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convexengineering · Jan 7, 2022 · 447feeb · 447feeb
1 parent 230f776
commit 447feeb
Showing 1 changed file with 3 additions and 12 deletions.
diff --git a/docs/source/examples/performance_modeling_output.txt b/docs/source/examples/performance_modeling_output.txt
@@ -112,18 +112,9 @@ Constraint Differences
 
 **********************
 
-Variable(s) of this solution which are not in the argument:
-  Fuselage.W
-  D[:]
-  Wburn[:]
-  Wing.rho
-  A
-  Wfuel[:]
-  S
-  Wing.W
-  c
-
 Relative Differences |above 1%|
 -------------------------------
-The largest is +0.217736%.
+Wburn : [ +102.1%   +101.6%   +101.1%   +100.5%  ] segment fuel burn
+Wfuel : [ +101.3%   +101.1%   +100.8%   +100.5%  ] fuel weight
+    D : [   +1.1%       -         -         -    ] drag force