="$ConnectionString" > .env
         │   ├── test_motor_service.py
         │   └── test_rocket_serice.py
         │
-        ├── test_routes
-        │   ├── test_environment_route.py
-        │   ├── test_flight_route.py
-        │   ├── test_motor_route.py
-        │   └── test_rocket_route.py
-        │
         ├── test_repositories
         │   ├── test_environment_repo.py
         │   ├── test_flight_repo.py

lib/models/rocket.py

@@ -17,6 +17,12 @@ class CoordinateSystemOrientation(str, Enum):
 
 
 class Rocket(BaseModel):
+
+    def __eq__(self, other):
+        if not isinstance(other, Rocket):
+            return False
+        return self.dict() == other.dict()
+
     # Required parameters
     motor: Motor
     radius: float

pyproject.toml

@@ -43,7 +43,6 @@ disable = """
     broad-exception-caught,
     raise-missing-from,
     too-many-instance-attributes,
-    redefined-outer-name,
     import-error,
     too-many-arguments,
     redefined-outer-name,

tests/test_routes/conftest.py

@@ -0,0 +1,95 @@
+import json
+import pytest
+
+from lib.models.rocket import Rocket
+from lib.models.motor import Motor, MotorTank, TankFluids, TankKinds
+from lib.models.environment import Env
+
+
+@pytest.fixture
+def stub_env():
+    env = Env(latitude=0, longitude=0)
+    env_json = env.model_dump_json()
+    return json.loads(env_json)
+
+
+@pytest.fixture
+def stub_motor():
+    motor = Motor(
+        thrust_source=[[0, 0]],
+        burn_time=0,
+        nozzle_radius=0,
+        dry_mass=0,
+        dry_inertia=[0, 0, 0],
+        center_of_dry_mass_position=0,
+    )
+    motor_json = motor.model_dump_json()
+    return json.loads(motor_json)
+
+
+@pytest.fixture
+def stub_tank():
+    tank = MotorTank(
+        geometry=[[(0, 0), 0]],
+        gas=TankFluids(name='gas', density=0),
+        liquid=TankFluids(name='liquid', density=0),
+        flux_time=(0, 0),
+        position=0,
+        discretize=0,
+        name='tank',
+    )
+    tank_json = tank.model_dump_json()
+    return json.loads(tank_json)
+
+
+@pytest.fixture
+def stub_level_tank(stub_tank):
+    stub_tank.update({'tank_kind': TankKinds.LEVEL, 'liquid_height': 0})
+    return stub_tank
+
+
+@pytest.fixture
+def stub_mass_flow_tank(stub_tank):
+    stub_tank.update(
+        {
+            'tank_kind': TankKinds.MASS_FLOW,
+            'gas_mass_flow_rate_in': 0,
+            'gas_mass_flow_rate_out': 0,
+            'liquid_mass_flow_rate_in': 0,
+            'liquid_mass_flow_rate_out': 0,
+            'initial_liquid_mass': 0,
+            'initial_gas_mass': 0,
+        }
+    )
+    return stub_tank
+
+
+@pytest.fixture
+def stub_ullage_tank(stub_tank):
+    stub_tank.update({'tank_kind': TankKinds.ULLAGE, 'ullage': 0})
+    return stub_tank
+
+
+@pytest.fixture
+def stub_mass_tank(stub_tank):
+    stub_tank.update(
+        {'tank_kind': TankKinds.MASS, 'liquid_mass': 0, 'gas_mass': 0}
+    )
+    return stub_tank
+
+
+@pytest.fixture
+def stub_rocket(stub_motor):
+    rocket = Rocket(
+        motor=stub_motor,
+        radius=0,
+        mass=0,
+        motor_position=0,
+        center_of_mass_without_motor=0,
+        inertia=[0, 0, 0],
+        power_off_drag=[(0, 0)],
+        power_on_drag=[(0, 0)],
+        coordinate_system_orientation='TAIL_TO_NOSE',
+    )
+    rocket_json = rocket.model_dump_json()
+    return json.loads(rocket_json)

tests/test_routes/test_environments_route.py

@@ -16,13 +16,6 @@
 client = TestClient(app)
 
 
-@pytest.fixture
-def stub_env():
-    env = Env(latitude=0, longitude=0)
-    env_json = env.model_dump_json()
-    return json.loads(env_json)
-
-
 @pytest.fixture
 def stub_env_summary():
     env_summary = EnvSummary()