ENH: add burn_start_time and burn_out_time to mcsolidmotor

Author: MateusStano

docs/notebooks/dispersion_analysis/dispersion_class_usage.ipynb

@@ -19,18 +19,9 @@
   },
   {
    "cell_type": "code",
-   "execution_count": 3,
+   "execution_count": 1,
    "metadata": {},
-   "outputs": [
-    {
-     "name": "stdout",
-     "output_type": "stream",
-     "text": [
-      "The autoreload extension is already loaded. To reload it, use:\n",
-      "  %reload_ext autoreload\n"
-     ]
-    }
-   ],
+   "outputs": [],
    "source": [
     "%load_ext autoreload\n",
     "%autoreload 2"
@@ -46,7 +37,7 @@
   },
   {
    "cell_type": "code",
-   "execution_count": 4,
+   "execution_count": 2,
    "metadata": {},
    "outputs": [],
    "source": [
@@ -75,7 +66,7 @@
   },
   {
    "cell_type": "code",
-   "execution_count": 5,
+   "execution_count": 3,
    "metadata": {},
    "outputs": [],
    "source": [
@@ -116,7 +107,7 @@
   },
   {
    "cell_type": "code",
-   "execution_count": 6,
+   "execution_count": 4,
    "metadata": {},
    "outputs": [],
    "source": [
@@ -133,24 +124,25 @@
   },
   {
    "cell_type": "code",
-   "execution_count": 7,
+   "execution_count": 5,
    "metadata": {},
    "outputs": [
     {
      "data": {
       "text/plain": [
-       "object: <rocketpy.environment.environment.Environment object at 0x00000242D3055D30>\n",
+       "object: <rocketpy.environment.environment.Environment object at 0x0000021119D58200>\n",
        "elevation: [113]\n",
        "gravity: ['Function from R1 to R1 : (height (m)) → (gravity (m/s²))']\n",
        "latitude: [39.3897]\n",
        "longitude: [-8.288964]\n",
        "wind_velocity_x_factor: 1.00000 ± 0.33000 (numpy.random.normal)\n",
        "wind_velocity_y_factor: 1.00000 ± 0.33000 (numpy.random.normal)\n",
-       "date: [(2023, 12, 10, 12)]\n",
+       "datum: ['SIRGAS2000']\n",
+       "timezone: ['UTC']\n",
        "ensemble_member: [0, 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17, 18, 19, 20, 21, 22, 23, 24, 25, 26, 27, 28, 29, 30]"
       ]
      },
-     "execution_count": 7,
+     "execution_count": 5,
      "metadata": {},
      "output_type": "execute_result"
     }
@@ -168,14 +160,14 @@
   },
   {
    "cell_type": "code",
-   "execution_count": 8,
+   "execution_count": 6,
    "metadata": {},
    "outputs": [
     {
      "name": "stdout",
      "output_type": "stream",
      "text": [
-      "[5.4868565741227835, 3.4970766908409914, 5.3253588908900245, 4.059176104591607, 4.215612011141973, 4.502052604362678, 4.74317323047254, 4.543846316731022, 4.215612011141973, 4.46569593156061]\n"
+      "[6.945158633629927, 8.580629399795324, 6.090321529581044, 8.29507654713753, 8.164411035755625, 9.57486298213925, 7.747329947135309, 6.878299591656838, 7.149819236691613, 8.750910295481544]\n"
      ]
     }
    ],
@@ -207,7 +199,7 @@
   },
   {
    "cell_type": "code",
-   "execution_count": 9,
+   "execution_count": 7,
    "metadata": {},
    "outputs": [
     {
@@ -216,7 +208,7 @@
        "6026.35"
       ]
      },
-     "execution_count": 9,
+     "execution_count": 7,
      "metadata": {},
      "output_type": "execute_result"
     }
@@ -251,10 +243,11 @@
     {
      "data": {
       "text/plain": [
-       "object: <rocketpy.motors.solid_motor.SolidMotor object at 0x00000242D3DA2330>\n",
+       "object: <rocketpy.motors.solid_motor.SolidMotor object at 0x00000211196A1970>\n",
        "thrust_source: [[[0, 0], [0.055, 100.0], [0.092, 1500.0], [0.1, 2000.0], [0.15, 2200.0], [0.2, 1800.0], [0.5, 1950.0], [1.0, 2034.0], [1.5, 2000.0], [2.0, 1900.0], [2.5, 1760.0], [2.9, 1700.0], [3.0, 1650.0], [3.3, 530.0], [3.4, 350.0], [3.9, 0.0]]]\n",
        "total_impulse: 6500.00000 ± 1000.00000 (numpy.random.normal)\n",
-       "burn_time: 5.27400 ± 1.00000 (numpy.random.normal)\n",
+       "burn_start_time: [0]\n",
+       "burn_out_time: [3.9]\n",
        "dry_mass: [1.815]\n",
        "dry_I_11: [0.125]\n",
        "dry_I_22: [0.125]\n",
@@ -283,7 +276,8 @@
    "source": [
     "mc_motor = McSolidMotor(\n",
     "    solid_motor=motor,\n",
-    "    burn_time=(5.274, 1),\n",
+    "    burn_start_time=(0, 0.5),\n",
+    "    burn_out_time=(5.274, 1),\n",
     "    grains_center_of_mass_position=0.001,\n",
     "    grain_density=50,\n",
     "    grain_separation=1 / 1000,\n",

rocketpy/monte_carlo/mc_solid_motor.py

@@ -19,7 +19,8 @@ def __init__(
         solid_motor,
         thrust_source=None,
         total_impulse=None,
-        burn_time=None,
+        burn_start_time=None,
+        burn_out_time=None,
         dry_mass=None,
         dry_inertia_11=None,
         dry_inertia_22=None,
@@ -113,12 +114,12 @@ def __init__(
             Radius of the throat in the motor in meters. Follows the standard
             input format of Dispersion Models.
         """
-
         super().__init__(
             solid_motor,
             thrust_source=thrust_source,
             total_impulse=total_impulse,
-            burn_time=burn_time,
+            burn_start_time=burn_start_time,
+            burn_out_time=burn_out_time,
             dry_mass=dry_mass,
             dry_I_11=dry_inertia_11,
             dry_I_22=dry_inertia_22,