ENH: Create a rocketpy file to store flight simulations

CHANGELOG.md

@@ -32,6 +32,7 @@ Attention: The newest changes should be on top -->
 
 ### Added
 
+- ENH: Create a rocketpy file to store flight simulations [#800](https://github.com/RocketPy-Team/RocketPy/pull/800)
 - ENH: Support for the RSE file format has been added to the library [#798](https://github.com/RocketPy-Team/RocketPy/pull/798)
 
 ### Changed

pyproject.toml

@@ -101,6 +101,7 @@ skip-magic-trailing-comma = false
 line-ending = "auto"
 docstring-code-format = false
 docstring-code-line-length = "dynamic"
+exclude = ["**/*.json", "**/*.rpy"]
 
 
 [tool.ruff.lint.pydocstyle]

rocketpy/_encoders.py

@@ -7,6 +7,8 @@
 import numpy as np
 
 from rocketpy.mathutils.function import Function
+from rocketpy.prints.flight_prints import _FlightPrints
+from rocketpy.plots.flight_plots import _FlightPlots
 
 
 class RocketPyEncoder(json.JSONEncoder):
@@ -75,6 +77,7 @@ class RocketPyDecoder(json.JSONDecoder):
     different types of objects from a JSON supported format."""
 
     def __init__(self, *args, **kwargs):
+        self.resimulate = kwargs.pop("resimulate", False)
         super().__init__(object_hook=self.object_hook, *args, **kwargs)
 
     def object_hook(self, obj):
@@ -84,7 +87,56 @@ def object_hook(self, obj):
             try:
                 class_ = get_class_from_signature(signature)
 
-                if hasattr(class_, "from_dict"):
+                if class_.__name__ == "Flight" and not self.resimulate:
+                    new_flight = class_.__new__(class_)
+                    new_flight.prints = _FlightPrints(new_flight)
+                    new_flight.plots = _FlightPlots(new_flight)
+                    attributes = (
+                        "rocket",
+                        "env",
+                        "rail_length",
+                        "inclination",
+                        "heading",
+                        "initial_solution",
+                        "terminate_on_apogee",
+                        "max_time",
+                        "max_time_step",
+                        "min_time_step",
+                        "rtol",
+                        "atol",
+                        "time_overshoot",
+                        "name",
+                        "solution",
+                        "out_of_rail_time",
+                        "apogee_time",
+                        "apogee",
+                        "parachute_events",
+                        "impact_state",
+                        "impact_velocity",
+                        "x_impact",
+                        "y_impact",
+                        "t_final",
+                        "flight_phases",
+                        "ax",
+                        "ay",
+                        "az",
+                        "out_of_rail_time_index",
+                        "function_evaluations",
+                        "alpha1",
+                        "alpha2",
+                        "alpha3",
+                        "R1",
+                        "R2",
+                        "R3",
+                        "M1",
+                        "M2",
+                        "M3",
+                    )
+                    for attribute in attributes:
+                        setattr(new_flight, attribute, obj[attribute])
+                    new_flight.t_initial = new_flight.initial_solution[0]
+                    return new_flight
+                elif hasattr(class_, "from_dict"):
                     return class_.from_dict(obj)
                 else:
                     # Filter keyword arguments

rocketpy/simulation/flight.py

@@ -3434,24 +3434,43 @@ def to_dict(self, include_outputs=False):
             "time_overshoot": self.time_overshoot,
             "name": self.name,
             "equations_of_motion": self.equations_of_motion,
+            # The following outputs are essential to run all_info method
+            "solution": self.solution,
+            "out_of_rail_time": self.out_of_rail_time,
+            "out_of_rail_time_index": self.out_of_rail_time_index,
+            "apogee_time": self.apogee_time,
+            "apogee": self.apogee,
+            "parachute_events": self.parachute_events,
+            "impact_state": self.impact_state,
+            "impact_velocity": self.impact_velocity,
+            "x_impact": self.x_impact,
+            "y_impact": self.y_impact,
+            "t_final": self.t_final,
+            "flight_phases": self.flight_phases,
+            "function_evaluations": self.function_evaluations,
+            "ax": self.ax,
+            "ay": self.ay,
+            "az": self.az,
+            "alpha1": self.alpha1,
+            "alpha2": self.alpha2,
+            "alpha3": self.alpha3,
+            "R1": self.R1,
+            "R2": self.R2,
+            "R3": self.R3,
+            "M1": self.M1,
+            "M2": self.M2,
+            "M3": self.M3,
         }
 
         if include_outputs:
             data.update(
                 {
                     "time": self.time,
-                    "out_of_rail_time": self.out_of_rail_time,
                     "out_of_rail_velocity": self.out_of_rail_velocity,
                     "out_of_rail_state": self.out_of_rail_state,
-                    "apogee": self.apogee,
-                    "apogee_time": self.apogee_time,
                     "apogee_x": self.apogee_x,
                     "apogee_y": self.apogee_y,
                     "apogee_state": self.apogee_state,
-                    "x_impact": self.x_impact,
-                    "y_impact": self.y_impact,
-                    "impact_velocity": self.impact_velocity,
-                    "impact_state": self.impact_state,
                     "x": self.x,
                     "y": self.y,
                     "z": self.z,
@@ -3465,12 +3484,6 @@ def to_dict(self, include_outputs=False):
                     "w1": self.w1,
                     "w2": self.w2,
                     "w3": self.w3,
-                    "ax": self.ax,
-                    "ay": self.ay,
-                    "az": self.az,
-                    "alpha1": self.alpha1,
-                    "alpha2": self.alpha2,
-                    "alpha3": self.alpha3,
                     "altitude": self.altitude,
                     "mach_number": self.mach_number,
                     "stream_velocity_x": self.stream_velocity_x,

rocketpy/utilities.py

@@ -2,7 +2,12 @@
 import inspect
 import traceback
 import warnings
+import json
+import os
 
+from pathlib import Path
+from importlib.metadata import version
+from datetime import date
 import matplotlib.pyplot as plt
 import numpy as np
 from scipy.integrate import solve_ivp
@@ -12,6 +17,7 @@
 from .plots.plot_helpers import show_or_save_plot
 from .rocket.aero_surface import TrapezoidalFins
 from .simulation.flight import Flight
+from ._encoders import RocketPyEncoder, RocketPyDecoder
 
 
 def compute_cd_s_from_drop_test(
@@ -688,3 +694,68 @@ def get_instance_attributes(instance):
         if not inspect.ismethod(member[1]) and not member[0].startswith("__"):
             attributes_dict[member[0]] = member[1]
     return attributes_dict
+
+
+def save_to_rpy(flight: Flight, filename: str, include_outputs=False):
+    """Saves a .rpy file into the given path, containing key simulation
+    informations to reproduce the results.
+
+    Parameters
+    ----------
+    flight : rocketpy.Flight
+        Flight object containing the rocket's flight data
+    filename : str
+        Path where the file will be saved in
+    include_outputs : bool, optional
+        If True, the function will include extra outputs into the file,
+        by default False
+
+    Returns
+    -------
+    None
+    """
+    file = Path(filename).with_suffix(".rpy")
+
+    with open(file, "w") as f:
+        data = {"date": str(date.today()), "version": version("rocketpy")}
+        data["simulation"] = flight
+        json.dump(
+            data,
+            f,
+            cls=RocketPyEncoder,
+            indent=2,
+            include_outputs=include_outputs,
+        )
+
+
+def load_from_rpy(filename: str, resimulate=False):
+    """Loads the saved data from a .rpy file into a Flight object.
+
+    Parameters
+    ----------
+    filename : str
+        Path where the file to be loaded is
+    resimulate : bool, optional
+        If True, the function will resimulate the Flight object,
+        by default False
+
+    Returns
+    -------
+    rocketpy.Flight
+        Flight object containing simulation information from the .rpy file
+    """
+    ext = os.path.splitext(os.path.basename(filename))[1]
+    if ext != ".rpy":  # pragma: no cover
+        raise ValueError(f"Invalid file extension: {ext}. Allowed: .rpy")
+
+    with open(filename, "r") as f:
+        data = json.load(f)
+        if data["version"] > version("rocketpy"):
+            warnings.warn(
+                "The file was saved in an updated version of",
+                f"RocketPy (v{data['version']}), the current",
+                f"imported module is v{version('rocketpy')}",
+            )
+        simulation = json.dumps(data["simulation"])
+        flight = json.loads(simulation, cls=RocketPyDecoder, resimulate=resimulate)
+    return flight