verbose output for cruise trim

Author: MrMinos

scripts/simple-body.ipynb

@@ -9,7 +9,7 @@
   },
   {
    "cell_type": "code",
-   "execution_count": 1,
+   "execution_count": 9,
    "source": [
     "import numpy as np\n",
     "import pandas as pd\n",
@@ -24,7 +24,7 @@
   },
   {
    "cell_type": "code",
-   "execution_count": 2,
+   "execution_count": 10,
    "source": [
     "aircraft_model = 'WaveRipper'"
    ],
@@ -40,7 +40,7 @@
   },
   {
    "cell_type": "code",
-   "execution_count": 3,
+   "execution_count": 11,
    "source": [
     "op_ground, props = trim(\n",
     "    aircraft=aircraft_model,\n",
@@ -65,13 +65,6 @@
      "output_type": "stream",
      "name": "stdout",
      "text": [
-      "\n",
-      "\n",
-      "     JSBSim Flight Dynamics Model v1.1.8 [GitHub build 588/commit c943f83deeb3e14bed7939ac65dfac789a7a0181] Jul 30 2021 15:04:27\n",
-      "            [JSBSim-ML v2.0]\n",
-      "\n",
-      "JSBSim startup beginning ...\n",
-      "\n",
       " final_simplex: (array([[-0.00398416, -0.0198497 ],\n",
       "       [-0.00397723, -0.01982051],\n",
       "       [-0.00397813, -0.01978912]]), array([0.0010305 , 0.00103479, 0.00109463]))\n",
@@ -106,14 +99,14 @@
       ]
      },
      "metadata": {},
-     "execution_count": 3
+     "execution_count": 11
     }
    ],
    "metadata": {}
   },
   {
    "cell_type": "code",
-   "execution_count": 4,
+   "execution_count": 12,
    "source": [
     "op_ground"
    ],
@@ -132,14 +125,14 @@
       ]
      },
      "metadata": {},
-     "execution_count": 4
+     "execution_count": 12
     }
    ],
    "metadata": {}
   },
   {
    "cell_type": "code",
-   "execution_count": 5,
+   "execution_count": 13,
    "source": [
     "log_ground = simulate(\n",
     "    aircraft=aircraft_model,\n",
@@ -168,7 +161,7 @@
   },
   {
    "cell_type": "code",
-   "execution_count": 6,
+   "execution_count": 17,
    "source": [
     "op_cruise, props = trim(\n",
     "    aircraft=aircraft_model,\n",
@@ -200,13 +193,41 @@
     "    # ],\n",
     "    cost=lambda fdm: fdm['fcs/throttle-cmd-norm'],\n",
     "    x0=[0.5, 0, 0, 0, 0, 0],\n",
-    "    verbose=False,\n",
+    "    verbose=True,\n",
     "    bounds=[[0, 1], [-1, 1], [-1, 1], [-1, 1], [-1, 1], [-1, 1]],\n",
     "    tol=1e-3\n",
     ")\n",
     "op_cruise"
    ],
    "outputs": [
+    {
+     "output_type": "stream",
+     "name": "stdout",
+     "text": [
+      " final_simplex: (array([[0.00000000e+00, 7.79320988e-05, 8.55709877e-04, 1.37422840e-03,\n",
+      "        3.80401235e-04, 5.36779835e-04],\n",
+      "       [0.00000000e+00, 9.51271005e-05, 8.67503644e-04, 1.34718471e-03,\n",
+      "        3.53561171e-04, 5.54578547e-04],\n",
+      "       [0.00000000e+00, 1.10616355e-04, 8.64988783e-04, 1.37300490e-03,\n",
+      "        3.56847637e-04, 5.53797416e-04],\n",
+      "       [0.00000000e+00, 1.03089039e-04, 8.57761536e-04, 1.38455695e-03,\n",
+      "        3.61631468e-04, 5.87665673e-04],\n",
+      "       [0.00000000e+00, 1.10478030e-04, 8.65550618e-04, 1.38227706e-03,\n",
+      "        3.77204869e-04, 5.69830379e-04],\n",
+      "       [0.00000000e+00, 8.86781397e-05, 8.81321220e-04, 1.41567947e-03,\n",
+      "        3.71172207e-04, 5.59161913e-04],\n",
+      "       [0.00000000e+00, 9.80941312e-05, 8.79452489e-04, 1.39160298e-03,\n",
+      "        3.71738854e-04, 5.68280515e-04]]), array([0., 0., 0., 0., 0., 0., 0.]))\n",
+      "           fun: 0.0\n",
+      "       message: 'Optimization terminated successfully.'\n",
+      "          nfev: 70\n",
+      "           nit: 28\n",
+      "        status: 0\n",
+      "       success: True\n",
+      "             x: array([0.00000000e+00, 7.79320988e-05, 8.55709877e-04, 1.37422840e-03,\n",
+      "       3.80401235e-04, 5.36779835e-04])\n"
+     ]
+    },
     {
      "output_type": "stream",
      "name": "stderr",
@@ -231,14 +252,14 @@
       ]
      },
      "metadata": {},
-     "execution_count": 6
+     "execution_count": 17
     }
    ],
    "metadata": {}
   },
   {
    "cell_type": "code",
-   "execution_count": 7,
+   "execution_count": 15,
    "source": [
     "log_cruise = simulate(\n",
     "    aircraft=aircraft_model,\n",
@@ -260,7 +281,7 @@
   },
   {
    "cell_type": "code",
-   "execution_count": 8,
+   "execution_count": 16,
    "source": [
     "op_cruise_auto = dict(op_cruise)\n",
     "#op_cruise_auto['ic/theta-deg'] = 0\n",