re-add PanelAero package for dot-derivatives computation using DLM model

Author: LeonDeligny

environment.yml

@@ -62,4 +62,5 @@ dependencies:
     - streamlit-autorefresh
     - vtk==9.3.0
     - scikit-optimize==0.10.2
-    - framat==0.5
+    - framat==0.5
+    - panelaero==2024.2

installation/Pentagrow/include/eigen/debug/gdb/printers.py

@@ -26,9 +26,10 @@
 #      register_eigen_printers (None)
 #      end
 
-import gdb
 import re
-import itertools
+import gdb
+
+from functools import partial
 
 
 class EigenMatrixPrinter:
@@ -90,7 +91,7 @@ def __iter__ (self):
 			return self
 
 		def next(self):
-                        return self.__next__()  # Python 2.x compatibility
+			return self.__next__()  # Python 2.x compatibility
 
 		def __next__(self):
 
@@ -156,7 +157,7 @@ def __iter__ (self):
 			return self
 
 		def next(self):
-                        return self.__next__()  # Python 2.x compatibility
+			return self.__next__()  # Python 2.x compatibility
 
 		def __next__(self):
 			element = self.currentElement
@@ -177,10 +178,10 @@ def children(self):
 	def to_string(self):
 		return "Eigen::Quaternion<%s> (data ptr: %s)" % (self.innerType, self.data)
 
-def build_eigen_dictionary ():
-	pretty_printers_dict[re.compile('^Eigen::Quaternion<.*>$')] = lambda val: EigenQuaternionPrinter(val)
-	pretty_printers_dict[re.compile('^Eigen::Matrix<.*>$')] = lambda val: EigenMatrixPrinter("Matrix", val)
-	pretty_printers_dict[re.compile('^Eigen::Array<.*>$')]  = lambda val: EigenMatrixPrinter("Array",  val)
+def build_eigen_dictionary():
+    pretty_printers_dict[re.compile('^Eigen::Quaternion<.*>$')] = EigenQuaternionPrinter
+    pretty_printers_dict[re.compile('^Eigen::Matrix<.*>$')] = partial(EigenMatrixPrinter, "Matrix")
+    pretty_printers_dict[re.compile('^Eigen::Array<.*>$')]  = partial(EigenMatrixPrinter, "Array")
 
 def register_eigen_printers(obj):
 	"Register eigen pretty-printers with objfile Obj"

src/ceasiompy/CPACSUpdater/func/utils.py

@@ -411,5 +411,7 @@ def plot_values(
 # ==============================================================================
 #    MAIN
 # ==============================================================================
+
+
 if __name__ == "__main__":
     log.info("Nothing to execute!")

src/ceasiompy/StaticStability/README.md

@@ -29,7 +29,6 @@ A unique (Mach, Altitude, AoA, AoS) in the aeromap suffices to do the Static Sta
 
 In the results directory you can find:
     1. a Markdown file which contains a table with the stability results (Stable/Unstable wrt to the 3 different axes) for the specific aeromap.
-
     2. A longitudinal, directional and lateral html plot of the Pitch, Yaw and Roll moments wrt AoA, AoS and AoS respectively.
 
 ## Installation or requirements