ENH: Allow for Alternative and Custom ODE Solvers.

.vscode/settings.json

@@ -245,6 +245,7 @@
         "pytest",
         "pytz",
         "quantile",
+        "Radau",
         "Rdot",
         "referece",
         "relativetoground",

CHANGELOG.md

@@ -32,7 +32,7 @@ Attention: The newest changes should be on top -->
 
 ### Added
 
--
+- ENH: Allow for Alternative and Custom ODE Solvers. [#748](https://github.com/RocketPy-Team/RocketPy/pull/748)
 
 ### Changed
 

rocketpy/simulation/flight.py

@@ -7,7 +7,7 @@
 
 import numpy as np
 import simplekml
-from scipy import integrate
+from scipy.integrate import BDF, DOP853, LSODA, RK23, RK45, OdeSolver, Radau
 
 from ..mathutils.function import Function, funcify_method
 from ..mathutils.vector_matrix import Matrix, Vector
@@ -24,8 +24,19 @@
     quaternions_to_spin,
 )
 
+ODE_SOLVER_MAP = {
+    'RK23': RK23,
+    'RK45': RK45,
+    'DOP853': DOP853,
+    'Radau': Radau,
+    'BDF': BDF,
+    'LSODA': LSODA,
+}
 
-class Flight:  # pylint: disable=too-many-public-methods
+
+# pylint: disable=too-many-public-methods
+# pylint: disable=too-many-instance-attributes
+class Flight:
     """Keeps all flight information and has a method to simulate flight.
 
     Attributes
@@ -506,6 +517,7 @@ def __init__(  # pylint: disable=too-many-arguments,too-many-statements
         verbose=False,
         name="Flight",
         equations_of_motion="standard",
+        ode_solver="LSODA",
     ):
         """Run a trajectory simulation.
 
@@ -581,10 +593,23 @@ def __init__(  # pylint: disable=too-many-arguments,too-many-statements
             more restricted set of equations of motion that only works for
             solid propulsion rockets. Such equations were used in RocketPy v0
             and are kept here for backwards compatibility.
+        ode_solver : str, ``scipy.integrate.OdeSolver``, optional
+            Integration method to use to solve the equations of motion ODE.
+            Available options are: 'RK23', 'RK45', 'DOP853', 'Radau', 'BDF',
+            'LSODA' from ``scipy.integrate.solve_ivp``.
+            Default is 'LSODA', which is recommended for most flights.
+            A custom ``scipy.integrate.OdeSolver`` can be passed as well.
+            For more information on the integration methods, see the scipy
+            documentation [1]_.
+
 
         Returns
         -------
         None
+
+        References
+        ----------
+        .. [1] https://docs.scipy.org/doc/scipy/reference/generated/scipy.integrate.solve_ivp.html
         """
         # Save arguments
         self.env = environment
@@ -605,6 +630,7 @@ def __init__(  # pylint: disable=too-many-arguments,too-many-statements
         self.terminate_on_apogee = terminate_on_apogee
         self.name = name
         self.equations_of_motion = equations_of_motion
+        self.ode_solver = ode_solver
 
         # Controller initialization
         self.__init_controllers()
@@ -651,15 +677,16 @@ def __simulate(self, verbose):
 
             # Create solver for this flight phase # TODO: allow different integrators
             self.function_evaluations.append(0)
-            phase.solver = integrate.LSODA(
+
+            phase.solver = self._solver(
                 phase.derivative,
                 t0=phase.t,
                 y0=self.y_sol,
                 t_bound=phase.time_bound,
-                min_step=self.min_time_step,
-                max_step=self.max_time_step,
                 rtol=self.rtol,
                 atol=self.atol,
+                max_step=self.max_time_step,
+                min_step=self.min_time_step,
             )
 
             # Initialize phase time nodes
@@ -691,13 +718,14 @@ def __simulate(self, verbose):
             for node_index, node in self.time_iterator(phase.time_nodes):
                 # Determine time bound for this time node
                 node.time_bound = phase.time_nodes[node_index + 1].t
-                # NOTE: Setting the time bound and status for the phase solver,
-                # and updating its internal state for the next integration step.
                 phase.solver.t_bound = node.time_bound
-                phase.solver._lsoda_solver._integrator.rwork[0] = phase.solver.t_bound
-                phase.solver._lsoda_solver._integrator.call_args[4] = (
-                    phase.solver._lsoda_solver._integrator.rwork
-                )
+                if self.__is_lsoda:
+                    phase.solver._lsoda_solver._integrator.rwork[0] = (
+                        phase.solver.t_bound
+                    )
+                    phase.solver._lsoda_solver._integrator.call_args[4] = (
+                        phase.solver._lsoda_solver._integrator.rwork
+                    )
                 phase.solver.status = "running"
 
                 # Feed required parachute and discrete controller triggers
@@ -1185,6 +1213,8 @@ def __init_solver_monitors(self):
         self.t = self.solution[-1][0]
         self.y_sol = self.solution[-1][1:]
 
+        self.__set_ode_solver(self.ode_solver)
+
     def __init_equations_of_motion(self):
         """Initialize equations of motion."""
         if self.equations_of_motion == "solid_propulsion":
@@ -1222,6 +1252,28 @@ def __cache_sensor_data(self):
                 sensor_data[sensor] = sensor.measured_data[:]
         self.sensor_data = sensor_data
 
+    def __set_ode_solver(self, solver):
+        """Sets the ODE solver to be used in the simulation.
+
+        Parameters
+        ----------
+        solver : str, ``scipy.integrate.OdeSolver``
+            Integration method to use to solve the equations of motion ODE,
+            or a custom ``scipy.integrate.OdeSolver``.
+        """
+        if isinstance(solver, OdeSolver):
+            self._solver = solver
+        else:
+            try:
+                self._solver = ODE_SOLVER_MAP[solver]
+            except KeyError as e:
+                raise ValueError(
+                    f"Invalid ``ode_solver`` input: {solver}. "
+                    f"Available options are: {', '.join(ODE_SOLVER_MAP.keys())}"
+                ) from e
+
+        self.__is_lsoda = hasattr(self._solver, "_lsoda_solver")
+
     @cached_property
     def effective_1rl(self):
         """Original rail length minus the distance measured from nozzle exit

tests/integration/test_flight.py

@@ -11,7 +11,8 @@
 
 
 @patch("matplotlib.pyplot.show")
-def test_all_info(mock_show, flight_calisto_robust):  # pylint: disable=unused-argument
+# pylint: disable=unused-argument
+def test_all_info(mock_show, flight_calisto_robust):
     """Test that the flight class is working as intended. This basically calls
     the all_info() method and checks if it returns None. It is not testing if
     the values are correct, but whether the method is working without errors.
@@ -27,6 +28,42 @@ def test_all_info(mock_show, flight_calisto_robust):  # pylint: disable=unused-a
     assert flight_calisto_robust.all_info() is None
 
 
+@pytest.mark.slow
+@patch("matplotlib.pyplot.show")
+@pytest.mark.parametrize("solver_method", ["RK45", "DOP853", "Radau", "BDF"])
+# RK23 is unstable and requires a very low tolerance to work
+# pylint: disable=unused-argument
+def test_all_info_different_solvers(
+    mock_show, calisto_robust, example_spaceport_env, solver_method
+):
+    """Test that the flight class is working as intended with different solver
+    methods. This basically calls the all_info() method and checks if it returns
+    None. It is not testing if the values are correct, but whether the method is
+    working without errors.
+
+    Parameters
+    ----------
+    mock_show : unittest.mock.MagicMock
+        Mock object to replace matplotlib.pyplot.show
+    calisto_robust : rocketpy.Rocket
+        Rocket to be simulated. See the conftest.py file for more info.
+    example_spaceport_env : rocketpy.Environment
+        Environment to be simulated. See the conftest.py file for more info.
+    solver_method : str
+        The solver method to be used in the simulation.
+    """
+    test_flight = Flight(
+        environment=example_spaceport_env,
+        rocket=calisto_robust,
+        rail_length=5.2,
+        inclination=85,
+        heading=0,
+        terminate_on_apogee=False,
+        ode_solver=solver_method,
+    )
+    assert test_flight.all_info() is None
+
+
 class TestExportData:
     """Tests the export_data method of the Flight class."""