rebuild documentation examples

convexengineering · Aug 10, 2020 · 03790a7 · 03790a7
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diff --git a/docs/source/examples/autosweep_output.txt b/docs/source/examples/autosweep_output.txt
@@ -37,5 +37,5 @@ l : [ +1        +2.5      +4       ]
 
 Most Sensitive Constraints (in last sweep)
 ------------------------------------------
-    +2 : A >= (l/3)²
+    +2 : A ≥ (l/3)²
 
diff --git a/docs/source/examples/beam_output.txt b/docs/source/examples/beam_output.txt
@@ -20,8 +20,8 @@ EI : -1                                                             Bending stif
 Most Sensitive Constraints
 --------------------------
     +4 : L = 5·dx
-    +1 : w[5] >= w[4] + 0.5·dx·(th[5] + th[4])
- +0.74 : th[2] >= th[1] + 0.5·dx·(M[2] + M[1])/EI
- +0.73 : w[4] >= w[3] + 0.5·dx·(th[4] + th[3])
- +0.64 : M[1] >= M[2] + 0.5·dx·(V[1] + V[2])
+    +1 : w[5] ≥ w[4] + 0.5·dx·(th[5] + th[4])
+ +0.74 : th[2] ≥ th[1] + 0.5·dx·(M[2] + M[1])/EI
+ +0.73 : w[4] ≥ w[3] + 0.5·dx·(th[4] + th[3])
+ +0.64 : M[1] ≥ M[2] + 0.5·dx·(V[1] + V[2])
 
diff --git a/docs/source/examples/boundschecking_output.txt b/docs/source/examples/boundschecking_output.txt
@@ -7,10 +7,10 @@ Cost
 
 Constraints
 -----------
- F >= D + T
+ F ≥ D + T
  D = rf·V²·Ap
  Ap = nu
  T = mf·V
- mf >= mi + mb
+ mf ≥ mi + mb
  mf = rf·V
- Fs <= mi
+ Fs ≤ mi
diff --git a/docs/source/examples/docstringparsing_output.txt b/docs/source/examples/docstringparsing_output.txt
@@ -50,7 +50,7 @@ h : +0.3   minimum height
 
 Most Sensitive Constraints
 --------------------------
-    +1 : A >= 2·(s[0]·s[1] + s[1]·s[2] + s[2]·s[0])
- +0.57 : V <= s[:].prod()
-  +0.3 : s[2] >= h
+    +1 : A ≥ 2·(s[0]·s[1] + s[1]·s[2] + s[2]·s[0])
+ +0.57 : V ≤ s[:].prod()
+  +0.3 : s[2] ≥ h
 
diff --git a/docs/source/examples/external_sp_output.txt b/docs/source/examples/external_sp_output.txt
@@ -11,5 +11,5 @@ y : 0.7071
 Most Sensitive Constraints
 --------------------------
     +1 : <external_constraint.ExternalConstraint object>
-    +1 : x >= 0.785
+    +1 : x ≥ 0.785
 
diff --git a/docs/source/examples/performance_modeling_output.txt b/docs/source/examples/performance_modeling_output.txt
@@ -7,31 +7,31 @@ Constraints
 -----------
  Mission
   "definition of Wburn":
-    Wfuel[:-1] >= Wfuel[1:] + Wburn[:-1]
+    Wfuel[:-1] ≥ Wfuel[1:] + Wburn[:-1]
   "require fuel for the last leg":
-    Wfuel[3] >= Wburn[3]
+    Wfuel[3] ≥ Wburn[3]
 
   FlightSegment
    AircraftP
     "fuel burn rate":
-      Wburn[:] >= 0.1·D[:]
+      Wburn[:] ≥ 0.1·D[:]
     "lift":
-      Aircraft.W + Wfuel[:] <= 0.5·rho[:]·CL[:]·S·V[:]²
+      Aircraft.W + Wfuel[:] ≤ 0.5·rho[:]·CL[:]·S·V[:]²
     "performance":
       WingAero
        "definition of D":
-         D[:] >= 0.5·rho[:]·V[:]²·CD[:]·S
+         D[:] ≥ 0.5·rho[:]·V[:]²·CD[:]·S
        "definition of Re":
          Re[:] = rho[:]·V[:]·c/mu[:]
        "drag model":
-         CD[:] >= 0.074/Re[:]^0.2 + CL[:]²/π/A/e[:]
+         CD[:] ≥ 0.074/Re[:]^0.2 + CL[:]²/π/A/e[:]
 
    FlightState
     (no constraints)
 
  Aircraft
   "definition of W":
-    Aircraft.W >= Aircraft.Fuselage.W + Aircraft.Wing.W
+    Aircraft.W ≥ Aircraft.Fuselage.W + Aircraft.Wing.W
   "components":
     Fuselage
      (no constraints)
@@ -40,7 +40,7 @@ Constraints
      "definition of mean chord":
        c = (S/A)^0.5
      "parametrization of wing weight":
-       Aircraft.Wing.W >= S·Aircraft.Wing.rho
+       Aircraft.Wing.W ≥ S·Aircraft.Wing.rho
 
 Optimal Cost
 ------------
@@ -84,15 +84,15 @@ rho : [ -0.12     -0.11     -0.11     -0.11    ] air density
 Most Sensitive Constraints
 --------------------------
        | Aircraft
-  +1.4 : .W >= .Fuselage.W + .Wing.W
+  +1.4 : .W ≥ .Fuselage.W + .Wing.W
 
        | Mission
-    +1 : Wfuel[0] >= Wfuel[1] + Wburn[0]
- +0.75 : Wfuel[1] >= Wfuel[2] + Wburn[1]
-  +0.5 : Wfuel[2] >= Wfuel[3] + Wburn[2]
+    +1 : Wfuel[0] ≥ Wfuel[1] + Wburn[0]
+ +0.75 : Wfuel[1] ≥ Wfuel[2] + Wburn[1]
+  +0.5 : Wfuel[2] ≥ Wfuel[3] + Wburn[2]
 
        | Aircraft.Wing
- +0.43 : .W >= S·.rho
+ +0.43 : .W ≥ S·.rho
 
 Insensitive Constraints |below +1e-05|
 --------------------------------------
@@ -110,8 +110,8 @@ Constraint Differences
 @@ -41,3 +41,4 @@
         c = (S/A)^0.5
       "parametrization of wing weight":
-        Aircraft.Wing.W >= S·Aircraft.Wing.rho
-+ Wburn[:] >= 0.2·D[:]
+        Aircraft.Wing.W ≥ S·Aircraft.Wing.rho
++ Wburn[:] ≥ 0.2·D[:]
 
 **********************
 
@@ -125,3 +125,4 @@ Sensitivity Differences |above 0.1|
 -----------------------------------
 The largest is -0.00451643.
 
+Links exceed link limit (56 > 50); skipping constraints inside arrays.
diff --git a/docs/source/examples/relaxation_output.txt b/docs/source/examples/relaxation_output.txt
@@ -7,8 +7,8 @@ Cost
 
 Constraints
 -----------
- x <= x_max
- x >= x_min
+ x ≤ x_max
+ x ≥ x_min
 
 With constraints relaxed equally
 ================================
@@ -20,10 +20,10 @@ Cost
 Constraints
 -----------
  "minimum relaxation":
-   C >= 1
+   C ≥ 1
  "relaxed constraints":
-   x <= C·x_max
-   x_min <= C·x
+   x ≤ C·x_max
+   x_min ≤ C·x
 
 Optimal Cost
 ------------
@@ -48,8 +48,8 @@ x_min : +0.5
 
 Most Sensitive Constraints
 --------------------------
-  +0.5 : x <= C·x_max
-  +0.5 : x_min <= C·x
+  +0.5 : x ≤ C·x_max
+  +0.5 : x_min ≤ C·x
 
 
 With constraints relaxed individually
@@ -62,10 +62,10 @@ Cost
 Constraints
 -----------
  "minimum relaxation":
-   C[:] >= 1
+   C[:] ≥ 1
  "relaxed constraints":
-   x <= C[0]·x_max
-   x_min <= C[1]·x
+   x ≤ C[0]·x_max
+   x_min ≤ C[1]·x
 
 Optimal Cost
 ------------
@@ -90,9 +90,9 @@ x_max : -0.99
 
 Most Sensitive Constraints
 --------------------------
-    +1 : x_min <= C[1]·x
- +0.99 : x <= C[0]·x_max
- +0.01 : C[0] >= 1
+    +1 : x_min ≤ C[1]·x
+ +0.99 : x ≤ C[0]·x_max
+ +0.01 : C[0] ≥ 1
 
 
 With constants relaxed individually
@@ -106,17 +106,17 @@ Constraints
 -----------
  Relax2
   "original constraints":
-    x <= x_max
-    x >= x_min
+    x ≤ x_max
+    x ≥ x_min
   "relaxation constraints":
     "x_max":
-      Relax2.x_max >= 1
-      x_max >= Relax2.OriginalValues.x_max/Relax2.x_max
-      x_max <= Relax2.OriginalValues.x_max·Relax2.x_max
+      Relax2.x_max ≥ 1
+      x_max ≥ Relax2.OriginalValues.x_max/Relax2.x_max
+      x_max ≤ Relax2.OriginalValues.x_max·Relax2.x_max
     "x_min":
-      Relax2.x_min >= 1
-      x_min >= Relax2.OriginalValues.x_min/Relax2.x_min
-      x_min <= Relax2.OriginalValues.x_min·Relax2.x_min
+      Relax2.x_min ≥ 1
+      x_min ≥ Relax2.OriginalValues.x_min/Relax2.x_min
+      x_min ≤ Relax2.OriginalValues.x_min·Relax2.x_min
 
 Optimal Cost
 ------------
@@ -145,9 +145,9 @@ x_max : -0.99
 
 Most Sensitive Constraints
 --------------------------
-    +1 : x >= x_min
-    +1 : x_min >= Relax2.OriginalValues.x_min/Relax2.x_min
- +0.99 : x <= x_max
- +0.99 : x_max <= Relax2.OriginalValues.x_max·Relax2.x_max
+    +1 : x ≥ x_min
+    +1 : x_min ≥ Relax2.OriginalValues.x_min/Relax2.x_min
+ +0.99 : x ≤ x_max
+ +0.99 : x_max ≤ Relax2.OriginalValues.x_max·Relax2.x_max
 
 
diff --git a/docs/source/examples/simple_box_output.txt b/docs/source/examples/simple_box_output.txt
@@ -25,6 +25,6 @@ A_{wall} : -1.5  upper limit, wall area
 
 Most Sensitive Constraints
 --------------------------
-  +1.5 : A_{wall} >= 2·h·w + 2·h·d
-  +0.5 : alpha <= h/w
+  +1.5 : A_{wall} ≥ 2·h·w + 2·h·d
+  +0.5 : alpha ≤ h/w
 
diff --git a/docs/source/examples/simple_sp_output.txt b/docs/source/examples/simple_sp_output.txt
@@ -10,8 +10,8 @@ y : 0.1
 
 Most Sensitive Constraints
 --------------------------
-  +1.1 : 1 - y <= x
- +0.11 : y <= 0.1
+  +1.1 : 1 - y ≤ x
+ +0.11 : y ≤ 0.1
 
 x values of each GP solve (note convergence)
 2.50000, 0.92548, 0.90003, 0.90000
diff --git a/docs/source/examples/simpleflight_output.txt b/docs/source/examples/simpleflight_output.txt
@@ -28,11 +28,11 @@ Most Sensitive Variables
 
 Most Sensitive Constraints
 --------------------------
-  +1.3 : W >= W_0 + W_w
-    +1 : C_D >= (CDA0)/S + k·C_f·(\frac{S}{S_{wet}}) + C_L²/(π·A·e)
-    +1 : D >= 0.5·\rho·S·C_D·V²
- +0.96 : W <= 0.5·\rho·S·C_L·V²
- +0.43 : C_f >= 0.074/Re^0.2
+  +1.3 : W ≥ W_0 + W_w
+    +1 : C_D ≥ (CDA0)/S + k·C_f·(\frac{S}{S_{wet}}) + C_L²/(π·A·e)
+    +1 : D ≥ 0.5·\rho·S·C_D·V²
+ +0.96 : W ≤ 0.5·\rho·S·C_L·V²
+ +0.43 : C_f ≥ 0.074/Re^0.2
 
 Solution Diff
 =============
@@ -82,11 +82,11 @@ Most Sensitive Variables
 
 Most Sensitive Constraints (in last sweep)
 ------------------------------------------
-    +1 : C_D >= (CDA0)/S + k·C_f·(\frac{S}{S_{wet}}) + C_L²/(π·A·e)
-    +1 : D >= 0.5·\rho·S·C_D·V²
-    +1 : W >= W_0 + W_w
- +0.57 : W <= 0.5·\rho·S·C_L·V²
- +0.54 : C_f >= 0.074/Re^0.2
+    +1 : C_D ≥ (CDA0)/S + k·C_f·(\frac{S}{S_{wet}}) + C_L²/(π·A·e)
+    +1 : D ≥ 0.5·\rho·S·C_D·V²
+    +1 : W ≥ W_0 + W_w
+ +0.57 : W ≤ 0.5·\rho·S·C_L·V²
+ +0.54 : C_f ≥ 0.074/Re^0.2
 
 Solution Diff
 =============

diff --git a/docs/source/examples/sin_approx_example_output.txt b/docs/source/examples/sin_approx_example_output.txt
@@ -10,6 +10,6 @@ y : 0.7854
 
 Most Sensitive Constraints
 --------------------------
-    +1 : x >= 0.785
-    +1 : y >= x
+    +1 : x ≥ 0.785
+    +1 : y ≥ x
 
diff --git a/docs/source/examples/sp_to_gp_sweep_output.txt b/docs/source/examples/sp_to_gp_sweep_output.txt
@@ -7,15 +7,15 @@ Warnings
 ========
 Unexpectedly Loose Constraints in sweep 0
 -----------------------------------------
-0.9585 >= 0.9187 : V_{f_{avail}} >= V_f
+0.9585 >= 0.9187 : V_{f_{avail}} ≥ V_f
 
 Unexpectedly Loose Constraints in sweep 1
 -----------------------------------------
-0.9585 >= 0.9187 : V_{f_{avail}} >= V_f
+0.9585 >= 0.9187 : V_{f_{avail}} ≥ V_f
 
 Unexpectedly Loose Constraints in sweep 2
 -----------------------------------------
-0.9585 >= 0.9187 : V_{f_{avail}} >= V_f
+0.9585 >= 0.9187 : V_{f_{avail}} ≥ V_f
 
 Swept Variables
 ---------------
@@ -52,9 +52,9 @@ Most Sensitive Variables
 
 Most Sensitive Constraints (in last sweep)
 ------------------------------------------
-  +1.2 : C_D >= (CDA0)/S + k·C_f·(\frac{S}{S_{wet}}) + C_L²/(π·A·e)
-  +1.2 : D >= 0.5·\rho·S·C_D·V²
-  +1.2 : T_{flight} >= Range/V
-  +1.2 : W_f >= TSFC·T_{flight}·D
- +0.74 : C_f >= 0.074/Re^0.2
+  +1.2 : C_D ≥ (CDA0)/S + k·C_f·(\frac{S}{S_{wet}}) + C_L²/(π·A·e)
+  +1.2 : D ≥ 0.5·\rho·S·C_D·V²
+  +1.2 : T_{flight} ≥ Range/V
+  +1.2 : W_f ≥ TSFC·T_{flight}·D
+ +0.74 : C_f ≥ 0.074/Re^0.2
 
diff --git a/docs/source/examples/unbounded_output.txt b/docs/source/examples/unbounded_output.txt
@@ -14,5 +14,5 @@ x : 1e+30
 
 Most Sensitive Constraints
 --------------------------
-    +1 : x <= 1e+30
+    +1 : x ≤ 1e+30
 
diff --git a/docs/source/examples/vectorize_output.txt b/docs/source/examples/vectorize_output.txt
@@ -10,7 +10,7 @@ x : 1
 
 Most Sensitive Constraints
 --------------------------
-    +1 : x >= 1
+    +1 : x ≥ 1
 
 __________
 
@@ -26,7 +26,7 @@ x : [ 1         2         1        ]
 
 Most Sensitive Constraints
 --------------------------
-    +1 : x[0] >= 1
-    +1 : x[1] >= 2
-    +1 : x[2] >= 1
+    +1 : x[0] ≥ 1
+    +1 : x[1] ≥ 2
+    +1 : x[2] ≥ 1
 
diff --git a/docs/source/examples/water_tank_output.txt b/docs/source/examples/water_tank_output.txt
@@ -17,7 +17,7 @@ Variable Sensitivities
 
 Most Sensitive Constraints
 --------------------------
-    +1 : A >= 2·(d[0]·d[1] + d[0]·d[2] + d[1]·d[2])
+    +1 : A ≥ 2·(d[0]·d[1] + d[0]·d[2] + d[1]·d[2])
  +0.67 : M = V·\rho
  +0.67 : V = d[0]·d[1]·d[2]