Skip to content
Failed

Console Output

Skipping 154 KB.. Full Log
91  2.0e-07  8.1e-03  1.2e-05  1.00e+00   1.666374709e+02   1.666379208e+02   1.1e-10  0.79  
92  1.8e-07  8.0e-03  1.1e-05  9.99e-01   1.666375000e+02   1.666379050e+02   9.5e-11  0.80  
93  1.6e-07  8.0e-03  9.9e-06  9.99e-01   1.666375262e+02   1.666378908e+02   8.6e-11  0.81  
94  1.5e-07  8.0e-03  8.9e-06  1.00e+00   1.666375497e+02   1.666378779e+02   7.7e-11  0.82  
95  1.3e-07  8.0e-03  8.0e-06  1.00e+00   1.666375709e+02   1.666378663e+02   6.9e-11  0.83  
96  1.2e-07  8.0e-03  7.2e-06  1.00e+00   1.666375900e+02   1.666378558e+02   6.2e-11  0.83  
97  1.1e-07  7.9e-03  6.5e-06  1.00e+00   1.666376072e+02   1.666378464e+02   5.6e-11  0.84  
98  9.5e-08  7.9e-03  5.8e-06  9.99e-01   1.666376226e+02   1.666378379e+02   5.1e-11  0.85  
99  8.6e-08  7.9e-03  5.2e-06  1.00e+00   1.666376365e+02   1.666378303e+02   4.6e-11  0.86  
100 7.7e-08  7.9e-03  4.7e-06  1.00e+00   1.666376490e+02   1.666378234e+02   4.1e-11  0.87  
101 6.9e-08  7.9e-03  4.2e-06  1.00e+00   1.666376603e+02   1.666378172e+02   3.7e-11  0.87  
102 6.2e-08  7.9e-03  3.8e-06  9.98e-01   1.666376704e+02   1.666378117e+02   3.3e-11  0.88  
103 5.6e-08  7.8e-03  3.4e-06  1.00e+00   1.666376796e+02   1.666378067e+02   3.0e-11  0.89  
104 5.1e-08  7.8e-03  3.1e-06  9.99e-01   1.666376878e+02   1.666378022e+02   2.7e-11  0.90  
105 4.6e-08  7.8e-03  2.8e-06  1.00e+00   1.666376951e+02   1.666377981e+02   2.4e-11  0.91  
106 4.1e-08  7.8e-03  2.5e-06  9.96e-01   1.666377018e+02   1.666377945e+02   2.2e-11  0.91  
107 3.7e-08  7.8e-03  2.3e-06  9.98e-01   1.666377078e+02   1.666377912e+02   2.0e-11  0.92  
108 3.3e-08  7.8e-03  2.0e-06  1.00e+00   1.666377132e+02   1.666377883e+02   1.8e-11  0.93  
109 3.0e-08  7.0e-03  1.8e-06  1.01e+00   1.666377181e+02   1.666377855e+02   1.6e-11  0.94  
110 2.7e-08  6.3e-03  1.6e-06  1.00e+00   1.666377224e+02   1.666377831e+02   1.4e-11  0.94  
111 2.4e-08  5.7e-03  1.5e-06  1.00e+00   1.666377264e+02   1.666377810e+02   1.3e-11  0.95  
112 2.2e-08  5.1e-03  1.3e-06  1.01e+00   1.666377300e+02   1.666377790e+02   1.2e-11  0.96  
113 2.0e-08  4.6e-03  1.2e-06  1.00e+00   1.666377332e+02   1.666377772e+02   1.0e-11  0.96  
114 2.0e-08  4.6e-03  1.2e-06  9.95e-01   1.666377333e+02   1.666377773e+02   1.0e-11  0.97  
115 1.8e-08  4.1e-03  1.1e-06  9.97e-01   1.666377361e+02   1.666377757e+02   9.4e-12  0.98  
116 1.6e-08  3.7e-03  9.7e-07  1.01e+00   1.666377387e+02   1.666377743e+02   8.5e-12  0.99  
117 1.5e-08  3.3e-03  8.7e-07  1.01e+00   1.666377410e+02   1.666377730e+02   7.6e-12  0.99  
118 1.3e-08  3.0e-03  7.8e-07  1.00e+00   1.666377431e+02   1.666377718e+02   6.9e-12  1.00  
119 1.2e-08  2.7e-03  7.0e-07  9.99e-01   1.666377450e+02   1.666377708e+02   6.2e-12  1.01  
120 1.1e-08  2.4e-03  6.3e-07  9.94e-01   1.666377466e+02   1.666377699e+02   5.6e-12  1.02  
121 9.7e-09  2.2e-03  5.7e-07  9.92e-01   1.666377481e+02   1.666377690e+02   5.0e-12  1.03  
122 9.0e-09  2.0e-03  5.1e-07  1.01e+00   1.666377495e+02   1.666377683e+02   4.5e-12  1.04  
123 8.2e-09  1.8e-03  4.6e-07  9.94e-01   1.666377507e+02   1.666377676e+02   4.1e-12  1.05  
124 7.3e-09  1.6e-03  4.2e-07  1.01e+00   1.666377519e+02   1.666377670e+02   3.7e-12  1.05  
125 6.6e-09  1.4e-03  3.7e-07  1.00e+00   1.666377528e+02   1.666377664e+02   3.3e-12  1.06  
126 5.9e-09  1.3e-03  3.4e-07  9.98e-01   1.666377537e+02   1.666377659e+02   3.0e-12  1.07  
127 7.8e-09  1.2e-03  3.0e-07  9.92e-01   1.666377545e+02   1.666377655e+02   2.7e-12  1.08  
128 7.0e-09  1.0e-03  2.7e-07  1.01e+00   1.666377552e+02   1.666377651e+02   2.4e-12  1.09  
129 6.3e-09  9.4e-04  2.5e-07  1.04e+00   1.666377560e+02   1.666377647e+02   2.2e-12  1.10  
130 4.4e-09  8.5e-04  2.2e-07  9.87e-01   1.666377566e+02   1.666377644e+02   2.0e-12  1.10  
131 2.2e-08  2.4e-04  4.3e-09  7.60e-01   1.666377647e+02   1.666377650e+02   5.2e-13  1.11  
Optimizer terminated. Time: 1.11    

solsta = 1, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 1.6663776471e+02    nrm: 2e+01    Viol.  con: 8e-07    var: 0e+00  
  Dual.    obj: 1.6663776503e+02    nrm: 9e+02    Viol.  con: 0e+00    var: 4e-03  
* End solution on dual form. *
Transforming to primal solution.
Solving took 1.14 seconds.
Using solver 'mosek'
Solving for 1768 variables.
MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (312) of matrix 'A'.
MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (450) of matrix 'A'.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Problem
  Name                   :                 
  Objective sense        : max             
  Type                   : GECO (general convex optimization problem)
  Constraints            : 1769            
  Cones                  : 0               
  Scalar variables       : 6131            
  Matrix variables       : 0               
  Integer variables      : 0               

Optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Freed constraints in eliminator : 482
Eliminator terminated.
Eliminator started.
Freed constraints in eliminator : 6
Eliminator terminated.
Eliminator - tries                  : 2                 time                   : 0.00            
Lin. dep.  - tries                  : 1                 time                   : 0.00            
Lin. dep.  - number                 : 0               
Presolve terminated. Time: 0.01    
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Problem
  Name                   :                 
  Objective sense        : max             
  Type                   : GECO (general convex optimization problem)
  Constraints            : 1769            
  Cones                  : 0               
  Scalar variables       : 6131            
  Matrix variables       : 0               
  Integer variables      : 0               

Optimizer  - threads                : 8               
Optimizer  - solved problem         : the primal      
Optimizer  - Constraints            : 873
Optimizer  - Cones                  : 0
Optimizer  - Scalar variables       : 3462              conic                  : 0               
Optimizer  - Semi-definite variables: 0                 scalarized             : 0               
Factor     - setup time             : 0.02              dense det. time        : 0.00            
Factor     - ML order time          : 0.00              GP order time          : 0.01            
Factor     - nonzeros before factor : 1.49e+04          after factor           : 1.57e+05        
Factor     - dense dim.             : 0                 flops                  : 3.26e+07        
Factor     - GP saved nzs           : 3.37e+04          GP saved flops         : 9.34e+05        
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+03  3.0e+03  1.2e+05  0.00e+00   -1.223844447e+05  2.000000000e+00   1.0e+00  0.03  
1   1.7e+03  2.2e+03  8.9e+04  -9.71e-01  -1.216526186e+05  2.621307516e+00   7.3e-01  0.04  
2   8.7e+02  1.1e+03  4.7e+04  -9.59e-01  -1.193637044e+05  4.626148661e+00   3.8e-01  0.05  
3   2.9e+02  3.8e+02  1.5e+04  -9.21e-01  -1.103995372e+05  1.997391954e+01   1.3e-01  0.06  
4   2.9e+02  3.8e+02  1.5e+04  -7.71e-01  -1.080822190e+05  2.042697686e+03   1.3e-01  0.07  
5   1.2e+02  1.6e+02  6.4e+03  -7.60e-01  -8.699173306e+04  6.321800779e+03   5.3e-02  0.07  
6   4.1e+01  5.4e+01  2.2e+03  -4.49e-01  -4.865820875e+04  1.101126990e+04   1.8e-02  0.08  
7   2.4e+01  3.2e+01  1.3e+03  1.99e-01   -3.315603760e+04  7.461031895e+03   1.1e-02  0.09  
8   1.2e+01  1.6e+01  6.5e+02  4.98e-01   -1.808984783e+04  4.488227388e+03   5.3e-03  0.10  
9   4.6e+00  6.0e+00  2.5e+02  7.63e-01   -7.017022285e+03  2.200334188e+03   2.0e-03  0.10  
10  2.1e+00  2.8e+00  1.1e+02  9.36e-01   -3.013574993e+03  1.298063265e+03   9.5e-04  0.11  
11  1.3e+00  1.6e+00  6.8e+01  9.86e-01   -1.733134262e+03  8.404669180e+02   5.6e-04  0.12  
12  8.1e-01  1.1e+00  4.4e+01  9.87e-01   -1.079217140e+03  6.046322849e+02   3.7e-04  0.13  
13  6.1e-01  8.2e-01  3.3e+01  9.60e-01   -7.896096919e+02  4.869528628e+02   2.8e-04  0.13  
14  3.6e-01  4.9e-01  1.9e+01  9.97e-01   -3.718428962e+02  3.755278439e+02   1.6e-04  0.14  
15  1.8e-01  2.6e-01  1.0e+01  9.91e-01   -1.239916996e+02  2.622463982e+02   8.4e-05  0.15  
16  8.5e-02  1.4e-01  4.7e+00  1.00e+00   2.254305964e+01   2.029655165e+02   4.0e-05  0.15  
17  7.2e-02  1.1e-01  4.0e+00  1.02e+00   4.882140998e+01   2.008632442e+02   3.4e-05  0.16  
18  2.2e-02  8.7e-02  1.3e+00  1.02e+00   1.302065439e+02   1.776815265e+02   1.1e-05  0.17  
19  7.3e-03  1.8e-01  4.1e-01  1.01e+00   1.552256873e+02   1.707986362e+02   3.5e-06  0.18  
20  2.9e-03  1.6e-01  1.7e-01  1.01e+00   1.619245831e+02   1.681612439e+02   1.4e-06  0.18  
21  1.5e-03  1.0e-01  8.9e-02  1.00e+00   1.640996354e+02   1.674649706e+02   7.6e-07  0.19  
22  5.3e-04  1.0e-01  3.1e-02  1.01e+00   1.656947408e+02   1.668767093e+02   2.7e-07  0.20  
23  1.9e-04  1.0e-01  1.1e-02  1.01e+00   1.662324741e+02   1.666610701e+02   1.0e-07  0.20  
24  1.7e-04  9.3e-02  1.0e-02  1.01e+00   1.662653398e+02   1.666509812e+02   9.0e-08  0.21  
25  1.5e-04  8.5e-02  9.3e-03  1.01e+00   1.662923135e+02   1.666392585e+02   8.1e-08  0.22  
26  1.4e-04  7.7e-02  8.4e-03  1.01e+00   1.663167164e+02   1.666288558e+02   7.3e-08  0.23  
27  1.2e-04  7.0e-02  7.5e-03  1.01e+00   1.663385691e+02   1.666194032e+02   6.5e-08  0.23  
28  1.1e-04  6.4e-02  6.8e-03  1.01e+00   1.663581774e+02   1.666108524e+02   5.9e-08  0.24  
29  1.0e-04  5.8e-02  6.1e-03  1.01e+00   1.663757676e+02   1.666031129e+02   5.3e-08  0.25  
30  9.1e-05  5.3e-02  5.5e-03  1.01e+00   1.663915491e+02   1.665961089e+02   4.8e-08  0.26  
31  8.2e-05  4.9e-02  4.9e-03  1.01e+00   1.664057090e+02   1.665897710e+02   4.3e-08  0.26  
32  7.4e-05  4.5e-02  4.4e-03  1.01e+00   1.664184151e+02   1.665840367e+02   3.9e-08  0.27  
33  6.6e-05  4.1e-02  4.0e-03  1.01e+00   1.664298179e+02   1.665788495e+02   3.5e-08  0.28  
34  6.0e-05  3.8e-02  3.6e-03  1.01e+00   1.664400524e+02   1.665741581e+02   3.1e-08  0.29  
35  5.4e-05  3.5e-02  3.2e-03  1.00e+00   1.664492392e+02   1.665699159e+02   2.8e-08  0.29  
36  4.8e-05  3.2e-02  2.9e-03  1.00e+00   1.664574865e+02   1.665660807e+02   2.5e-08  0.30  
37  4.3e-05  3.0e-02  2.6e-03  1.00e+00   1.664648914e+02   1.665626140e+02   2.3e-08  0.31  
38  3.9e-05  2.7e-02  2.4e-03  1.00e+00   1.664715405e+02   1.665594811e+02   2.1e-08  0.32  
39  3.5e-05  2.5e-02  2.1e-03  1.00e+00   1.664775117e+02   1.665566504e+02   1.9e-08  0.33  
40  3.2e-05  2.4e-02  1.9e-03  1.00e+00   1.664828746e+02   1.665540932e+02   1.7e-08  0.33  
41  2.8e-05  2.2e-02  1.7e-03  1.00e+00   1.664876918e+02   1.665517834e+02   1.5e-08  0.34  
42  2.6e-05  2.1e-02  1.6e-03  1.00e+00   1.664920191e+02   1.665496975e+02   1.3e-08  0.35  
43  2.3e-05  1.9e-02  1.4e-03  1.00e+00   1.664959069e+02   1.665478142e+02   1.2e-08  0.36  
44  2.1e-05  1.8e-02  1.3e-03  1.00e+00   1.664994001e+02   1.665461142e+02   1.1e-08  0.37  
45  1.9e-05  1.7e-02  1.1e-03  1.00e+00   1.665025391e+02   1.665445798e+02   9.8e-09  0.38  
46  1.7e-05  1.6e-02  1.0e-03  1.00e+00   1.665053603e+02   1.665431953e+02   8.9e-09  0.39  
47  1.5e-05  1.5e-02  9.2e-04  1.00e+00   1.665078959e+02   1.665419462e+02   8.0e-09  0.40  
48  1.4e-05  1.5e-02  8.2e-04  1.00e+00   1.665101753e+02   1.665408196e+02   7.2e-09  0.41  
49  1.2e-05  1.4e-02  7.4e-04  1.00e+00   1.665122245e+02   1.665398036e+02   6.5e-09  0.42  
50  1.1e-05  1.3e-02  6.7e-04  1.00e+00   1.665140670e+02   1.665388876e+02   5.8e-09  0.43  
51  9.9e-06  1.3e-02  6.0e-04  1.00e+00   1.665157237e+02   1.665380619e+02   5.2e-09  0.44  
52  8.9e-06  1.2e-02  5.4e-04  1.00e+00   1.665172136e+02   1.665373176e+02   4.7e-09  0.46  
53  8.0e-06  1.2e-02  4.9e-04  1.00e+00   1.665185536e+02   1.665366470e+02   4.2e-09  0.46  
54  7.2e-06  1.2e-02  4.4e-04  1.00e+00   1.665197588e+02   1.665360426e+02   3.8e-09  0.47  
55  6.5e-06  1.1e-02  3.9e-04  1.00e+00   1.665208428e+02   1.665354981e+02   3.4e-09  0.48  
56  5.9e-06  1.1e-02  3.6e-04  1.00e+00   1.665218178e+02   1.665350076e+02   3.1e-09  0.49  
57  5.3e-06  1.1e-02  3.2e-04  1.00e+00   1.665226949e+02   1.665345656e+02   2.8e-09  0.50  
58  4.8e-06  1.0e-02  2.9e-04  1.00e+00   1.665234838e+02   1.665341674e+02   2.5e-09  0.51  
59  4.3e-06  1.0e-02  2.6e-04  1.00e+00   1.665241934e+02   1.665338087e+02   2.3e-09  0.51  
60  3.8e-06  1.0e-02  2.3e-04  1.00e+00   1.665248317e+02   1.665334854e+02   2.0e-09  0.52  
61  3.5e-06  9.8e-03  2.1e-04  1.00e+00   1.665254057e+02   1.665331941e+02   1.8e-09  0.53  
62  3.1e-06  9.7e-03  1.9e-04  1.00e+00   1.665259221e+02   1.665329316e+02   1.6e-09  0.54  
63  2.8e-06  9.5e-03  1.7e-04  1.00e+00   1.665263864e+02   1.665326951e+02   1.5e-09  0.55  
64  2.5e-06  9.4e-03  1.5e-04  1.00e+00   1.665268042e+02   1.665324819e+02   1.3e-09  0.55  
65  2.3e-06  9.2e-03  1.4e-04  1.00e+00   1.665271799e+02   1.665322899e+02   1.2e-09  0.56  
66  2.0e-06  9.1e-03  1.2e-04  1.00e+00   1.665275179e+02   1.665321169e+02   1.1e-09  0.57  
67  1.8e-06  9.0e-03  1.1e-04  1.00e+00   1.665278220e+02   1.665319611e+02   9.7e-10  0.58  
68  1.7e-06  8.9e-03  1.0e-04  1.00e+00   1.665280955e+02   1.665318208e+02   8.7e-10  0.59  
69  1.5e-06  8.9e-03  9.0e-05  1.00e+00   1.665283416e+02   1.665316944e+02   7.9e-10  0.59  
70  1.3e-06  8.8e-03  8.1e-05  1.00e+00   1.665285630e+02   1.665315805e+02   7.1e-10  0.60  
71  1.2e-06  8.7e-03  7.3e-05  1.00e+00   1.665287621e+02   1.665314779e+02   6.4e-10  0.61  
72  1.1e-06  8.7e-03  6.6e-05  1.00e+00   1.665289413e+02   1.665313854e+02   5.7e-10  0.62  
73  9.8e-07  8.6e-03  5.9e-05  1.00e+00   1.665291024e+02   1.665313022e+02   5.2e-10  0.63  
74  8.8e-07  8.6e-03  5.3e-05  1.00e+00   1.665292473e+02   1.665312271e+02   4.6e-10  0.63  
75  7.9e-07  8.5e-03  4.8e-05  1.00e+00   1.665293777e+02   1.665311595e+02   4.2e-10  0.64  
76  7.1e-07  8.5e-03  4.3e-05  1.00e+00   1.665294950e+02   1.665310986e+02   3.8e-10  0.65  
77  6.4e-07  8.4e-03  3.9e-05  1.00e+00   1.665296004e+02   1.665310437e+02   3.4e-10  0.66  
78  5.8e-07  8.4e-03  3.5e-05  1.00e+00   1.665296952e+02   1.665309942e+02   3.0e-10  0.67  
79  5.2e-07  8.3e-03  3.2e-05  1.00e+00   1.665297805e+02   1.665309496e+02   2.7e-10  0.67  
80  4.7e-07  8.3e-03  2.8e-05  1.00e+00   1.665298572e+02   1.665309093e+02   2.5e-10  0.68  
81  4.2e-07  8.3e-03  2.6e-05  1.00e+00   1.665299261e+02   1.665308731e+02   2.2e-10  0.69  
82  3.8e-07  8.2e-03  2.3e-05  1.00e+00   1.665299881e+02   1.665308404e+02   2.0e-10  0.70  
83  3.4e-07  8.2e-03  2.1e-05  1.00e+00   1.665300439e+02   1.665308109e+02   1.8e-10  0.71  
84  3.1e-07  8.2e-03  1.9e-05  1.00e+00   1.665300941e+02   1.665307844e+02   1.6e-10  0.71  
85  2.8e-07  8.2e-03  1.7e-05  1.00e+00   1.665301392e+02   1.665307605e+02   1.5e-10  0.72  
86  2.5e-07  8.1e-03  1.5e-05  1.00e+00   1.665301797e+02   1.665307389e+02   1.3e-10  0.73  
87  2.2e-07  8.1e-03  1.4e-05  1.00e+00   1.665302162e+02   1.665307195e+02   1.2e-10  0.74  
88  2.0e-07  8.1e-03  1.2e-05  1.00e+00   1.665302490e+02   1.665307020e+02   1.1e-10  0.74  
89  1.8e-07  8.1e-03  1.1e-05  1.00e+00   1.665302786e+02   1.665306863e+02   9.6e-11  0.75  
90  1.6e-07  8.1e-03  9.9e-06  1.00e+00   1.665303052e+02   1.665306721e+02   8.6e-11  0.76  
91  1.5e-07  8.0e-03  8.9e-06  1.00e+00   1.665303291e+02   1.665306593e+02   7.7e-11  0.77  
92  1.3e-07  8.0e-03  8.0e-06  1.00e+00   1.665303506e+02   1.665306478e+02   7.0e-11  0.78  
93  1.2e-07  8.0e-03  7.2e-06  1.00e+00   1.665303699e+02   1.665306374e+02   6.3e-11  0.78  
94  1.1e-07  8.0e-03  6.5e-06  1.00e+00   1.665303873e+02   1.665306281e+02   5.6e-11  0.79  
95  9.6e-08  8.0e-03  5.8e-06  1.00e+00   1.665304030e+02   1.665306197e+02   5.1e-11  0.80  
96  8.7e-08  7.9e-03  5.3e-06  1.00e+00   1.665304171e+02   1.665306121e+02   4.6e-11  0.81  
97  7.8e-08  7.9e-03  4.7e-06  1.00e+00   1.665304298e+02   1.665306053e+02   4.1e-11  0.82  
98  7.0e-08  7.9e-03  4.3e-06  1.00e+00   1.665304412e+02   1.665305991e+02   3.7e-11  0.83  
99  6.3e-08  7.9e-03  3.8e-06  9.99e-01   1.665304515e+02   1.665305936e+02   3.3e-11  0.83  
100 5.7e-08  7.9e-03  3.4e-06  1.00e+00   1.665304607e+02   1.665305887e+02   3.0e-11  0.84  
101 5.1e-08  7.8e-03  3.1e-06  1.00e+00   1.665304691e+02   1.665305842e+02   2.7e-11  0.85  
102 4.6e-08  7.8e-03  2.8e-06  1.00e+00   1.665304766e+02   1.665305802e+02   2.4e-11  0.86  
103 4.1e-08  7.8e-03  2.5e-06  9.99e-01   1.665304833e+02   1.665305766e+02   2.2e-11  0.87  
104 3.7e-08  7.8e-03  2.3e-06  9.99e-01   1.665304894e+02   1.665305733e+02   2.0e-11  0.87  
105 3.4e-08  7.8e-03  2.0e-06  9.99e-01   1.665304948e+02   1.665305704e+02   1.8e-11  0.88  
106 3.0e-08  7.7e-03  1.8e-06  1.00e+00   1.665304997e+02   1.665305678e+02   1.6e-11  0.89  
107 2.7e-08  7.7e-03  1.6e-06  1.00e+00   1.665305041e+02   1.665305655e+02   1.4e-11  0.90  
108 2.4e-08  7.7e-03  1.5e-06  9.97e-01   1.665305081e+02   1.665305633e+02   1.3e-11  0.91  
109 2.2e-08  6.9e-03  1.3e-06  1.00e+00   1.665305117e+02   1.665305614e+02   1.2e-11  0.91  
110 2.0e-08  6.2e-03  1.2e-06  9.97e-01   1.665305149e+02   1.665305596e+02   1.0e-11  0.92  
111 1.8e-08  5.6e-03  1.1e-06  9.97e-01   1.665305178e+02   1.665305581e+02   9.4e-12  0.93  
112 1.6e-08  5.0e-03  9.7e-07  1.00e+00   1.665305205e+02   1.665305567e+02   8.5e-12  0.94  
113 1.5e-08  4.5e-03  8.8e-07  9.96e-01   1.665305228e+02   1.665305554e+02   7.6e-12  0.95  
114 1.3e-08  4.1e-03  7.9e-07  9.88e-01   1.665305249e+02   1.665305545e+02   6.9e-12  0.96  
115 1.2e-08  3.7e-03  7.1e-07  9.88e-01   1.665305268e+02   1.665305535e+02   6.2e-12  0.97  
116 1.1e-08  3.3e-03  6.4e-07  9.98e-01   1.665305285e+02   1.665305524e+02   5.6e-12  0.98  
117 9.9e-09  3.0e-03  5.8e-07  9.78e-01   1.665305300e+02   1.665305517e+02   5.0e-12  0.98  
118 8.9e-09  2.7e-03  5.2e-07  9.91e-01   1.665305314e+02   1.665305510e+02   4.5e-12  0.99  
119 8.0e-09  2.4e-03  4.7e-07  9.99e-01   1.665305327e+02   1.665305503e+02   4.1e-12  1.00  
120 7.2e-09  2.2e-03  4.2e-07  1.01e+00   1.665305338e+02   1.665305496e+02   3.7e-12  1.01  
121 6.5e-09  2.0e-03  3.8e-07  9.92e-01   1.665305348e+02   1.665305491e+02   3.3e-12  1.02  
122 5.9e-09  1.8e-03  3.4e-07  9.85e-01   1.665305358e+02   1.665305486e+02   3.0e-12  1.02  
123 5.3e-09  1.6e-03  3.1e-07  9.93e-01   1.665305366e+02   1.665305481e+02   2.7e-12  1.03  
124 4.8e-09  1.4e-03  2.8e-07  9.93e-01   1.665305373e+02   1.665305477e+02   2.4e-12  1.04  
125 4.4e-09  1.3e-03  2.5e-07  9.82e-01   1.665305380e+02   1.665305473e+02   2.2e-12  1.05  
126 3.9e-09  1.2e-03  2.2e-07  9.90e-01   1.665305386e+02   1.665305470e+02   2.0e-12  1.06  
127 3.6e-09  1.0e-03  2.0e-07  1.00e+00   1.665305391e+02   1.665305467e+02   1.8e-12  1.07  
128 3.4e-09  9.3e-04  1.8e-07  9.96e-01   1.665305396e+02   1.665305464e+02   1.6e-12  1.08  
129 3.1e-09  8.4e-04  1.6e-07  1.01e+00   1.665305400e+02   1.665305462e+02   1.4e-12  1.08  
130 3.3e-10  8.8e-05  1.7e-08  1.00e+00   1.665305435e+02   1.665305442e+02   1.5e-13  1.09  
Optimizer terminated. Time: 1.09    

solsta = 1, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 1.6653054354e+02    nrm: 2e+01    Viol.  con: 5e-09    var: 0e+00  
  Dual.    obj: 1.6653054419e+02    nrm: 1e+03    Viol.  con: 0e+00    var: 6e-04  
* End solution on dual form. *
Transforming to primal solution.
Solving took 1.12 seconds.
Using solver 'mosek'
Solving for 1768 variables.
MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (450) of matrix 'A'.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Problem
  Name                   :                 
  Objective sense        : max             
  Type                   : GECO (general convex optimization problem)
  Constraints            : 1769            
  Cones                  : 0               
  Scalar variables       : 6131            
  Matrix variables       : 0               
  Integer variables      : 0               

Optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Freed constraints in eliminator : 482
Eliminator terminated.
Eliminator started.
Freed constraints in eliminator : 6
Eliminator terminated.
Eliminator - tries                  : 2                 time                   : 0.00            
Lin. dep.  - tries                  : 1                 time                   : 0.00            
Lin. dep.  - number                 : 0               
Presolve terminated. Time: 0.01    
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Problem
  Name                   :                 
  Objective sense        : max             
  Type                   : GECO (general convex optimization problem)
  Constraints            : 1769            
  Cones                  : 0               
  Scalar variables       : 6131            
  Matrix variables       : 0               
  Integer variables      : 0               

Optimizer  - threads                : 8               
Optimizer  - solved problem         : the primal      
Optimizer  - Constraints            : 873
Optimizer  - Cones                  : 0
Optimizer  - Scalar variables       : 3462              conic                  : 0               
Optimizer  - Semi-definite variables: 0                 scalarized             : 0               
Factor     - setup time             : 0.02              dense det. time        : 0.00            
Factor     - ML order time          : 0.00              GP order time          : 0.02            
Factor     - nonzeros before factor : 1.49e+04          after factor           : 1.57e+05        
Factor     - dense dim.             : 0                 flops                  : 3.26e+07        
Factor     - GP saved nzs           : 3.37e+04          GP saved flops         : 9.34e+05        
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+03  3.0e+03  1.2e+05  0.00e+00   -1.223814476e+05  2.000000000e+00   1.0e+00  0.04  
1   1.7e+03  2.2e+03  8.9e+04  -9.71e-01  -1.216494472e+05  2.619367401e+00   7.3e-01  0.05  
2   8.8e+02  1.1e+03  4.7e+04  -9.59e-01  -1.193668588e+05  4.615079961e+00   3.8e-01  0.06  
3   2.9e+02  3.8e+02  1.5e+04  -9.22e-01  -1.103488376e+05  2.001954112e+01   1.3e-01  0.07  
4   2.9e+02  3.7e+02  1.5e+04  -7.70e-01  -1.080517227e+05  2.030288678e+03   1.3e-01  0.08  
5   1.2e+02  1.6e+02  6.4e+03  -7.60e-01  -8.691249091e+04  6.300042381e+03   5.3e-02  0.08  
6   3.3e+01  4.4e+01  1.8e+03  -4.48e-01  -4.076173705e+04  1.195352215e+04   1.5e-02  0.09  
7   2.0e+01  2.6e+01  1.1e+03  3.43e-01   -2.786822718e+04  7.429401555e+03   8.9e-03  0.10  
8   1.0e+01  1.3e+01  5.5e+02  5.95e-01   -1.543124716e+04  4.210800516e+03   4.6e-03  0.11  
9   3.8e+00  5.0e+00  2.0e+02  8.09e-01   -5.794203935e+03  1.901433143e+03   1.7e-03  0.12  
10  2.0e+00  2.7e+00  1.1e+02  9.51e-01   -2.950006101e+03  1.198522177e+03   9.1e-04  0.13  
11  8.4e-01  1.1e+00  4.6e+01  9.87e-01   -1.120062289e+03  6.297849203e+02   3.8e-04  0.13  
12  8.2e-01  1.1e+00  4.4e+01  9.56e-01   -1.104063312e+03  6.055348872e+02   3.7e-04  0.14  
13  5.2e-01  6.8e-01  2.8e+01  9.72e-01   -6.586925530e+02  4.339055833e+02   2.4e-04  0.15  
14  3.3e-01  4.4e-01  1.8e+01  1.00e+00   -3.420367133e+02  3.489387007e+02   1.5e-04  0.16  
15  1.1e-01  1.8e-01  6.4e+00  9.98e-01   -2.743178241e+01  2.173562659e+02   5.4e-05  0.17  
16  8.4e-02  1.3e-01  4.7e+00  1.02e+00   2.608518550e+01   2.049294771e+02   4.0e-05  0.17  
17  6.2e-02  9.8e-02  3.5e+00  1.02e+00   6.444236661e+01   1.967541398e+02   2.9e-05  0.18  
18  2.0e-02  8.0e-02  1.1e+00  1.02e+00   1.340709579e+02   1.769759093e+02   9.6e-06  0.19  
19  6.6e-03  1.7e-01  3.8e-01  1.01e+00   1.562513680e+02   1.703536155e+02   3.2e-06  0.20  
20  2.7e-03  2.1e-01  1.6e-01  1.01e+00   1.620619472e+02   1.679613977e+02   1.3e-06  0.21  
21  1.2e-03  1.2e-01  7.1e-02  1.01e+00   1.645571871e+02   1.672153103e+02   6.1e-07  0.21  
22  3.4e-04  1.2e-01  2.1e-02  1.01e+00   1.659288219e+02   1.667080189e+02   1.8e-07  0.22  
23  1.5e-04  1.0e-01  9.4e-03  1.01e+00   1.662327709e+02   1.665829207e+02   8.3e-08  0.23  
24  7.1e-05  8.5e-02  4.4e-03  1.01e+00   1.663630105e+02   1.665261053e+02   3.9e-08  0.24  
25  6.4e-05  7.7e-02  4.0e-03  1.01e+00   1.663764090e+02   1.665232521e+02   3.5e-08  0.25  
26  5.8e-05  7.0e-02  3.6e-03  1.01e+00   1.663863543e+02   1.665184592e+02   3.1e-08  0.25  
27  5.2e-05  6.4e-02  3.2e-03  1.01e+00   1.663954693e+02   1.665143316e+02   2.8e-08  0.26  
28  4.7e-05  5.8e-02  2.9e-03  1.01e+00   1.664036141e+02   1.665105620e+02   2.6e-08  0.27  
29  4.2e-05  5.3e-02  2.6e-03  1.01e+00   1.664109292e+02   1.665071595e+02   2.3e-08  0.28  
30  3.8e-05  4.9e-02  2.3e-03  1.01e+00   1.664174953e+02   1.665040837e+02   2.1e-08  0.29  
31  3.4e-05  4.5e-02  2.1e-03  1.01e+00   1.664233907e+02   1.665013049e+02   1.9e-08  0.29  
32  3.1e-05  4.1e-02  1.9e-03  1.01e+00   1.664286846e+02   1.664987947e+02   1.7e-08  0.30  
33  2.8e-05  3.8e-02  1.7e-03  1.00e+00   1.664334388e+02   1.664965276e+02   1.5e-08  0.31  
34  2.5e-05  3.5e-02  1.5e-03  1.00e+00   1.664377089e+02   1.664944805e+02   1.4e-08  0.32  
35  2.2e-05  3.2e-02  1.4e-03  1.00e+00   1.664415447e+02   1.664926323e+02   1.2e-08  0.32  
36  2.0e-05  3.0e-02  1.2e-03  1.00e+00   1.664449907e+02   1.664909640e+02   1.1e-08  0.33  
37  1.8e-05  2.8e-02  1.1e-03  1.00e+00   1.664480869e+02   1.664894583e+02   9.9e-09  0.34  
38  1.6e-05  2.6e-02  1.0e-03  1.00e+00   1.664508690e+02   1.664880997e+02   8.9e-09  0.35  
39  1.5e-05  2.4e-02  9.1e-04  1.00e+00   1.664533693e+02   1.664868740e+02   8.0e-09  0.36  
40  1.3e-05  2.2e-02  8.2e-04  1.00e+00   1.664556164e+02   1.664857684e+02   7.2e-09  0.37  
41  1.2e-05  2.1e-02  7.4e-04  1.00e+00   1.664576363e+02   1.664847712e+02   6.5e-09  0.37  
42  1.1e-05  2.0e-02  6.6e-04  1.00e+00   1.664594521e+02   1.664838720e+02   5.8e-09  0.38  
43  9.6e-06  1.8e-02  6.0e-04  1.00e+00   1.664610846e+02   1.664830613e+02   5.3e-09  0.39  
44  8.7e-06  1.7e-02  5.4e-04  1.00e+00   1.664625525e+02   1.664823305e+02   4.7e-09  0.40  
45  7.8e-06  1.6e-02  4.8e-04  1.00e+00   1.664638724e+02   1.664816719e+02   4.3e-09  0.41  
46  7.0e-06  1.6e-02  4.3e-04  1.00e+00   1.664650594e+02   1.664810783e+02   3.8e-09  0.42  
47  6.3e-06  1.5e-02  3.9e-04  1.00e+00   1.664661269e+02   1.664805435e+02   3.5e-09  0.42  
48  5.7e-06  1.4e-02  3.5e-04  1.00e+00   1.664670870e+02   1.664800616e+02   3.1e-09  0.43  
49  5.1e-06  1.3e-02  3.2e-04  1.00e+00   1.664679506e+02   1.664796275e+02   2.8e-09  0.44  
50  4.6e-06  1.3e-02  2.9e-04  1.00e+00   1.664687275e+02   1.664792364e+02   2.5e-09  0.45  
51  4.1e-06  1.2e-02  2.6e-04  1.00e+00   1.664694263e+02   1.664788842e+02   2.3e-09  0.46  
52  3.7e-06  1.2e-02  2.3e-04  1.00e+00   1.664700549e+02   1.664785668e+02   2.0e-09  0.46  
53  3.4e-06  1.2e-02  2.1e-04  1.00e+00   1.664706203e+02   1.664782810e+02   1.8e-09  0.47  
54  3.0e-06  1.1e-02  1.9e-04  1.00e+00   1.664711290e+02   1.664780235e+02   1.7e-09  0.48  
55  2.7e-06  1.1e-02  1.7e-04  1.00e+00   1.664715866e+02   1.664777916e+02   1.5e-09  0.49  
56  2.4e-06  1.1e-02  1.5e-04  1.00e+00   1.664719983e+02   1.664775828e+02   1.3e-09  0.50  
57  2.2e-06  1.0e-02  1.4e-04  1.00e+00   1.664723688e+02   1.664773948e+02   1.2e-09  0.50  
58  2.0e-06  1.0e-02  1.2e-04  1.00e+00   1.664727021e+02   1.664772255e+02   1.1e-09  0.51  
59  1.8e-06  9.8e-03  1.1e-04  1.00e+00   1.664730022e+02   1.664770732e+02   9.8e-10  0.52  
60  1.6e-06  9.6e-03  9.9e-05  1.00e+00   1.664732721e+02   1.664769360e+02   8.8e-10  0.53  
61  1.4e-06  9.4e-03  9.0e-05  1.00e+00   1.664735151e+02   1.664768126e+02   7.9e-10  0.54  
62  1.3e-06  9.3e-03  8.1e-05  1.00e+00   1.664737337e+02   1.664767015e+02   7.1e-10  0.55  
63  1.2e-06  9.1e-03  7.3e-05  1.00e+00   1.664739305e+02   1.664766015e+02   6.4e-10  0.55  
64  1.1e-06  9.0e-03  6.5e-05  1.00e+00   1.664741076e+02   1.664765115e+02   5.8e-10  0.56  
65  9.5e-07  8.9e-03  5.9e-05  1.00e+00   1.664742669e+02   1.664764304e+02   5.2e-10  0.57  
66  8.5e-07  8.8e-03  5.3e-05  1.00e+00   1.664744103e+02   1.664763575e+02   4.7e-10  0.58  
67  7.7e-07  8.7e-03  4.8e-05  1.00e+00   1.664745393e+02   1.664762918e+02   4.2e-10  0.58  
68  6.9e-07  8.6e-03  4.3e-05  1.00e+00   1.664746554e+02   1.664762326e+02   3.8e-10  0.59  
69  6.2e-07  8.5e-03  3.9e-05  1.00e+00   1.664747598e+02   1.664761793e+02   3.4e-10  0.60  
70  5.6e-07  8.4e-03  3.5e-05  1.00e+00   1.664748538e+02   1.664761313e+02   3.1e-10  0.61  
71  5.0e-07  8.4e-03  3.1e-05  1.00e+00   1.664749383e+02   1.664760881e+02   2.8e-10  0.62  
72  4.5e-07  8.3e-03  2.8e-05  1.00e+00   1.664750143e+02   1.664760492e+02   2.5e-10  0.62  
73  4.1e-07  8.3e-03  2.5e-05  1.00e+00   1.664750827e+02   1.664760141e+02   2.2e-10  0.63  
74  3.7e-07  8.2e-03  2.3e-05  1.00e+00   1.664751442e+02   1.664759824e+02   2.0e-10  0.64  
75  3.3e-07  8.2e-03  2.0e-05  1.00e+00   1.664751995e+02   1.664759540e+02   1.8e-10  0.65  
76  3.0e-07  8.1e-03  1.8e-05  1.00e+00   1.664752493e+02   1.664759283e+02   1.6e-10  0.66  
77  2.7e-07  8.1e-03  1.7e-05  1.00e+00   1.664752941e+02   1.664759052e+02   1.5e-10  0.67  
78  2.4e-07  8.1e-03  1.5e-05  1.00e+00   1.664753344e+02   1.664758844e+02   1.3e-10  0.67  
79  2.2e-07  8.0e-03  1.3e-05  1.00e+00   1.664753707e+02   1.664758656e+02   1.2e-10  0.68  
80  2.0e-07  8.0e-03  1.2e-05  1.00e+00   1.664754033e+02   1.664758488e+02   1.1e-10  0.69  
81  1.8e-07  8.0e-03  1.1e-05  1.00e+00   1.664754326e+02   1.664758336e+02   9.6e-11  0.70  
82  1.6e-07  7.9e-03  9.8e-06  1.00e+00   1.664754590e+02   1.664758199e+02   8.7e-11  0.71  
83  1.4e-07  7.9e-03  8.8e-06  1.00e+00   1.664754828e+02   1.664758076e+02   7.8e-11  0.72  
84  1.3e-07  7.9e-03  7.9e-06  1.00e+00   1.664755042e+02   1.664757965e+02   7.0e-11  0.72  
85  1.2e-07  7.9e-03  7.1e-06  1.00e+00   1.664755234e+02   1.664757865e+02   6.3e-11  0.73  
86  1.0e-07  7.8e-03  6.4e-06  1.00e+00   1.664755408e+02   1.664757775e+02   5.7e-11  0.75  
87  9.3e-08  7.8e-03  5.8e-06  1.00e+00   1.664755563e+02   1.664757694e+02   5.1e-11  0.76  
88  8.4e-08  7.8e-03  5.2e-06  9.99e-01   1.664755704e+02   1.664757622e+02   4.6e-11  0.76  
89  7.6e-08  7.8e-03  4.7e-06  1.00e+00   1.664755830e+02   1.664757556e+02   4.1e-11  0.77  
90  6.8e-08  7.8e-03  4.2e-06  9.97e-01   1.664755943e+02   1.664757497e+02   3.7e-11  0.78  
91  6.1e-08  7.8e-03  3.8e-06  1.00e+00   1.664756046e+02   1.664757444e+02   3.4e-11  0.79  
92  5.5e-08  7.7e-03  3.4e-06  9.99e-01   1.664756138e+02   1.664757396e+02   3.0e-11  0.80  
93  5.0e-08  7.7e-03  3.1e-06  1.00e+00   1.664756220e+02   1.664757353e+02   2.7e-11  0.80  
94  4.5e-08  7.7e-03  2.8e-06  1.00e+00   1.664756295e+02   1.664757314e+02   2.4e-11  0.81  
95  4.0e-08  7.7e-03  2.5e-06  1.00e+00   1.664756362e+02   1.664757279e+02   2.2e-11  0.82  
96  3.6e-08  7.7e-03  2.2e-06  1.00e+00   1.664756422e+02   1.664757248e+02   2.0e-11  0.83  
97  3.3e-08  7.7e-03  2.0e-06  1.00e+00   1.664756477e+02   1.664757220e+02   1.8e-11  0.84  
98  2.9e-08  7.7e-03  1.8e-06  1.00e+00   1.664756526e+02   1.664757194e+02   1.6e-11  0.85  
99  2.6e-08  7.7e-03  1.6e-06  1.00e+00   1.664756570e+02   1.664757171e+02   1.4e-11  0.86  
100 2.4e-08  7.6e-03  1.5e-06  1.00e+00   1.664756609e+02   1.664757151e+02   1.3e-11  0.87  
101 2.1e-08  7.6e-03  1.3e-06  1.00e+00   1.664756645e+02   1.664757132e+02   1.2e-11  0.88  
102 1.9e-08  7.6e-03  1.2e-06  1.00e+00   1.664756677e+02   1.664757116e+02   1.1e-11  0.89  
103 1.7e-08  7.6e-03  1.1e-06  9.94e-01   1.664756706e+02   1.664757101e+02   9.5e-12  0.89  
104 1.6e-08  6.8e-03  9.7e-07  1.00e+00   1.664756732e+02   1.664757087e+02   8.5e-12  0.90  
105 1.4e-08  6.2e-03  8.7e-07  1.01e+00   1.664756756e+02   1.664757075e+02   7.7e-12  0.91  
106 1.3e-08  5.5e-03  7.8e-07  1.00e+00   1.664756777e+02   1.664757064e+02   6.9e-12  0.92  
107 1.1e-08  5.0e-03  7.0e-07  1.00e+00   1.664756795e+02   1.664757054e+02   6.2e-12  0.93  
108 1.0e-08  4.5e-03  6.3e-07  9.95e-01   1.664756812e+02   1.664757045e+02   5.6e-12  0.93  
109 9.2e-09  4.0e-03  5.7e-07  1.01e+00   1.664756828e+02   1.664757037e+02   5.1e-12  0.94  
110 3.5e-09  4.1e-04  5.8e-08  9.98e-01   1.664756951e+02   1.664756973e+02   5.3e-13  0.95  
Optimizer terminated. Time: 0.95    

solsta = 1, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 1.6647569515e+02    nrm: 2e+01    Viol.  con: 1e-07    var: 0e+00  
  Dual.    obj: 1.6647569729e+02    nrm: 1e+03    Viol.  con: 0e+00    var: 3e-03  
* End solution on dual form. *
Transforming to primal solution.
Solving took 0.976 seconds.
Using solver 'mosek'
Solving for 1768 variables.
MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (313) of matrix 'A'.
MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (450) of matrix 'A'.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Problem
  Name                   :                 
  Objective sense        : max             
  Type                   : GECO (general convex optimization problem)
  Constraints            : 1769            
  Cones                  : 0               
  Scalar variables       : 6131            
  Matrix variables       : 0               
  Integer variables      : 0               

Optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Freed constraints in eliminator : 482
Eliminator terminated.
Eliminator started.
Freed constraints in eliminator : 6
Eliminator terminated.
Eliminator - tries                  : 2                 time                   : 0.00            
Lin. dep.  - tries                  : 1                 time                   : 0.00            
Lin. dep.  - number                 : 0               
Presolve terminated. Time: 0.01    
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Problem
  Name                   :                 
  Objective sense        : max             
  Type                   : GECO (general convex optimization problem)
  Constraints            : 1769            
  Cones                  : 0               
  Scalar variables       : 6131            
  Matrix variables       : 0               
  Integer variables      : 0               

Optimizer  - threads                : 8               
Optimizer  - solved problem         : the primal      
Optimizer  - Constraints            : 873
Optimizer  - Cones                  : 0
Optimizer  - Scalar variables       : 3462              conic                  : 0               
Optimizer  - Semi-definite variables: 0                 scalarized             : 0               
Factor     - setup time             : 0.02              dense det. time        : 0.00            
Factor     - ML order time          : 0.00              GP order time          : 0.01            
Factor     - nonzeros before factor : 1.49e+04          after factor           : 1.57e+05        
Factor     - dense dim.             : 0                 flops                  : 3.26e+07        
Factor     - GP saved nzs           : 3.37e+04          GP saved flops         : 9.34e+05        
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+03  3.0e+03  1.2e+05  0.00e+00   -1.223801642e+05  2.000000000e+00   1.0e+00  0.03  
1   1.7e+03  2.2e+03  8.9e+04  -9.71e-01  -1.216483304e+05  2.618565322e+00   7.3e-01  0.04  
2   8.8e+02  1.1e+03  4.7e+04  -9.59e-01  -1.193676752e+05  4.610922688e+00   3.8e-01  0.05  
3   2.9e+02  3.8e+02  1.5e+04  -9.22e-01  -1.103165945e+05  2.004323456e+01   1.3e-01  0.06  
4   2.9e+02  3.7e+02  1.5e+04  -7.70e-01  -1.080284782e+05  2.025515228e+03   1.3e-01  0.07  
5   1.2e+02  1.5e+02  6.3e+03  -7.60e-01  -8.689193228e+04  6.277145300e+03   5.2e-02  0.08  
6   2.9e+01  3.7e+01  1.5e+03  -4.47e-01  -3.555978381e+04  1.254685311e+04   1.3e-02  0.09  
7   1.8e+01  2.4e+01  9.7e+02  4.41e-01   -2.517278879e+04  7.242664304e+03   8.0e-03  0.09  
8   1.0e+01  1.3e+01  5.5e+02  6.44e-01   -1.529020587e+04  4.344385208e+03   4.5e-03  0.10  
9   3.9e+00  5.1e+00  2.1e+02  8.11e-01   -6.021009645e+03  1.946579789e+03   1.8e-03  0.11  
10  2.0e+00  2.6e+00  1.1e+02  9.48e-01   -2.964906920e+03  1.186949867e+03   9.1e-04  0.12  
11  8.4e-01  1.1e+00  4.6e+01  9.87e-01   -1.106052242e+03  6.319965104e+02   3.8e-04  0.13  
12  8.1e-01  1.1e+00  4.4e+01  9.51e-01   -1.097849102e+03  6.089590342e+02   3.7e-04  0.14  
13  5.2e-01  6.8e-01  2.8e+01  9.70e-01   -6.574957640e+02  4.370627639e+02   2.4e-04  0.14  
14  3.2e-01  4.3e-01  1.8e+01  1.00e+00   -3.348534794e+02  3.460902080e+02   1.5e-04  0.15  
15  1.1e-01  1.7e-01  6.2e+00  9.99e-01   -2.180331029e+01  2.157527514e+02   5.2e-05  0.16  
16  8.5e-02  1.3e-01  4.7e+00  1.02e+00   2.564071194e+01   2.060915714e+02   4.0e-05  0.17  
17  4.8e-02  9.3e-02  2.7e+00  1.02e+00   8.830023858e+01   1.901940651e+02   2.3e-05  0.18  
18  1.2e-02  1.7e-01  7.0e-01  1.02e+00   1.470192463e+02   1.734322407e+02   5.9e-06  0.18  
19  3.5e-03  2.1e-01  2.1e-01  1.01e+00   1.607382761e+02   1.684750030e+02   1.7e-06  0.19  
20  2.1e-03  2.2e-01  1.2e-01  1.00e+00   1.630800225e+02   1.676831725e+02   1.0e-06  0.20  
21  6.2e-04  1.5e-01  3.7e-02  1.01e+00   1.654579564e+02   1.668570066e+02   3.2e-07  0.21  
22  4.6e-04  1.2e-01  2.8e-02  9.95e-01   1.657162583e+02   1.667485014e+02   2.4e-07  0.22  
23  2.4e-04  8.3e-02  1.5e-02  9.83e-01   1.660592328e+02   1.666093529e+02   1.3e-07  0.24  
24  2.0e-04  7.0e-02  1.2e-02  1.00e+00   1.661253009e+02   1.665865316e+02   1.1e-07  0.25  
25  1.8e-04  6.4e-02  1.1e-02  1.01e+00   1.661586806e+02   1.665735495e+02   9.6e-08  0.26  
26  1.6e-04  5.9e-02  1.0e-02  1.01e+00   1.661875497e+02   1.665608333e+02   8.7e-08  0.27  
27  1.5e-04  5.3e-02  9.0e-03  1.01e+00   1.662136630e+02   1.665495611e+02   7.8e-08  0.28  
28  1.3e-04  4.9e-02  8.1e-03  1.00e+00   1.662370559e+02   1.665393192e+02   7.0e-08  0.29  
29  1.2e-04  4.5e-02  7.3e-03  1.00e+00   1.662580556e+02   1.665300572e+02   6.3e-08  0.30  
30  1.1e-04  4.1e-02  6.6e-03  1.00e+00   1.662769026e+02   1.665216766e+02   5.7e-08  0.30  
31  9.6e-05  3.8e-02  5.9e-03  1.00e+00   1.662938192e+02   1.665140945e+02   5.1e-08  0.31  
32  8.7e-05  3.5e-02  5.3e-03  1.00e+00   1.663090035e+02   1.665072347e+02   4.6e-08  0.32  
33  7.8e-05  3.2e-02  4.8e-03  1.00e+00   1.663226331e+02   1.665010285e+02   4.2e-08  0.33  
34  7.0e-05  3.0e-02  4.3e-03  1.00e+00   1.663348676e+02   1.664954137e+02   3.7e-08  0.33  
35  6.3e-05  2.7e-02  3.9e-03  1.00e+00   1.663458504e+02   1.664903343e+02   3.4e-08  0.34  
36  5.7e-05  2.5e-02  3.5e-03  1.00e+00   1.663557101e+02   1.664857397e+02   3.0e-08  0.35  
37  5.1e-05  2.4e-02  3.1e-03  1.00e+00   1.663645623e+02   1.664815845e+02   2.7e-08  0.36  
38  4.6e-05  2.2e-02  2.8e-03  1.00e+00   1.663725107e+02   1.664778272e+02   2.5e-08  0.37  
39  4.1e-05  2.1e-02  2.6e-03  1.00e+00   1.663796481e+02   1.664744304e+02   2.2e-08  0.37  
40  3.7e-05  1.9e-02  2.3e-03  1.00e+00   1.663860580e+02   1.664713600e+02   2.0e-08  0.38  
41  3.4e-05  1.8e-02  2.1e-03  1.00e+00   1.663918150e+02   1.664685853e+02   1.8e-08  0.39  
42  3.0e-05  1.7e-02  1.9e-03  1.00e+00   1.663969860e+02   1.664660781e+02   1.6e-08  0.40  
43  2.7e-05  1.6e-02  1.7e-03  1.00e+00   1.664016309e+02   1.664638129e+02   1.5e-08  0.40  
44  2.5e-05  1.5e-02  1.5e-03  1.00e+00   1.664058036e+02   1.664617668e+02   1.3e-08  0.41  
45  2.2e-05  1.5e-02  1.4e-03  1.00e+00   1.664095523e+02   1.664599187e+02   1.2e-08  0.42  
46  2.0e-05  1.4e-02  1.2e-03  1.00e+00   1.664129203e+02   1.664582497e+02   1.1e-08  0.43  
47  1.8e-05  1.3e-02  1.1e-03  1.00e+00   1.664159464e+02   1.664567427e+02   9.5e-09  0.44  
48  1.6e-05  1.3e-02  9.9e-04  1.00e+00   1.664186655e+02   1.664553820e+02   8.6e-09  0.45  
49  1.4e-05  1.2e-02  8.9e-04  1.00e+00   1.664211089e+02   1.664541537e+02   7.7e-09  0.46  
50  1.3e-05  1.2e-02  8.0e-04  1.00e+00   1.664233046e+02   1.664530450e+02   6.9e-09  0.46  
51  1.2e-05  1.1e-02  7.2e-04  1.00e+00   1.664252780e+02   1.664520443e+02   6.3e-09  0.47  
52  1.1e-05  1.1e-02  6.5e-04  1.00e+00   1.664270516e+02   1.664511413e+02   5.6e-09  0.48  
53  9.5e-06  1.1e-02  5.8e-04  1.00e+00   1.664286458e+02   1.664503266e+02   5.1e-09  0.49  
54  8.5e-06  1.1e-02  5.3e-04  1.00e+00   1.664300788e+02   1.664495916e+02   4.6e-09  0.50  
55  7.7e-06  1.0e-02  4.7e-04  1.00e+00   1.664313669e+02   1.664489285e+02   4.1e-09  0.50  
56  6.9e-06  1.0e-02  4.3e-04  1.00e+00   1.664325250e+02   1.664483305e+02   3.7e-09  0.51  
57  6.2e-06  9.9e-03  3.8e-04  1.00e+00   1.664335662e+02   1.664477912e+02   3.3e-09  0.52  
58  5.6e-06  9.7e-03  3.4e-04  1.00e+00   1.664345023e+02   1.664473049e+02   3.0e-09  0.53  
59  5.0e-06  9.5e-03  3.1e-04  1.00e+00   1.664353439e+02   1.664468664e+02   2.7e-09  0.53  
60  4.5e-06  9.4e-03  2.8e-04  1.00e+00   1.664361007e+02   1.664464710e+02   2.4e-09  0.54  
61  4.1e-06  9.2e-03  2.5e-04  1.00e+00   1.664367812e+02   1.664461145e+02   2.2e-09  0.55  
62  3.7e-06  9.1e-03  2.3e-04  1.00e+00   1.664373931e+02   1.664457931e+02   2.0e-09  0.56  
63  3.3e-06  9.0e-03  2.0e-04  1.00e+00   1.664379433e+02   1.664455033e+02   1.8e-09  0.57  
64  3.0e-06  8.9e-03  1.8e-04  1.00e+00   1.664384380e+02   1.664452421e+02   1.6e-09  0.58  
65  2.7e-06  8.8e-03  1.7e-04  1.00e+00   1.664388829e+02   1.664450067e+02   1.4e-09  0.59  
66  2.4e-06  8.7e-03  1.5e-04  1.00e+00   1.664392831e+02   1.664447945e+02   1.3e-09  0.59  
67  2.2e-06  8.6e-03  1.3e-04  1.00e+00   1.664396430e+02   1.664446034e+02   1.2e-09  0.60  
68  2.0e-06  8.6e-03  1.2e-04  1.00e+00   1.664399668e+02   1.664444312e+02   1.0e-09  0.61  
69  1.8e-06  8.5e-03  1.1e-04  1.00e+00   1.664402581e+02   1.664442761e+02   9.4e-10  0.62  
70  1.6e-06  8.4e-03  9.7e-05  1.00e+00   1.664405202e+02   1.664441363e+02   8.5e-10  0.63  
71  1.4e-06  8.4e-03  8.8e-05  1.00e+00   1.664407559e+02   1.664440105e+02   7.6e-10  0.63  
72  1.3e-06  8.3e-03  7.9e-05  1.00e+00   1.664409680e+02   1.664438972e+02   6.9e-10  0.64  
73  1.2e-06  8.3e-03  7.1e-05  1.00e+00   1.664411588e+02   1.664437951e+02   6.2e-10  0.65  
74  1.0e-06  8.2e-03  6.4e-05  1.00e+00   1.664413305e+02   1.664437031e+02   5.6e-10  0.66  
75  9.3e-07  8.2e-03  5.8e-05  1.00e+00   1.664414849e+02   1.664436203e+02   5.0e-10  0.67  
76  8.4e-07  8.1e-03  5.2e-05  1.00e+00   1.664416238e+02   1.664435457e+02   4.5e-10  0.67  
77  7.6e-07  8.1e-03  4.7e-05  1.00e+00   1.664417488e+02   1.664434785e+02   4.0e-10  0.68  
78  6.8e-07  8.1e-03  4.2e-05  1.00e+00   1.664418612e+02   1.664434180e+02   3.6e-10  0.69  
79  6.1e-07  8.0e-03  3.8e-05  1.00e+00   1.664419624e+02   1.664433635e+02   3.3e-10  0.70  
80  5.5e-07  8.0e-03  3.4e-05  1.00e+00   1.664420534e+02   1.664433144e+02   3.0e-10  0.71  
81  5.0e-07  8.0e-03  3.1e-05  1.00e+00   1.664421352e+02   1.664432702e+02   2.7e-10  0.72  
82  4.5e-07  7.9e-03  2.8e-05  1.00e+00   1.664422089e+02   1.664432303e+02   2.4e-10  0.72  
83  4.0e-07  7.9e-03  2.5e-05  1.00e+00   1.664422751e+02   1.664431944e+02   2.2e-10  0.73  
84  3.6e-07  7.9e-03  2.2e-05  1.00e+00   1.664423347e+02   1.664431621e+02   1.9e-10  0.74  
85  3.3e-07  7.9e-03  2.0e-05  1.00e+00   1.664423883e+02   1.664431330e+02   1.7e-10  0.75  
86  2.9e-07  7.8e-03  1.8e-05  1.00e+00   1.664424366e+02   1.664431067e+02   1.6e-10  0.76  
87  2.6e-07  7.8e-03  1.6e-05  1.00e+00   1.664424800e+02   1.664430831e+02   1.4e-10  0.77  
88  2.4e-07  7.8e-03  1.5e-05  1.00e+00   1.664425190e+02   1.664430619e+02   1.3e-10  0.77  
89  2.1e-07  7.8e-03  1.3e-05  1.00e+00   1.664425542e+02   1.664430428e+02   1.1e-10  0.78  
90  1.9e-07  7.8e-03  1.2e-05  1.00e+00   1.664425858e+02   1.664430256e+02   1.0e-10  0.79  
91  1.7e-07  7.8e-03  1.1e-05  1.00e+00   1.664426143e+02   1.664430101e+02   9.3e-11  0.80  
92  1.6e-07  7.7e-03  9.6e-06  1.00e+00   1.664426399e+02   1.664429961e+02   8.3e-11  0.81  
93  1.4e-07  7.7e-03  8.6e-06  1.00e+00   1.664426630e+02   1.664429836e+02   7.5e-11  0.82  
94  1.3e-07  7.7e-03  7.8e-06  1.00e+00   1.664426838e+02   1.664429723e+02   6.8e-11  0.82  
95  1.1e-07  7.7e-03  7.0e-06  1.00e+00   1.664427025e+02   1.664429622e+02   6.1e-11  0.83  
96  1.0e-07  7.7e-03  6.3e-06  1.00e+00   1.664427193e+02   1.664429530e+02   5.5e-11  0.84  
97  9.2e-08  7.7e-03  5.7e-06  1.00e+00   1.664427344e+02   1.664429448e+02   4.9e-11  0.85  
98  8.3e-08  7.7e-03  5.1e-06  9.99e-01   1.664427480e+02   1.664429374e+02   4.4e-11  0.86  
99  7.5e-08  7.6e-03  4.6e-06  1.00e+00   1.664427603e+02   1.664429307e+02   4.0e-11  0.87  
100 6.7e-08  7.6e-03  4.1e-06  1.00e+00   1.664427713e+02   1.664429247e+02   3.6e-11  0.87  
101 6.0e-08  7.6e-03  3.7e-06  1.00e+00   1.664427813e+02   1.664429193e+02   3.2e-11  0.88  
102 5.4e-08  7.6e-03  3.3e-06  9.98e-01   1.664427902e+02   1.664429145e+02   2.9e-11  0.89  
103 4.9e-08  7.6e-03  3.0e-06  1.00e+00   1.664427983e+02   1.664429101e+02   2.6e-11  0.90  
104 4.4e-08  7.6e-03  2.7e-06  1.00e+00   1.664428055e+02   1.664429062e+02   2.4e-11  0.91  
105 4.0e-08  7.6e-03  2.4e-06  1.00e+00   1.664428120e+02   1.664429026e+02   2.1e-11  0.92  
106 3.6e-08  7.6e-03  2.2e-06  1.00e+00   1.664428179e+02   1.664428994e+02   1.9e-11  0.92  
107 3.2e-08  7.6e-03  2.0e-06  9.97e-01   1.664428232e+02   1.664428966e+02   1.7e-11  0.93  
108 2.9e-08  7.6e-03  1.8e-06  9.99e-01   1.664428279e+02   1.664428940e+02   1.5e-11  0.94  
109 2.6e-08  7.5e-03  1.6e-06  9.96e-01   1.664428322e+02   1.664428917e+02   1.4e-11  0.95  
110 2.3e-08  7.5e-03  1.4e-06  9.98e-01   1.664428360e+02   1.664428896e+02   1.3e-11  0.95  
111 2.1e-08  6.8e-03  1.3e-06  1.00e+00   1.664428395e+02   1.664428877e+02   1.1e-11  0.96  
112 1.9e-08  6.1e-03  1.2e-06  9.97e-01   1.664428426e+02   1.664428860e+02   1.0e-11  0.97  
113 1.7e-08  5.5e-03  1.1e-06  1.00e+00   1.664428454e+02   1.664428845e+02   9.1e-12  0.98  
114 1.6e-08  4.9e-03  9.5e-07  1.00e+00   1.664428480e+02   1.664428831e+02   8.2e-12  0.99  
115 1.4e-08  4.4e-03  8.5e-07  1.01e+00   1.664428503e+02   1.664428818e+02   7.4e-12  0.99  
116 1.3e-08  4.0e-03  7.7e-07  1.00e+00   1.664428524e+02   1.664428807e+02   6.7e-12  1.00  
117 1.2e-08  4.0e-03  6.9e-07  9.96e-01   1.664428541e+02   1.664428800e+02   6.0e-12  1.01  
118 1.0e-08  3.6e-03  6.2e-07  9.92e-01   1.664428558e+02   1.664428791e+02   5.4e-12  1.02  
119 9.2e-09  3.2e-03  5.6e-07  1.02e+00   1.664428574e+02   1.664428781e+02   4.9e-12  1.02  
120 8.3e-09  2.9e-03  5.0e-07  9.88e-01   1.664428587e+02   1.664428774e+02   4.4e-12  1.03  
121 7.5e-09  2.6e-03  4.5e-07  1.02e+00   1.664428601e+02   1.664428766e+02   4.0e-12  1.04  
122 6.8e-09  2.3e-03  4.1e-07  9.75e-01   1.664428611e+02   1.664428760e+02   3.6e-12  1.05  
123 6.1e-09  2.1e-03  3.7e-07  1.02e+00   1.664428621e+02   1.664428755e+02   3.3e-12  1.06  
124 5.5e-09  1.9e-03  3.3e-07  9.96e-01   1.664428630e+02   1.664428750e+02   3.0e-12  1.07  
125 5.0e-09  1.7e-03  3.0e-07  1.00e+00   1.664428638e+02   1.664428746e+02   2.7e-12  1.07  
126 4.5e-09  1.5e-03  2.7e-07  9.84e-01   1.664428645e+02   1.664428742e+02   2.4e-12  1.08  
127 4.6e-08  1.5e-03  2.6e-07  9.86e-01   1.664428643e+02   1.664428750e+02   2.3e-12  1.09  
128 3.6e-08  1.4e-03  2.4e-07  1.06e+00   1.664428651e+02   1.664428743e+02   2.1e-12  1.10  
129 3.2e-08  1.2e-03  2.1e-07  9.94e-01   1.664428657e+02   1.664428740e+02   1.9e-12  1.10  
130 2.9e-08  1.1e-03  1.9e-07  1.03e+00   1.664428663e+02   1.664428736e+02   1.8e-12  1.11  
131 2.6e-08  9.9e-04  1.7e-07  9.43e-01   1.664428667e+02   1.664428733e+02   1.6e-12  1.12  
132 2.3e-08  8.9e-04  1.5e-07  1.01e+00   1.664428671e+02   1.664428731e+02   1.4e-12  1.13  
133 2.1e-08  8.0e-04  1.4e-07  1.02e+00   1.664428675e+02   1.664428728e+02   1.3e-12  1.13  
134 1.9e-08  7.2e-04  1.3e-07  1.01e+00   1.664428678e+02   1.664428726e+02   1.2e-12  1.14  
135 1.7e-08  6.5e-04  1.1e-07  9.86e-01   1.664428681e+02   1.664428724e+02   1.1e-12  1.15  
136 1.5e-08  5.8e-04  1.0e-07  9.94e-01   1.664428684e+02   1.664428722e+02   9.6e-13  1.16  
Optimizer terminated. Time: 1.16    

solsta = 1, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 1.6644286838e+02    nrm: 2e+01    Viol.  con: 4e-07    var: 0e+00  
  Dual.    obj: 1.6644287224e+02    nrm: 1e+03    Viol.  con: 0e+00    var: 4e-03  
* End solution on dual form. *
Transforming to primal solution.
Solving took 1.19 seconds.
Using solver 'mosek'
Solving for 1768 variables.
MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (312) of matrix 'A'.
MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (450) of matrix 'A'.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Problem
  Name                   :                 
  Objective sense        : max             
  Type                   : GECO (general convex optimization problem)
  Constraints            : 1769            
  Cones                  : 0               
  Scalar variables       : 6131            
  Matrix variables       : 0               
  Integer variables      : 0               

Optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Freed constraints in eliminator : 482
Eliminator terminated.
Eliminator started.
Freed constraints in eliminator : 6
Eliminator terminated.
Eliminator - tries                  : 2                 time                   : 0.00            
Lin. dep.  - tries                  : 1                 time                   : 0.00            
Lin. dep.  - number                 : 0               
Presolve terminated. Time: 0.01    
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Problem
  Name                   :                 
  Objective sense        : max             
  Type                   : GECO (general convex optimization problem)
  Constraints            : 1769            
  Cones                  : 0               
  Scalar variables       : 6131            
  Matrix variables       : 0               
  Integer variables      : 0               

Optimizer  - threads                : 8               
Optimizer  - solved problem         : the primal      
Optimizer  - Constraints            : 873
Optimizer  - Cones                  : 0
Optimizer  - Scalar variables       : 3462              conic                  : 0               
Optimizer  - Semi-definite variables: 0                 scalarized             : 0               
Factor     - setup time             : 0.02              dense det. time        : 0.00            
Factor     - ML order time          : 0.00              GP order time          : 0.01            
Factor     - nonzeros before factor : 1.49e+04          after factor           : 1.57e+05        
Factor     - dense dim.             : 0                 flops                  : 3.26e+07        
Factor     - GP saved nzs           : 3.37e+04          GP saved flops         : 9.34e+05        
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+03  3.0e+03  1.2e+05  0.00e+00   -1.223796803e+05  2.000000000e+00   1.0e+00  0.04  
1   1.7e+03  2.2e+03  8.9e+04  -9.71e-01  -1.216476084e+05  2.618554922e+00   7.3e-01  0.05  
2   8.8e+02  1.1e+03  4.7e+04  -9.59e-01  -1.193666125e+05  4.610537506e+00   3.8e-01  0.06  
3   2.9e+02  3.7e+02  1.5e+04  -9.22e-01  -1.102966097e+05  2.005786766e+01   1.3e-01  0.07  
4   2.9e+02  3.7e+02  1.5e+04  -7.69e-01  -1.080118792e+05  2.024242288e+03   1.3e-01  0.08  
5   1.2e+02  1.5e+02  6.3e+03  -7.60e-01  -8.686643901e+04  6.264842071e+03   5.2e-02  0.09  
6   2.7e+01  3.5e+01  1.5e+03  -4.47e-01  -3.361423875e+04  1.275613178e+04   1.2e-02  0.10  
7   1.7e+01  2.2e+01  9.2e+02  4.78e-01   -2.409624449e+04  7.121560004e+03   7.6e-03  0.11  
8   1.0e+01  1.3e+01  5.3e+02  6.63e-01   -1.491091001e+04  4.313499207e+03   4.4e-03  0.12  
9   3.8e+00  5.0e+00  2.1e+02  8.17e-01   -5.882084267e+03  1.917880415e+03   1.7e-03  0.12  
10  2.0e+00  2.6e+00  1.1e+02  9.49e-01   -2.856912142e+03  1.168394898e+03   8.8e-04  0.13  
11  8.4e-01  1.1e+00  4.6e+01  9.87e-01   -1.134284740e+03  6.217436659e+02   3.8e-04  0.14  
12  8.2e-01  1.1e+00  4.5e+01  9.52e-01   -1.122688405e+03  5.985078074e+02   3.7e-04  0.15  
13  5.2e-01  6.8e-01  2.8e+01  9.70e-01   -6.636991795e+02  4.331771302e+02   2.4e-04  0.16  
14  3.0e-01  4.1e-01  1.7e+01  1.00e+00   -3.097111699e+02  3.352546183e+02   1.4e-04  0.17  
15  1.1e-01  1.7e-01  5.9e+00  1.00e+00   -1.482958391e+01  2.136502396e+02   5.0e-05  0.18  
16  8.4e-02  1.3e-01  4.7e+00  1.02e+00   2.760730165e+01   2.071351104e+02   4.0e-05  0.19  
17  4.8e-02  9.4e-02  2.7e+00  1.02e+00   8.723176146e+01   1.898083063e+02   2.3e-05  0.20  
18  1.6e-02  9.0e-02  8.7e-01  1.02e+00   1.418963690e+02   1.747571509e+02   7.4e-06  0.21  
19  7.2e-03  7.0e-02  4.1e-01  1.01e+00   1.546961115e+02   1.700499165e+02   3.5e-06  0.21  
20  1.7e-03  1.6e-01  1.0e-01  1.01e+00   1.636916571e+02   1.675254609e+02   8.6e-07  0.22  
21  1.0e-03  1.1e-01  6.3e-02  9.76e-01   1.647504813e+02   1.670947428e+02   5.3e-07  0.23  
22  3.5e-04  1.2e-01  2.2e-02  9.86e-01   1.658617377e+02   1.666773466e+02   1.9e-07  0.24  
23  1.6e-04  9.6e-02  1.0e-02  1.00e+00   1.661549018e+02   1.665439119e+02   9.0e-08  0.25  
24  6.2e-05  9.2e-02  4.0e-03  1.01e+00   1.663208740e+02   1.664687668e+02   3.5e-08  0.26  
25  3.0e-05  7.9e-02  1.9e-03  1.01e+00   1.663730748e+02   1.664449304e+02   1.7e-08  0.27  
26  2.7e-05  7.3e-02  1.7e-03  1.01e+00   1.663788267e+02   1.664435430e+02   1.5e-08  0.27  
27  2.4e-05  6.6e-02  1.6e-03  1.01e+00   1.663831112e+02   1.664413337e+02   1.4e-08  0.28  
28  2.2e-05  6.0e-02  1.4e-03  1.01e+00   1.663870609e+02   1.664394512e+02   1.2e-08  0.29  
29  2.0e-05  5.5e-02  1.3e-03  1.01e+00   1.663905952e+02   1.664377370e+02   1.1e-08  0.30  
30  1.8e-05  5.0e-02  1.1e-03  1.00e+00   1.663937727e+02   1.664361929e+02   1.0e-08  0.31  
31  1.6e-05  4.6e-02  1.0e-03  1.00e+00   1.663966270e+02   1.664347990e+02   9.0e-09  0.32  
32  1.4e-05  4.2e-02  9.2e-04  1.00e+00   1.663991915e+02   1.664335414e+02   8.1e-09  0.32  
33  1.3e-05  3.9e-02  8.3e-04  1.00e+00   1.664014960e+02   1.664324068e+02   7.3e-09  0.33  
34  1.2e-05  3.6e-02  7.5e-04  1.00e+00   1.664035668e+02   1.664313834e+02   6.6e-09  0.34  
35  1.0e-05  3.3e-02  6.7e-04  1.00e+00   1.664054279e+02   1.664304602e+02   5.9e-09  0.35  
36  9.4e-06  3.1e-02  6.1e-04  1.00e+00   1.664071006e+02   1.664296277e+02   5.3e-09  0.35  
37  8.5e-06  2.8e-02  5.5e-04  1.00e+00   1.664086041e+02   1.664288769e+02   4.8e-09  0.36  
38  7.6e-06  2.6e-02  4.9e-04  1.00e+00   1.664099557e+02   1.664281999e+02   4.3e-09  0.37  
39  6.9e-06  2.4e-02  4.4e-04  1.00e+00   1.664111708e+02   1.664275896e+02   3.9e-09  0.38  
40  6.2e-06  2.3e-02  4.0e-04  1.00e+00   1.664122633e+02   1.664270395e+02   3.5e-09  0.39  
41  5.6e-06  2.1e-02  3.6e-04  1.00e+00   1.664132456e+02   1.664265435e+02   3.1e-09  0.40  
42  5.0e-06  2.0e-02  3.2e-04  1.00e+00   1.664141289e+02   1.664260966e+02   2.8e-09  0.41  
43  4.5e-06  1.9e-02  2.9e-04  1.00e+00   1.664149231e+02   1.664256937e+02   2.5e-09  0.41  
44  4.1e-06  1.8e-02  2.6e-04  1.00e+00   1.664156374e+02   1.664253307e+02   2.3e-09  0.42  
45  3.7e-06  1.7e-02  2.4e-04  1.00e+00   1.664162797e+02   1.664250035e+02   2.1e-09  0.43  
46  3.3e-06  1.6e-02  2.1e-04  1.00e+00   1.664168573e+02   1.664247086e+02   1.9e-09  0.43  
47  3.0e-06  1.5e-02  1.9e-04  1.00e+00   1.664173768e+02   1.664244429e+02   1.7e-09  0.45  
48  2.7e-06  1.4e-02  1.7e-04  1.00e+00   1.664178440e+02   1.664242034e+02   1.5e-09  0.45  
49  2.4e-06  1.4e-02  1.5e-04  1.00e+00   1.664182643e+02   1.664239877e+02   1.4e-09  0.46  
50  2.2e-06  1.3e-02  1.4e-04  1.00e+00   1.664186423e+02   1.664237934e+02   1.2e-09  0.47  
51  1.9e-06  1.3e-02  1.2e-04  1.00e+00   1.664189825e+02   1.664236185e+02   1.1e-09  0.48  
52  1.7e-06  1.2e-02  1.1e-04  1.00e+00   1.664192885e+02   1.664234609e+02   9.8e-10  0.49  
53  1.6e-06  1.2e-02  1.0e-04  1.00e+00   1.664195638e+02   1.664233190e+02   8.9e-10  0.50  
54  1.4e-06  1.1e-02  9.1e-05  1.00e+00   1.664198115e+02   1.664231912e+02   8.0e-10  0.51  
55  1.3e-06  1.1e-02  8.2e-05  1.00e+00   1.664200344e+02   1.664230761e+02   7.2e-10  0.52  
56  1.1e-06  1.1e-02  7.4e-05  1.00e+00   1.664202349e+02   1.664229724e+02   6.5e-10  0.52  
57  1.0e-06  1.0e-02  6.6e-05  1.00e+00   1.664204153e+02   1.664228791e+02   5.8e-10  0.53  
58  9.3e-07  1.0e-02  6.0e-05  1.00e+00   1.664205776e+02   1.664227951e+02   5.2e-10  0.54  
59  8.4e-07  9.9e-03  5.4e-05  1.00e+00   1.664207236e+02   1.664227194e+02   4.7e-10  0.55  
60  7.5e-07  9.7e-03  4.8e-05  1.00e+00   1.664208550e+02   1.664226512e+02   4.2e-10  0.55  
61  6.8e-07  9.5e-03  4.4e-05  1.00e+00   1.664209732e+02   1.664225898e+02   3.8e-10  0.56  
62  6.1e-07  9.3e-03  3.9e-05  1.00e+00   1.664210796e+02   1.664225345e+02   3.4e-10  0.57  
63  5.5e-07  9.2e-03  3.5e-05  1.00e+00   1.664211752e+02   1.664224847e+02   3.1e-10  0.58  
64  4.9e-07  9.0e-03  3.2e-05  1.00e+00   1.664212613e+02   1.664224398e+02   2.8e-10  0.58  
65  4.4e-07  8.9e-03  2.9e-05  1.00e+00   1.664213387e+02   1.664223994e+02   2.5e-10  0.59  
66  4.0e-07  8.8e-03  2.6e-05  1.00e+00   1.664214083e+02   1.664223629e+02   2.3e-10  0.61  
67  3.6e-07  8.7e-03  2.3e-05  1.00e+00   1.664214710e+02   1.664223301e+02   2.0e-10  0.62  
68  3.2e-07  8.6e-03  2.1e-05  1.00e+00   1.664215273e+02   1.664223006e+02   1.8e-10  0.63  
69  2.9e-07  8.5e-03  1.9e-05  1.00e+00   1.664215780e+02   1.664222740e+02   1.6e-10  0.64  
70  2.6e-07  8.4e-03  1.7e-05  1.00e+00   1.664216237e+02   1.664222500e+02   1.5e-10  0.65  
71  2.4e-07  8.4e-03  1.5e-05  1.00e+00   1.664216647e+02   1.664222284e+02   1.3e-10  0.66  
72  2.1e-07  8.3e-03  1.4e-05  1.00e+00   1.664217017e+02   1.664222090e+02   1.2e-10  0.67  
73  1.9e-07  8.2e-03  1.2e-05  1.00e+00   1.664217349e+02   1.664221915e+02   1.1e-10  0.68  
74  1.7e-07  8.2e-03  1.1e-05  1.00e+00   1.664217648e+02   1.664221758e+02   9.7e-11  0.69  
75  1.5e-07  8.1e-03  1.0e-05  1.00e+00   1.664217917e+02   1.664221616e+02   8.7e-11  0.70  
76  1.4e-07  8.1e-03  9.0e-06  9.99e-01   1.664218160e+02   1.664221488e+02   7.9e-11  0.71  
77  1.3e-07  8.0e-03  8.1e-06  1.00e+00   1.664218378e+02   1.664221373e+02   7.1e-11  0.72  
78  1.1e-07  8.0e-03  7.3e-06  1.00e+00   1.664218574e+02   1.664221270e+02   6.4e-11  0.73  
79  1.0e-07  8.0e-03  6.5e-06  1.00e+00   1.664218750e+02   1.664221177e+02   5.7e-11  0.74  
80  9.1e-08  7.9e-03  5.9e-06  1.00e+00   1.664218909e+02   1.664221093e+02   5.2e-11  0.75  
81  8.2e-08  7.9e-03  5.3e-06  1.00e+00   1.664219052e+02   1.664221018e+02   4.6e-11  0.76  
82  7.4e-08  7.9e-03  4.8e-06  9.99e-01   1.664219181e+02   1.664220950e+02   4.2e-11  0.77  
83  6.7e-08  7.9e-03  4.3e-06  1.00e+00   1.664219297e+02   1.664220889e+02   3.8e-11  0.78  
84  6.0e-08  7.8e-03  3.9e-06  9.99e-01   1.664219401e+02   1.664220834e+02   3.4e-11  0.79  
85  5.4e-08  7.8e-03  3.5e-06  1.00e+00   1.664219495e+02   1.664220784e+02   3.0e-11  0.80  
86  4.9e-08  7.8e-03  3.1e-06  9.99e-01   1.664219579e+02   1.664220740e+02   2.7e-11  0.81  
87  4.4e-08  7.8e-03  2.8e-06  9.99e-01   1.664219655e+02   1.664220700e+02   2.5e-11  0.82  
88  3.9e-08  7.7e-03  2.5e-06  1.00e+00   1.664219723e+02   1.664220664e+02   2.2e-11  0.83  
89  3.5e-08  7.7e-03  2.3e-06  1.00e+00   1.664219785e+02   1.664220631e+02   2.0e-11  0.84  
90  3.2e-08  7.7e-03  2.1e-06  1.00e+00   1.664219840e+02   1.664220602e+02   1.8e-11  0.85  
91  2.9e-08  7.7e-03  1.8e-06  1.00e+00   1.664219890e+02   1.664220576e+02   1.6e-11  0.86  
92  2.6e-08  7.7e-03  1.7e-06  1.00e+00   1.664219935e+02   1.664220552e+02   1.5e-11  0.88  
93  2.3e-08  7.7e-03  1.5e-06  9.99e-01   1.664219975e+02   1.664220531e+02   1.3e-11  0.88  
94  2.1e-08  7.6e-03  1.3e-06  9.98e-01   1.664220012e+02   1.664220511e+02   1.2e-11  0.89  
95  1.9e-08  7.6e-03  1.2e-06  1.00e+00   1.664220044e+02   1.664220494e+02   1.1e-11  0.90  
96  1.7e-08  7.6e-03  1.1e-06  1.00e+00   1.664220074e+02   1.664220479e+02   9.6e-12  0.92  
97  1.5e-08  7.6e-03  9.8e-07  1.00e+00   1.664220100e+02   1.664220465e+02   8.6e-12  0.93  
98  1.4e-08  7.6e-03  8.8e-07  1.00e+00   1.664220124e+02   1.664220452e+02   7.8e-12  0.93  
99  1.3e-08  6.8e-03  8.0e-07  1.01e+00   1.664220146e+02   1.664220441e+02   7.0e-12  0.94  
100 1.1e-08  6.1e-03  7.2e-07  1.00e+00   1.664220165e+02   1.664220430e+02   6.3e-12  0.96  
101 1.0e-08  5.5e-03  6.4e-07  9.99e-01   1.664220183e+02   1.664220421e+02   5.7e-12  0.97  
102 9.1e-09  5.0e-03  5.8e-07  9.95e-01   1.664220198e+02   1.664220413e+02   5.1e-12  0.98  
103 8.2e-09  4.5e-03  5.2e-07  1.00e+00   1.664220212e+02   1.664220406e+02   4.6e-12  0.99  
104 7.4e-09  4.0e-03  4.7e-07  1.00e+00   1.664220225e+02   1.664220399e+02   4.1e-12  1.00  
105 1.5e-08  3.7e-03  4.2e-07  9.00e-01   1.664220234e+02   1.664220402e+02   3.7e-12  1.01  
106 1.7e-08  3.4e-03  3.8e-07  9.02e-01   1.664220242e+02   1.664220413e+02   3.3e-12  1.02  
107 1.3e-08  3.0e-03  3.4e-07  1.00e+00   1.664220252e+02   1.664220407e+02   3.0e-12  1.03  
108 1.2e-08  2.7e-03  3.1e-07  1.02e+00   1.664220261e+02   1.664220399e+02   2.7e-12  1.04  
109 1.1e-08  2.5e-03  2.8e-07  1.00e+00   1.664220269e+02   1.664220393e+02   2.5e-12  1.05  
110 1.0e-08  2.2e-03  2.5e-07  1.01e+00   1.664220276e+02   1.664220388e+02   2.2e-12  1.06  
111 1.1e-08  2.0e-03  2.2e-07  8.59e-01   1.664220282e+02   1.664220388e+02   2.0e-12  1.08  
112 9.5e-09  1.8e-03  2.0e-07  1.00e+00   1.664220288e+02   1.664220383e+02   1.8e-12  1.09  
113 8.6e-09  1.6e-03  1.8e-07  1.00e+00   1.664220293e+02   1.664220379e+02   1.6e-12  1.10  
114 7.8e-09  1.5e-03  1.6e-07  1.00e+00   1.664220298e+02   1.664220375e+02   1.5e-12  1.11  
115 7.0e-09  1.3e-03  1.5e-07  9.96e-01   1.664220302e+02   1.664220371e+02   1.3e-12  1.12  
116 6.3e-09  1.2e-03  1.3e-07  1.00e+00   1.664220305e+02   1.664220368e+02   1.2e-12  1.13  
117 5.7e-09  1.1e-03  1.2e-07  9.97e-01   1.664220309e+02   1.664220365e+02   1.1e-12  1.15  
118 5.2e-09  9.7e-04  1.1e-07  1.00e+00   1.664220312e+02   1.664220363e+02   9.7e-13  1.16  
Optimizer terminated. Time: 1.16    

solsta = 1, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 1.6642203117e+02    nrm: 2e+01    Viol.  con: 1e-07    var: 0e+00  
  Dual.    obj: 1.6642203625e+02    nrm: 1e+03    Viol.  con: 0e+00    var: 9e-03  
* End solution on dual form. *
Transforming to primal solution.
Solving took 1.19 seconds.
Using solver 'mosek'
Solving for 1768 variables.
MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (313) of matrix 'A'.
MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (450) of matrix 'A'.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Problem
  Name                   :                 
  Objective sense        : max             
  Type                   : GECO (general convex optimization problem)
  Constraints            : 1769            
  Cones                  : 0               
  Scalar variables       : 6131            
  Matrix variables       : 0               
  Integer variables      : 0               

Optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Freed constraints in eliminator : 482
Eliminator terminated.
Eliminator started.
Freed constraints in eliminator : 6
Eliminator terminated.
Eliminator - tries                  : 2                 time                   : 0.00            
Lin. dep.  - tries                  : 1                 time                   : 0.00            
Lin. dep.  - number                 : 0               
Presolve terminated. Time: 0.02    
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Problem
  Name                   :                 
  Objective sense        : max             
  Type                   : GECO (general convex optimization problem)
  Constraints            : 1769            
  Cones                  : 0               
  Scalar variables       : 6131            
  Matrix variables       : 0               
  Integer variables      : 0               

Optimizer  - threads                : 8               
Optimizer  - solved problem         : the primal      
Optimizer  - Constraints            : 873
Optimizer  - Cones                  : 0
Optimizer  - Scalar variables       : 3462              conic                  : 0               
Optimizer  - Semi-definite variables: 0                 scalarized             : 0               
Factor     - setup time             : 0.03              dense det. time        : 0.00            
Factor     - ML order time          : 0.00              GP order time          : 0.02            
Factor     - nonzeros before factor : 1.49e+04          after factor           : 1.57e+05        
Factor     - dense dim.             : 0                 flops                  : 3.26e+07        
Factor     - GP saved nzs           : 3.37e+04          GP saved flops         : 9.34e+05        
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+03  3.0e+03  1.2e+05  0.00e+00   -1.223788450e+05  2.000000000e+00   1.0e+00  0.05  
1   1.7e+03  2.2e+03  8.9e+04  -9.71e-01  -1.216464201e+05  2.618823612e+00   7.3e-01  0.06  
2   8.8e+02  1.1e+03  4.7e+04  -9.59e-01  -1.193651315e+05  4.610867248e+00   3.8e-01  0.07  
3   2.9e+02  3.7e+02  1.5e+04  -9.22e-01  -1.102819975e+05  2.006632579e+01   1.3e-01  0.08  
4   2.9e+02  3.7e+02  1.5e+04  -7.69e-01  -1.080008064e+05  2.022086612e+03   1.3e-01  0.09  
5   1.2e+02  1.5e+02  6.3e+03  -7.59e-01  -8.679764001e+04  6.271578903e+03   5.2e-02  0.10  
6   2.7e+01  3.5e+01  1.4e+03  -4.46e-01  -3.331156973e+04  1.276898522e+04   1.2e-02  0.11  
7   1.7e+01  2.2e+01  9.1e+02  4.84e-01   -2.390955460e+04  7.088701501e+03   7.6e-03  0.12  
8   9.9e+00  1.3e+01  5.3e+02  6.66e-01   -1.478698502e+04  4.288484843e+03   4.4e-03  0.14  
9   3.8e+00  4.9e+00  2.0e+02  8.19e-01   -5.783602810e+03  1.894120710e+03   1.7e-03  0.15  
10  1.9e+00  2.5e+00  1.0e+02  9.50e-01   -2.752723046e+03  1.147878748e+03   8.5e-04  0.16  
11  8.6e-01  1.1e+00  4.7e+01  9.88e-01   -1.163553864e+03  6.311053338e+02   3.9e-04  0.17  
12  8.3e-01  1.1e+00  4.5e+01  9.53e-01   -1.146181136e+03  6.056748478e+02   3.8e-04  0.18  
13  5.2e-01  6.8e-01  2.8e+01  9.71e-01   -6.643878606e+02  4.338683157e+02   2.4e-04  0.20  
14  3.0e-01  4.0e-01  1.6e+01  1.00e+00   -3.001695787e+02  3.312568167e+02   1.4e-04  0.21  
15  1.0e-01  1.6e-01  5.8e+00  1.00e+00   -1.111857075e+01  2.124409044e+02   4.9e-05  0.22  
16  8.3e-02  1.3e-01  4.6e+00  1.02e+00   2.954416115e+01   2.070652180e+02   3.9e-05  0.23  
17  4.6e-02  9.2e-02  2.6e+00  1.02e+00   9.054315273e+01   1.887141196e+02   2.2e-05  0.24  
18  1.2e-02  1.7e-01  6.8e-01  1.02e+00   1.474804520e+02   1.732840791e+02   5.8e-06  0.25  
19  4.0e-03  1.9e-01  2.3e-01  1.01e+00   1.599979590e+02   1.685737685e+02   1.9e-06  0.26  
20  1.6e-03  1.1e-01  9.4e-02  1.01e+00   1.638684180e+02   1.673751081e+02   8.0e-07  0.27  
21  6.4e-04  9.4e-02  3.8e-02  1.01e+00   1.653872518e+02   1.668180858e+02   3.3e-07  0.29  
22  2.4e-04  9.6e-02  1.4e-02  1.01e+00   1.660337135e+02   1.665706256e+02   1.3e-07  0.30  
23  9.1e-05  9.3e-02  5.6e-03  1.01e+00   1.662643767e+02   1.664734884e+02   5.0e-08  0.31  
24  8.2e-05  8.5e-02  5.1e-03  1.01e+00   1.662801856e+02   1.664683641e+02   4.5e-08  0.32  
25  7.4e-05  7.7e-02  4.6e-03  1.01e+00   1.662931282e+02   1.664624192e+02   4.0e-08  0.33  
26  6.7e-05  7.0e-02  4.1e-03  1.01e+00   1.663048697e+02   1.664571799e+02   3.6e-08  0.34  
27  6.0e-05  6.4e-02  3.7e-03  1.01e+00   1.663153795e+02   1.664524151e+02   3.3e-08  0.35  
28  5.4e-05  5.8e-02  3.3e-03  1.01e+00   1.663248144e+02   1.664481107e+02   2.9e-08  0.36  
29  4.8e-05  5.3e-02  3.0e-03  1.01e+00   1.663332809e+02   1.664442181e+02   2.6e-08  0.37  
30  4.4e-05  4.9e-02  2.7e-03  1.01e+00   1.663408801e+02   1.664406994e+02   2.4e-08  0.38  
31  3.9e-05  4.5e-02  2.4e-03  1.01e+00   1.663477017e+02   1.664375192e+02   2.1e-08  0.40  
32  3.5e-05  4.1e-02  2.2e-03  1.01e+00   1.663538259e+02   1.664346455e+02   1.9e-08  0.40  
33  3.2e-05  3.8e-02  2.0e-03  1.01e+00   1.663593248e+02   1.664320492e+02   1.7e-08  0.41  
34  2.9e-05  3.5e-02  1.8e-03  1.00e+00   1.663642629e+02   1.664297041e+02   1.6e-08  0.42  
35  2.6e-05  3.2e-02  1.6e-03  1.00e+00   1.663686978e+02   1.664275861e+02   1.4e-08  0.44  
36  2.3e-05  3.0e-02  1.4e-03  1.00e+00   1.663726813e+02   1.664256736e+02   1.3e-08  0.45  
37  2.1e-05  2.8e-02  1.3e-03  1.00e+00   1.663762595e+02   1.664239469e+02   1.1e-08  0.46  
38  1.9e-05  2.6e-02  1.2e-03  1.00e+00   1.663794741e+02   1.664223881e+02   1.0e-08  0.47  
39  1.7e-05  2.4e-02  1.0e-03  1.00e+00   1.663823623e+02   1.664209811e+02   9.2e-09  0.48  
40  1.5e-05  2.2e-02  9.4e-04  1.00e+00   1.663849573e+02   1.664197112e+02   8.3e-09  0.49  
41  1.4e-05  2.1e-02  8.5e-04  1.00e+00   1.663872893e+02   1.664185653e+02   7.5e-09  0.51  
42  1.2e-05  2.0e-02  7.6e-04  1.00e+00   1.663893850e+02   1.664175315e+02   6.7e-09  0.52  
43  1.1e-05  1.8e-02  6.9e-04  1.00e+00   1.663912685e+02   1.664165987e+02   6.0e-09  0.53  
44  1.0e-05  1.7e-02  6.2e-04  1.00e+00   1.663929614e+02   1.664157574e+02   5.4e-09  0.54  
45  9.0e-06  1.7e-02  5.6e-04  1.00e+00   1.663944832e+02   1.664149986e+02   4.9e-09  0.55  
46  8.1e-06  1.6e-02  5.0e-04  1.00e+00   1.663958513e+02   1.664143143e+02   4.4e-09  0.56  
47  7.3e-06  1.5e-02  4.5e-04  1.00e+00   1.663970812e+02   1.664136972e+02   4.0e-09  0.57  
48  6.5e-06  1.4e-02  4.1e-04  1.00e+00   1.663981870e+02   1.664131409e+02   3.6e-09  0.58  
49  5.9e-06  1.4e-02  3.7e-04  1.00e+00   1.663991812e+02   1.664126394e+02   3.2e-09  0.59  
50  5.3e-06  1.3e-02  3.3e-04  1.00e+00   1.664000753e+02   1.664121873e+02   2.9e-09  0.60  
51  4.8e-06  1.3e-02  3.0e-04  1.00e+00   1.664008792e+02   1.664117798e+02   2.6e-09  0.61  
52  4.3e-06  1.2e-02  2.7e-04  1.00e+00   1.664016021e+02   1.664114125e+02   2.3e-09  0.62  
53  3.9e-06  1.2e-02  2.4e-04  1.00e+00   1.664022522e+02   1.664110814e+02   2.1e-09  0.63  
54  3.5e-06  1.1e-02  2.2e-04  1.00e+00   1.664028368e+02   1.664107829e+02   1.9e-09  0.64  
55  3.1e-06  1.1e-02  1.9e-04  1.00e+00   1.664033625e+02   1.664105139e+02   1.7e-09  0.65  
56  2.8e-06  1.1e-02  1.7e-04  1.00e+00   1.664038353e+02   1.664102715e+02   1.5e-09  0.67  
57  2.5e-06  1.1e-02  1.6e-04  1.00e+00   1.664042606e+02   1.664100531e+02   1.4e-09  0.68  
58  2.3e-06  1.0e-02  1.4e-04  1.00e+00   1.664046431e+02   1.664098564e+02   1.2e-09  0.69  
59  2.1e-06  1.0e-02  1.3e-04  1.00e+00   1.664049873e+02   1.664096792e+02   1.1e-09  0.71  
60  1.8e-06  9.8e-03  1.1e-04  1.00e+00   1.664052969e+02   1.664095196e+02   1.0e-09  0.72  
61  1.7e-06  9.7e-03  1.0e-04  1.00e+00   1.664055754e+02   1.664093758e+02   9.1e-10  0.73  
62  1.5e-06  9.5e-03  9.3e-05  1.00e+00   1.664058260e+02   1.664092464e+02   8.2e-10  0.74  
63  1.3e-06  9.3e-03  8.4e-05  1.00e+00   1.664060515e+02   1.664091298e+02   7.4e-10  0.75  
64  1.2e-06  9.2e-03  7.5e-05  1.00e+00   1.664062543e+02   1.664090248e+02   6.6e-10  0.76  
65  1.1e-06  9.1e-03  6.8e-05  1.00e+00   1.664064368e+02   1.664089302e+02   6.0e-10  0.77  
66  9.8e-07  9.0e-03  6.1e-05  1.00e+00   1.664066010e+02   1.664088451e+02   5.4e-10  0.78  
67  8.8e-07  8.9e-03  5.5e-05  1.00e+00   1.664067487e+02   1.664087684e+02   4.8e-10  0.80  
68  8.0e-07  8.8e-03  4.9e-05  1.00e+00   1.664068816e+02   1.664086993e+02   4.3e-10  0.80  
69  7.2e-07  8.7e-03  4.4e-05  1.00e+00   1.664070012e+02   1.664086371e+02   3.9e-10  0.81  
70  6.4e-07  8.6e-03  4.0e-05  1.00e+00   1.664071087e+02   1.664085811e+02   3.5e-10  0.82  
71  5.8e-07  8.5e-03  3.6e-05  1.00e+00   1.664072054e+02   1.664085306e+02   3.2e-10  0.83  
72  5.2e-07  8.5e-03  3.2e-05  1.00e+00   1.664072925e+02   1.664084851e+02   2.9e-10  0.85  
73  4.7e-07  8.4e-03  2.9e-05  1.00e+00   1.664073707e+02   1.664084441e+02   2.6e-10  0.85  
74  4.2e-07  8.3e-03  2.6e-05  1.00e+00   1.664074411e+02   1.664084072e+02   2.3e-10  0.86  
75  3.8e-07  8.3e-03  2.4e-05  1.00e+00   1.664075045e+02   1.664083739e+02   2.1e-10  0.87  
76  3.4e-07  8.2e-03  2.1e-05  1.00e+00   1.664075614e+02   1.664083439e+02   1.9e-10  0.88  
77  3.1e-07  8.2e-03  1.9e-05  1.00e+00   1.664076127e+02   1.664083169e+02   1.7e-10  0.89  
78  2.8e-07  8.1e-03  1.7e-05  1.00e+00   1.664076588e+02   1.664082926e+02   1.5e-10  0.90  
79  2.5e-07  8.1e-03  1.5e-05  1.00e+00   1.664077003e+02   1.664082707e+02   1.4e-10  0.91  
80  2.2e-07  8.1e-03  1.4e-05  1.00e+00   1.664077376e+02   1.664082510e+02   1.2e-10  0.92  
81  2.0e-07  8.0e-03  1.3e-05  1.00e+00   1.664077712e+02   1.664082333e+02   1.1e-10  0.93  
82  1.8e-07  8.0e-03  1.1e-05  1.00e+00   1.664078015e+02   1.664082173e+02   9.9e-11  0.93  
83  1.6e-07  8.0e-03  1.0e-05  1.00e+00   1.664078287e+02   1.664082029e+02   9.0e-11  0.95  
84  1.5e-07  8.0e-03  9.2e-06  1.00e+00   1.664078531e+02   1.664081899e+02   8.1e-11  0.95  
85  1.3e-07  7.9e-03  8.2e-06  1.00e+00   1.664078752e+02   1.664081783e+02   7.3e-11  0.96  
86  1.2e-07  7.9e-03  7.4e-06  1.00e+00   1.664078950e+02   1.664081678e+02   6.5e-11  0.97  
87  1.1e-07  7.9e-03  6.7e-06  1.00e+00   1.664079128e+02   1.664081583e+02   5.9e-11  0.98  
88  9.7e-08  7.9e-03  6.0e-06  1.00e+00   1.664079289e+02   1.664081498e+02   5.3e-11  0.99  
89  8.7e-08  7.8e-03  5.4e-06  1.00e+00   1.664079433e+02   1.664081422e+02   4.8e-11  1.00  
90  7.8e-08  7.8e-03  4.9e-06  1.00e+00   1.664079563e+02   1.664081353e+02   4.3e-11  1.01  
91  7.1e-08  7.8e-03  4.4e-06  1.00e+00   1.664079680e+02   1.664081291e+02   3.9e-11  1.01  
92  6.4e-08  7.8e-03  3.9e-06  1.00e+00   1.664079785e+02   1.664081235e+02   3.5e-11  1.02  
93  5.7e-08  7.8e-03  3.5e-06  1.00e+00   1.664079880e+02   1.664081185e+02   3.1e-11  1.03  
94  5.1e-08  7.8e-03  3.2e-06  1.00e+00   1.664079965e+02   1.664081140e+02   2.8e-11  1.04  
95  4.6e-08  7.8e-03  2.9e-06  1.00e+00   1.664080042e+02   1.664081099e+02   2.5e-11  1.05  
96  4.2e-08  7.7e-03  2.6e-06  1.00e+00   1.664080111e+02   1.664081062e+02   2.3e-11  1.06  
97  3.7e-08  7.7e-03  2.3e-06  1.00e+00   1.664080173e+02   1.664081029e+02   2.0e-11  1.07  
98  3.4e-08  7.7e-03  2.1e-06  9.99e-01   1.664080229e+02   1.664080999e+02   1.8e-11  1.07  
99  3.0e-08  7.7e-03  1.9e-06  1.00e+00   1.664080279e+02   1.664080973e+02   1.7e-11  1.08  
100 2.7e-08  7.7e-03  1.7e-06  9.99e-01   1.664080325e+02   1.664080949e+02   1.5e-11  1.10  
101 2.5e-08  7.7e-03  1.5e-06  9.99e-01   1.664080365e+02   1.664080927e+02   1.3e-11  1.11  
102 2.2e-08  7.6e-03  1.4e-06  9.98e-01   1.664080402e+02   1.664080908e+02   1.2e-11  1.11  
103 2.0e-08  7.6e-03  1.2e-06  1.00e+00   1.664080435e+02   1.664080891e+02   1.1e-11  1.12  
104 1.8e-08  7.6e-03  1.1e-06  9.98e-01   1.664080465e+02   1.664080875e+02   9.8e-12  1.13  
105 1.6e-08  7.6e-03  1.0e-06  9.98e-01   1.664080491e+02   1.664080861e+02   8.8e-12  1.14  
106 1.5e-08  6.8e-03  9.0e-07  1.00e+00   1.664080515e+02   1.664080848e+02   7.9e-12  1.15  
107 1.3e-08  6.2e-03  8.1e-07  9.99e-01   1.664080537e+02   1.664080836e+02   7.1e-12  1.15  
108 1.2e-08  5.5e-03  7.3e-07  9.97e-01   1.664080557e+02   1.664080826e+02   6.4e-12  1.16  
109 1.1e-08  5.0e-03  6.6e-07  9.97e-01   1.664080574e+02   1.664080816e+02   5.8e-12  1.17  
110 9.6e-09  4.5e-03  5.9e-07  1.00e+00   1.664080590e+02   1.664080808e+02   5.2e-12  1.18  
111 8.6e-09  4.0e-03  5.3e-07  1.01e+00   1.664080605e+02   1.664080800e+02   4.7e-12  1.19  
112 7.7e-09  3.6e-03  4.8e-07  1.01e+00   1.664080618e+02   1.664080793e+02   4.3e-12  1.20  
113 7.0e-09  3.3e-03  4.3e-07  1.00e+00   1.664080629e+02   1.664080787e+02   3.8e-12  1.21  
114 6.3e-09  2.9e-03  3.9e-07  1.01e+00   1.664080640e+02   1.664080781e+02   3.5e-12  1.22  
115 5.7e-09  2.6e-03  3.5e-07  9.94e-01   1.664080649e+02   1.664080776e+02   3.1e-12  1.23  
116 5.1e-09  2.4e-03  3.1e-07  9.84e-01   1.664080657e+02   1.664080772e+02   2.8e-12  1.25  
117 2.1e-08  2.4e-03  3.1e-07  -3.26e-01  1.664080664e+02   1.664080752e+02   2.6e-12  1.26  
118 2.1e-08  2.1e-03  2.8e-07  1.02e+00   1.664080676e+02   1.664080744e+02   2.2e-12  1.27  
119 1.8e-08  2.0e-03  2.5e-07  9.97e-01   1.664080680e+02   1.664080743e+02   2.0e-12  1.28  
120 1.7e-08  1.8e-03  2.3e-07  9.92e-01   1.664080686e+02   1.664080742e+02   1.8e-12  1.29  
121 1.5e-08  1.7e-03  2.1e-07  1.03e+00   1.664080691e+02   1.664080741e+02   1.6e-12  1.29  
122 1.3e-08  1.5e-03  1.9e-07  1.02e+00   1.664080696e+02   1.664080740e+02   1.5e-12  1.30  
123 1.2e-08  1.3e-03  1.7e-07  1.04e+00   1.664080700e+02   1.664080739e+02   1.3e-12  1.31  
124 1.1e-08  1.2e-03  1.5e-07  1.01e+00   1.664080703e+02   1.664080738e+02   1.2e-12  1.32  
125 9.8e-09  1.1e-03  1.4e-07  9.98e-01   1.664080706e+02   1.664080737e+02   1.1e-12  1.33  
126 8.9e-09  9.8e-04  1.2e-07  9.96e-01   1.664080709e+02   1.664080737e+02   9.8e-13  1.34  
Optimizer terminated. Time: 1.34    

solsta = 1, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 1.6640807086e+02    nrm: 2e+01    Viol.  con: 1e-07    var: 0e+00  
  Dual.    obj: 1.6640807369e+02    nrm: 1e+03    Viol.  con: 0e+00    var: 4e-03  
* End solution on dual form. *
Transforming to primal solution.
Solving took 1.38 seconds.
Solving took 9 GP solves and 18.5 seconds.

Solves with these variables bounded:
   value near lower bound: Mission.CruiseAlt
   value near upper bound: Mission.Aircraft.HorizontalTail.WingBox.M_{r_{out}}, Mission.Aircraft.Engine.Thrust.\alpha_{max}, Mission.Aircraft.Wing.WingNoStruct.A_{tri}, Mission.TotalTime, Mission.Aircraft.LandingGear.d_{nacelle}, Mission.T_{t_{4.1_{max-Cruise}}}

Checking for relaxed constants...
Solution check warning: Primal solution computed cost did not match solver-returned cost: 1.4957403142127757e+110 vs 1.49570493199e+110
GP iteration 0 has relaxed constants

Cost
----
 1.496e+110

Free Variables
--------------
                   | Mission.Aircraft.Engine.Turbine.Relax
        C_{p_{t2}} : 2.251                                                Cp Value for Combustion Products in LP Turbine

                   | Mission.Aircraft.Fuselage.Relax
          l_{nose} : 1.042                                                Nose length
          n_{pass} : [ 2.86     ]                                         Number of passengers

                   | Mission.Aircraft.Relax
f_{L_{total/wing}} : 1.656                                                Total lift as a percentage of wing lift

                   | Mission.Aircraft.Wing.WingNoStruct.Relax
     \tan(\Lambda) : 1.133                                                Tangent of quarter-chord sweep angle

                   | Mission.FlightState.Atmosphere.Relax
           L_{atm} : [ 1.77      1         1         1         1        ] Temperature lapse rate
            T_{sl} : [ 1         1         1.25      1         1        ] Temperature at sea level

                   | Mission.Relax
           R_{req} : 2.362                                                Required Cruise Range

Solution check warning: Primal solution computed cost did not match solver-returned cost: 7.485942833952247e+74 vs 7.48576841516e+74
GP iteration 1 has relaxed constants

Cost
----
 7.486e+74

Free Variables
--------------
          | Mission.Aircraft.Engine.Combustor.Relax
hold_{4a} : 1.093        1+(gamma-1)/2 * M_4a**2

          | Mission.Aircraft.Fuselage.Relax
 n_{pass} : [ 1.03     ] Number of passengers

          | Mission.Aircraft.LandingGear.Relax
 h_{hold} : 1.006        Hold height

WEIGHT DIFFERENCES


Total Fuel Weight Percent Diff: [-92.94682601]


Total Aircraft Weight Percent Diff: [-21.48053826]


Engine Weight Percent Diff: -56.27816263501683


Fuselage Weight Percent Diff: -0.8697283781658797


Payload Weight Percent Diff: [-0.0400356]


VT Weight Percent Diff: -8.607712900393501


HT Weight Percent Diff: -93.23330431885311


Wing Weight Percent Diff: 8.267573259901017




WING DIFFERENCES


Wing Span Percent Diff: -0.029994358510184876


Wing Area Percent Diff: 32.89970105408197




HORIZONTAL TAIL DIFFERENCES


HT Area Percent Diff: 40.48862631668246




VERTICAL TAIL DIFFERENCES




VT Span Percent Diff: -11.02232031308826


VT Area Percent Diff: -60.38681772051953




CRUISE SEGMENT 1 DRAG DIFFERENCES


Overall Cd Percent Diff: [-18.54721004]


L/D Percent Diff: [24.01023756]


Nacelle Cd Percent Diff: [-94.27640786]


HT Cd Percent Diff: [-80.7694112] dimensionless


Fuselage Cd Percent Diff: [108.78752887]


VT Cd Percent Diff: [-58.00288783] dimensionless


Wing Cd percent Diff: [-14.229156]
Induced Drag Cd Percent Diff: [1.21939606]




CRUISE SEGMENT 1 TSFC DIFFERENCES


Initial Cruise TSFC Percent Diff: [-90.57036149]




FUSELAGE DIFFERENCES




Weight of HB material: -38.360425524416385 


Weight of VB material: 87.8200230270085 
Fan Propulsive Efficiency in Cruise Segment 1
---------------------
[0.71260522]
Mission1
========

Cost
----
 W_{f_{total}}[:].sum()

Constraints
-----------
   W_{buoy}[:] >= \rho_{cabin}[:]*9.81*V_{cabin}
   PRFC[:] = W_{f_{primary}}[:]/9.81*h_{f}/(R_{req}*W_{payload}[:])
   x_{CG}[:]*W_{avg}[:] >= x_{misc}*W_{misc} + x_{CG_{lg}}*W_{lg} + 0.5*(W_{fuse} + W_{payload}[:])*l_{fuse} + W_{ht}*x_{CG_{ht}} + W_{vt}*x_{CG_{vt}} + n_{eng}*W_{engsys}*x_{eng} + W_{wing}*(x_{wing} + \Delta x_{AC_{wing}}) + (F_{fuel}[:] + f_{fuel_{res}})*W_{f_{primary}}[:]*(x_{wing} + \Delta x_{AC_{wing}}*F_{fuel}[:])
   x_{CG}[3] <= \Delta x_n + x_n
   \Delta x_m + x_{CG}[3] >= x_m
   \tan(\phi)*(z_{CG} + l_m) + x_{CG}[3] <= x_m
   C_{D_{fuse}}[:] = 0.018081
   M_{fuseD} = 0.72
   W_{start}[0] = W_{total}[:]
   W_{start}[:] >= W_{end}[:] + W_{burn}[:]
   W_{start}[1:] = W_{end}[:4]
   W_{dry}[:] + W_{payload}[:] + f_{fuel_{res}}*W_{f_{primary}}[:] <= W_{end}[-1]
   W_{f_{climb}}[:] >= 0 + W_{burn}[:3][0] + W_{burn}[:3][1] + W_{burn}[:3][2]
   W_{f_{cruise}}[:] >= 0 + W_{burn}[3:][0] + W_{burn}[3:][1]
   hft[2] >= CruiseAlt
   hft[1:5] = hft[:4] + dhft[1:5]
   hft[0] = dhft[0]
   dhft[1:3] = dhft[:2]
   RC[0] >= 2.5e+03
   RC[:3] >= RC_{min}[:3]
   \theta[2] >= 0.015
   hft[2] >= MinCruiseAlt
   n_{eng}*F[:] >= D[:] + W_{avg}[:]*\theta[:]
   R_{segment}[3:4] = R_{segment}[4:5]
   M[3:5] >= M_{min}
   0 + R_{segment}[0] + R_{segment}[1] + R_{segment}[2] + R_{segment}[3] + R_{segment}[4] >= R_{req}
   Fsafetyfac*F[0] = T_e
   W_{burn}[:] = n_{eng}*TSFC[:]*thr[:]*F[:]
   V_2[:] = M_2[:]*a[:]
   \alpha_{max,w}[:3] = 0.18
   \alpha_{max,w}[3:] = 0.1
   0 + thr[0] + thr[1] + thr[2] + thr[3] + thr[4] <= TotalTime
   0 + thr[:3][0] + thr[:3][1] + thr[:3][2] <= ClimbTime
   ClimbTime <= MaxClimbTime
   T_{t_{4.1}}[3:] <= T_{t_{4.1_{max-Cruise}}}
   F_{fuel}[0] >= (0 + W_{burn}[1:][0] + W_{burn}[1:][1] + W_{burn}[1:][2] + W_{burn}[1:][3] + 1e-07*W_{f_{primary}}[:])/W_{f_{primary}}[:]
   F_{fuel}[:] <= 1.0000001
   F_{fuel}[1] >= (0 + W_{burn}[2:][0] + W_{burn}[2:][1] + W_{burn}[2:][2] + 1e-07*W_{f_{primary}}[:])/W_{f_{primary}}[:]
   F_{fuel}[:] <= 1.0000001
   F_{fuel}[2] >= (0 + W_{burn}[3:][0] + W_{burn}[3:][1] + 1e-07*W_{f_{primary}}[:])/W_{f_{primary}}[:]
   F_{fuel}[:] <= 1.0000001
   F_{fuel}[3] >= (0 + W_{burn}[4:][0] + 1e-07*W_{f_{primary}}[:])/W_{f_{primary}}[:]
   F_{fuel}[:] <= 1.0000001
   F_{fuel}[4] >= (0 + 1e-07*W_{f_{primary}}[:])/W_{f_{primary}}[:]
   F_{fuel}[:] <= 1.0000001
   OPR[:] <= OPR_{max}
 
 Aircraft
     Fuselage
       W_{lugg}[:] >= f_{lugg,2}*n_{pass}[:]*2*W_{checked} + f_{lugg,1}*n_{pass}[:]*W_{checked} + W_{carry on}
       W_{pass}[:] >= n_{pass}[:]*W_{avg. pass}
       W_{payload}[:] >= W_{pass}[:] + W_{lugg}[:] + W_{cargo}
       W_{payload}[:] >= n_{pass}[:]*W_{avg. pass_{total}}
       W_{payload}[:] <= W_{payload_{max}}
       n_{pass}[:] <= n_{seat}
       n_{rows} = n_{seat}/SPR
       l_{shell} = n_{rows}*p_s
       \theta_{db} = w_{db}/R_{fuse}
       R_{fuse}*(1 - 0.5*\theta_{db}^2) <= h_{db}
       A_{db} >= (2*h_{db} + \Delta R_{fuse})*t_{db}
       (PI + 2*\theta_{db} + 2*\theta_{db}*(1 - \theta_{db}^2/2))*R_{fuse}^2 + 2*\Delta R_{fuse}*R_{fuse} <= A_{fuse}
       A_{skin} >= (2PI + 4*\theta_{db})*R_{fuse}*t_{skin} + 2*\Delta R_{fuse}*t_{skin}
       w_{floor} = w_{fuse}
       R_{fuse} + w_{db} >= w_{fuse}
       h_{fuse} = R_{fuse} + 0.5*\Delta R_{fuse}
       t_{skin}*(1 + r_E*f_{string}*\rho_{skin}/\rho_{bend}) >= t_{shell}
       S_{nose} >= (2PI + 4*\theta_{db})*R_{fuse}^2
       S_{bulk} >= (2PI + 4*\theta_{db})*R_{fuse}^2
       l_{fuse} = l_{nose} + l_{shell} + l_{cone}
       l_{cone} = R_{fuse}/\lambda_{cone}
       x_{shell1} = l_{nose}
       x_{shell2} >= l_{nose} + l_{shell}
       t_{skin} = \Delta P_{over}*R_{fuse}/\sigma_{skin}
       t_{db} = 2*\Delta P_{over}*w_{db}/\sigma_{skin}
       \sigma_x = \Delta P_{over}*R_{fuse}/(2*t_{shell})
       \sigma_{\theta} = \Delta P_{over}*R_{fuse}/t_{skin}
       l_{floor} >= l_{shell} + 2*R_{fuse}
       P_{floor} >= N_{land}*(W_{payload_{max}} + W_{seat})
       A_{floor} >= 2*M_{floor}/(\sigma_{floor}*h_{floor}) + 1.5*S_{floor}/\tau_{floor}
       V_{floor} = 2*w_{floor}*A_{floor}
       W_{floor} >= \rho_{floor}*g*V_{floor} + 2*w_{floor}*l_{floor}*W''_{floor}
       \tau_{cone} = \sigma_{skin}
       W_{cone} >= \rho_{cone}*g*V_{cone}*(1 + f_{string} + f_{frame})
       x_{tail} >= l_{nose} + l_{shell} + 0.5*l_{cone}
       -2*R_{fuse}^2*\Delta R_{fuse}*\theta_{db}^2*t_{shell} + 1.57*R_{fuse}*\Delta R_{fuse}^2*t_{shell} + 3.14*R_{fuse}^3*t_{shell} + 4*R_{fuse}^2*\Delta R_{fuse}*t_{shell} + 4*R_{fuse}^3*\theta_{db}*t_{shell} + R_{fuse}*\Delta R_{fuse}^2*\theta_{db}*t_{shell} >= I_{h_{shell}}
       (PI*R_{fuse}^2 + 8*w_{db}*R_{fuse} + (2PI + 4*\theta_{db})*w_{db}^2)*R_{fuse}*t_{shell} >= I_{v_{shell}}
       x_{hbend_{Land}} >= x_{wing}
       x_{hbend_{Land}} <= l_{fuse}
       x_{hbend_{MLF}} >= x_{wing}
       x_{hbend_{MLF}} <= l_{fuse}
       A_{0h} = A_{2h_{Land}}*(x_{shell2} - x_{hbend_{Land}})^0 + A_{1h_{Land}}*(x_{tail} - x_{hbend_{Land}})
       A_{0h} = A_{2h_{MLF}}*(x_{shell2} - x_{hbend_{MLF}})^0 + A_{1h_{MLF}}*(x_{tail} - x_{hbend_{MLF}})
       A_{2h_{Land}} >= N_{land}*(W_{payload_{max}} + W_{padd} + W_{shell} + W_{window} + W_{insul} + W_{floor} + W_{seat})/(2*l_{shell}*h_{fuse}*\sigma_{M_h})
       A_{2h_{MLF}} >= Mission1.Aircraft.Fuselage.N_{lift}*(W_{payload_{max}} + W_{padd} + W_{shell} + W_{window} + W_{insul} + W_{floor} + W_{seat})/(2*l_{shell}*h_{fuse}*\sigma_{M_h})
       A_{0h} = I_{h_{shell}}/(r_E*h_{fuse}^2)
       A_{2h_{Land}}*(x_{shell2} - x_f)^0 + A_{1h_{Land}}*(x_{tail} - x_f) - A_{0h} <= A_{hbendf_{Land}}
       A_{2h_{MLF}}*(x_{shell2} - x_f)^0 + A_{1h_{MLF}}*(x_{tail} - x_f) - A_{0h} <= A_{hbendf_{MLF}}
       A_{2h_{Land}}*(x_{shell2} - x_b)^0 + A_{1h_{Land}}*(x_{tail} - x_b) - A_{0h} <= A_{hbendb_{Land}}
       A_{2h_{MLF}}*(x_{shell2} - x_b)^0 + A_{1h_{MLF}}*(x_{tail} - x_b) - A_{0h} <= A_{hbendb_{MLF}}
       A_{2h_{Land}}/3*(x_{shell2} - x_f)^0 - (x_{shell2} - x_{hbend_{Land}})^0 + A_{1h_{Land}}/2*(x_{tail} - x_f)^0 - (x_{tail} - x_{hbend_{Land}})^0 - A_{0h}*(x_{hbend_{Land}} - x_f) <= V_{hbend_{f}}
       A_{2h_{MLF}}/3*(x_{shell2} - x_f)^0 - (x_{shell2} - x_{hbend_{MLF}})^0 + A_{1h_{MLF}}/2*(x_{tail} - x_f)^0 - (x_{tail} - x_{hbend_{MLF}})^0 - A_{0h}*(x_{hbend_{MLF}} - x_f) <= V_{hbend_{f}}
       A_{2h_{Land}}/3*(x_{shell2} - x_b)^0 - (x_{shell2} - x_{hbend_{Land}})^0 + A_{1h_{Land}}/2*(x_{tail} - x_b)^0 - (x_{tail} - x_{hbend_{Land}})^0 - A_{0h}*(x_{hbend_{Land}} - x_b) <= V_{hbend_{b}}
       A_{2h_{MLF}}/3*(x_{shell2} - x_b)^0 - (x_{shell2} - x_{hbend_{MLF}})^0 + A_{1h_{MLF}}/2*(x_{tail} - x_b)^0 - (x_{tail} - x_{hbend_{MLF}})^0 - A_{0h}*(x_{hbend_{MLF}} - x_b) <= V_{hbend_{b}}
       V_{hbend_{c}} >= 0.5*(A_{hbendf_{Land}} + A_{hbendb_{Land}})*c_0*Mission1.Aircraft.Fuselage.r_{w/c}
       V_{hbend_{c}} >= 0.5*(A_{hbendf_{MLF}} + A_{hbendb_{MLF}})*c_0*Mission1.Aircraft.Fuselage.r_{w/c}
       V_{hbend} >= V_{hbend_{c}} + V_{hbend_{f}} + V_{hbend_{b}}
       W_{hbend} >= g*\rho_{bend}*V_{hbend}
       x_{vbend} >= x_{wing}
       x_{vbend} <= l_{fuse}
       B_{0v} = B_{1v}*(x_{tail} - x_{vbend})
       B_{0v} = I_{v_{shell}}/(r_E*w_{fuse}^2)
       B_{1v}*(x_{tail} - x_b) - B_{0v} <= A_{vbend_{b}}
       0.5*B_{1v}*(x_{tail} - x_b)^0 - (x_{tail} - x_{vbend})^0 - B_{0v}*(x_{vbend} - x_b) <= V_{vbend_{b}}
       V_{vbend_{c}} >= 0.5*A_{vbend_{b}}*c_0*Mission1.Aircraft.Fuselage.r_{w/c}
       V_{vbend} >= V_{vbend_{b}} + V_{vbend_{c}}
       W_{vbend} >= \rho_{bend}*g*V_{vbend}
       x_f = x_{wing} + 0.5*c_0*Mission1.Aircraft.Fuselage.r_{w/c}
       x_b = x_{wing} - 0.5*c_0*Mission1.Aircraft.Fuselage.r_{w/c}
       \sigma_{bend} - r_E*\Delta P_{over}/2*R_{fuse}/t_{shell} >= \sigma_{M_h}
       \sigma_{bend} - r_E*\Delta P_{over}/2*R_{fuse}/t_{shell} >= \sigma_{M_v}
       V_{cyl} = A_{skin}*l_{shell}
       V_{nose} = S_{nose}*t_{skin}
       V_{bulk} = S_{bulk}*t_{skin}
       V_{db} = A_{db}*l_{shell}
       V_{cabin} >= A_{fuse}*(l_{shell} + 0.67*l_{nose} + 0.67*R_{fuse})
       W_{apu} = W_{payload_{max}}*f_{apu}
       W_{db} = \rho_{skin}*g*V_{db}
       W_{insul} >= W''_{insul}*(3.46 + 2*\theta_{db})*R_{fuse}*l_{shell} + 0.55*(S_{nose} + S_{bulk})
       W_{window} >= W'_{window}*l_{shell}
       W_{padd} = W_{payload_{max}}*f_{padd}
       W_{seat} >= W'_{seat}*n_{seat}
       W_{seat} >= f_{seat}*W_{payload_{max}}
       W_{skin} >= \rho_{skin}*g*(V_{cyl} + V_{nose} + V_{bulk})
       W_{shell} >= W_{skin}*(1 + f_{string} + f_{fadd} + f_{frame}) + W_{db}
       W_{fuse} >= C_{fuse}*(W_{shell} + W_{floor} + W_{insul} + W_{apu} + W_{fix} + W_{window} + W_{padd} + W_{seat} + W_{hbend} + W_{vbend} + W_{cone})
     
     Wing
       WingNoStruct
         A_{rect} = c_{tip}*b
         0.5*(1 - \lambda)*c_{root}*b <= A_{tri}
         p >= 1 + 2*\lambda
         2*q >= 1 + p
         y_{mac} = b/3*q/p
         mac >= 0.667*(1 + \lambda + \lambda^2)*c_{root}/q
         \lambda = c_{tip}/c_{root}
         S = b*(c_{root} + c_{tip})/2
         0.0524*\lambda^4 - 0.15*\lambda^3 + 0.166*\lambda^2 - 0.0706*\lambda + 0.0119 <= f(\lambda_w)
         e*(1 + f(\lambda_w)*AR) <= 1
         \lambda >= 0.15
         V_{fuel, max} <= 0.303*mac^2*b*\tau
         W_{fuel_{wing}} <= \rho_{fuel}*V_{fuel, max}*g
         b <= b_{max}
       
       WingBox
         AR = b^2/S
         0.423*Mission1.Aircraft.Wing.WingBox.r_{w/c}*\tau^2*t_{cap} >= 0.92*Mission1.Aircraft.Wing.WingBox.r_{w/c}*\tau*t_{cap}^2 + I_{cap}
         \nu^3.94 >= 0.86*p^-2.38 + 0.14*p^0.56
         W_{web} >= 8*\rho_{web}*g*r_h*\tau*t_{web}*S^1.5*\nu/(3*AR^0.5)
         \tau <= \tau_{max_w}
         W_{struct} >= W_{web} + W_{cap}
         AR*L_{max}*q^2/(\tau*S*t_{web}*\sigma_{max,shear}) <= 12
         W_{cap} >= 8*\rho_{cap}*g*Mission1.Aircraft.Wing.WingBox.r_{w/c}*t_{cap}*S^1.5*\nu/(3*AR^0.5)
         Mission1.Aircraft.Wing.WingBox.N_{lift} = 3
         Mission1.Aircraft.Wing.WingBox.M_r*AR*q^2*\tau/(S*I_{cap}*\sigma_{max}) <= 8
         \lambda = taper
         W_{wing} >= C_{wing}*W_{struct} + W_{struct}*(f_{flap} + f_{slat} + f_{aileron} + f_{lete} + f_{ribs} + f_{spoiler} + f_{watt})
         0.0417*(c_{root} + 5*c_{tip})/S*b^2*\tan(\Lambda) >= \Delta x_{AC_{wing}}
     
     Engine
         Compressor
           (no constraints)
         
         Combustor
           (no constraints)
         
         Turbine
           (no constraints)
         
         Thrust
           (no constraints)
         
         FanMap
           (no constraints)
         
         LPCMap
           (no constraints)
         
         HPCMap
           (no constraints)
         
         Sizing
           A_{2} >= A_{5} + A_{7}
         
         FlightState
             V[:] = V[:]
             a[:] = (\gamma[:]*R[:]*T_{atm}[:])^0.5
             V[:] = M[:]*a[:]
           
           Altitude
             h[:] = hft[:]
           
           Atmosphere
             (P_{atm}[:]/p_{sl}[:])^0.190222560396 = T_{atm}[:]/T_{sl}[:]
             \rho[:] = P_{atm}[:]/(R_{atm}[:]/M_{atm}[:]*T_{atm}[:])
             T_{sl}[:] = T_{atm}[:] + L_{atm}[:]*h[:]
             \mu[:] = C_1[:]*T_{atm}[:]^1.5/(6.64*T_s[:]^0.72)
         
         EnginePerformance
           CompressorPerformance
               T_{t_0}[:] = T_{atm}[:]/c1[:]^-1
               h_{t_0}[:] = C_{p_{air}*T_{t_0}[:]
               P_{t_{1.8}}[:] = \pi_{d}*P_{t_0}[:]
               T_{t_{1.8}}[:] = T_{t_0}[:]
               h_{t_{1.8}}[:] = h_{t_0}[:]
               P_{t_0}[:] = f_{BLI_{P}}*P_{atm}[:]/c1[:]^-3.5
               T_{T_{2}}[:] = T_{t_{1.8}}[:]
               h_{T_{2}}[:] = h_{t_{1.8}}[:]
               P_{T_{2}}[:] = P_{t_{1.8}}[:]
               P_{t_{2.1}}[:] = \pi_{f}[:]*P_{T_{2}}[:]
               T_{t_{2.1}}[:] = T_{T_{2}}[:]*\pi_{f}[:]^0.307767877016
               h_{t_{2.1}}[:] = C_{p_{air}*T_{t_{2.1}}[:]
               P_{t_7}[:] = \pi_{fn}*P_{t_{2.1}}[:]
               T_{t_7}[:] = T_{t_{2.1}}[:]
               h_{t_7}[:] = h_{t_{2.1}}[:]
               P_{t_{2.5}}[:] = \pi_{lc}[:]*\pi_{f}[:]*P_{T_{2}}[:]
               T_{t_{2.5}}[:] = T_{T_{2}}[:]*(\pi_{f}[:]*\pi_{lc}[:])^0.309448280152
               h_{t_{2.5}}[:] = T_{t_{2.5}}[:]*C_{p_{1}
               P_{t_3}[:] = \pi_{hc}[:]*P_{t_{2.5}}[:]
               T_{t_3}[:] = T_{t_{2.5}}[:]*\pi_{hc}[:]^0.293761306491
               h_{t_3}[:] = C_{p_{2}*T_{t_3}[:]
           
           CombustorPerformance
             h_{t_4}[:] = C_{p_{c}}*T_{t_4}[:]
             h_{t_{4.1}}[:] = C_{p_{c}}*T_{t_{4.1}}[:]
             fp1[:] = f[:] + 1
             M_{4a}[:] = 0.1025
             fp1[:]*u_{4.1}[:] = (u_{4a}[:]*fp1[:]*\alpha_c*u_c[:])^0.5
             T_{4.1}[:] <= [[T_{t_{4.1}}[0,0] - u_{4.1}[0,0]^2*0.5/C_{p_{c}}], [T_{t_{4.1}}[1,0] - u_{4.1}[1,0]^2*0.5/C_{p_{c}}], [T_{t_{4.1}}[2,0] - u_{4.1}[2,0]^2*0.5/C_{p_{c}}], [T_{t_{4.1}}[3,0] - u_{4.1}[3,0]^2*0.5/C_{p_{c}}], [T_{t_{4.1}}[4,0] - u_{4.1}[4,0]^2*0.5/C_{p_{c}}]]
             P_{t_{4.1}}[:] = P_{4a}[:]*(T_{t_{4.1}}[:]/T_{4.1}[:])^-4.19488817891
             u_{4a}[:] = M_{4a}[:]*(1.31*Mission1.Aircraft.Engine.EngineConstants.R*T_{t_4}[:])^0.5/hold_{4a}
             u_c[:] = r_{uc}*u_{4a}[:]
             P_{4a}[:] = P_{t_4}[:]*hold_{4a}^4.19488817891
           
           TurbinePerformance
             h_{t_{4.5}}[:] = C_{p_{t1}}*T_{t_{4.5}}[:]
             P_{t_{4.9}}[:] = \pi_{LPT}[:]*P_{t_{4.5}}[:]
             \pi_{LPT}[:] = (T_{t_{4.9}}[:]/T_{t_{4.5}}[:])^3.5188700565
             h_{t_{4.9}}[:] = C_{p_{t2}}*T_{t_{4.9}}[:]
             P_{t_5}[:] = \pi_{tn}*P_{t_{4.9}}[:]
             T_{t_5}[:] = T_{t_{4.9}}[:]
             h_{t_5}[:] = h_{t_{4.9}}[:]
           
           ThrustPerformance
             P_{8}[:] = P_{atm}[:]
             h_{8}[:] = C_{p_{fex}*T_{8}[:]
             u_{8}[:]^2 + 2*h_{8}[:] <= 2*h_{t_8}[:]
             (P_{8}[:]/P_{t_8}[:])^0.279019466474 = T_{8}[:]/T_{t_8}[:]
             h_{t_8}[:] = C_{p_{fex}*T_{t_8}[:]
             P_{6}[:] = P_{atm}[:]
             (P_{6}[:]/P_{t_6}[:])^0.285714285714 = T_{6}[:]/T_{t_6}[:]
             u_{6}[:]^2 + 2*h_6[:] <= 2*h_{t_6}[:]
             h_6[:] = C_{p_{tex}*T_{6}[:]
             h_{t_6}[:] = C_{p_{tex}*T_{t_6}[:]
             \alpha[:] = m_{fan}[:]/m_{core}[:]
             \alpha_{+1}[:] = \alpha[:] + 1
             \alpha[:] <= \alpha_{max}
             F[:] <= F_{6}[:] + F_{8}[:]
             F_{sp}[:] = F[:]/(\alpha_{+1}[:]*m_{core}[:]*a[:])
             TSFC[:] = 1/I_{sp}[:]
             F_{8}[:]/(\alpha[:]*m_{core}[:]) + V[:]*f_{BLI_{V}} <= u_{8}[:]
           
           FanMapPerformance
             m_{tild_f}[:] = m_{f}[:]/\bar{m}_{fan_{D}}
           
           LPCMapPerformance
             m_{tild_lc}[:] = m_{lc}[:]/m_{lc_D}
           
           HPCMapPerformance
             m_{tild_{hc}}[:] = m_{hc}[:]/m_{hc_D}
           
           SizingPerformance
             P_{7}[:] >= P_{atm}[:]
             M_7[:] <= 1
             a_{7}[:] = (1.4*Mission1.Aircraft.Engine.EngineConstants.R*T_{7}[:])^0.5
             a_{7}[:]*M_7[:] = u_{7}[:]
             \rho_7[:] = P_{7}[:]/(Mission1.Aircraft.Engine.EngineConstants.R*T_{7}[:])
             P_{5}[:] >= P_{atm}[:]
             M_5[:] <= 1
             a_{5}[:] = (1.39*Mission1.Aircraft.Engine.EngineConstants.R*T_{5}[:])^0.5
             a_{5}[:]*M_5[:] = u_{5}[:]
             \rho_5[:] = P_{5}[:]/(Mission1.Aircraft.Engine.EngineConstants.R*T_{5}[:])
             h_{2}[:] = C_{p_{1}*T_{2}[:]
             \rho_{2}[:] = P_{2}[:]/(Mission1.Aircraft.Engine.EngineConstants.R*T_{2}[:])
             u_{2}[:] = M_2[:]*(C_{p_{1}*Mission1.Aircraft.Engine.EngineConstants.R*T_{2}[:]/dum[:])^0.5
             h_{2.5}[:] = C_{p_{2}*T_{2.5}[:]
             \rho_{2.5}[:] = P_{2.5}[:]/(Mission1.Aircraft.Engine.EngineConstants.R*T_{2.5}[:])
             u_{2.5}[:] = M_{2.5}[:]*(C_{p_{2}*Mission1.Aircraft.Engine.EngineConstants.R*T_{2.5}[:]/dum[:])^0.5
         m_{total}[:]/\alpha_{+1}[:]*1/100*9.81*(1.68e+03 + 17.7*\pi_{f}[:]*\pi_{lc}[:]*\pi_{hc}[:]/30 + 1.66e+03*(\alpha[:]/5)^1.2) <= W_{engine}
           d_{f} = (4*A_{2}/(PI*HTR_{f_{SUB}}))^0.5
           d_{LPC} = (4*A_{2.5}/(PI*HTR_{lpc_{SUB}}))^0.5
           \eta_{B}*f[:]*h_{f} >= [[(1 - \alpha_c)*h_{t_4}[0,0] - (1 - \alpha_c)*h_{t_3}[0,0]], [(1 - \alpha_c)*h_{t_4}[1,0] - (1 - \alpha_c)*h_{t_3}[1,0]], [(1 - \alpha_c)*h_{t_4}[2,0] - (1 - \alpha_c)*h_{t_3}[2,0]], [(1 - \alpha_c)*h_{t_4}[3,0] - (1 - \alpha_c)*h_{t_3}[3,0]], [(1 - \alpha_c)*h_{t_4}[4,0] - (1 - \alpha_c)*h_{t_3}[4,0]]] + C_{p_{fuel}*f[:]*([[T_{t_4}[0,0] - T_{t_f}], [T_{t_4}[1,0] - T_{t_f}], [T_{t_4}[2,0] - T_{t_f}], [T_{t_4}[3,0] - T_{t_f}], [T_{t_4}[4,0] - T_{t_f}]])
           h_{t_{4.1}}[:]*fp1[:] <= (1 - \alpha_c + f[:])*h_{t_4}[:] + \alpha_c*h_{t_3}[:]
           P_{t_4}[:] = \pi_{b}*P_{t_3}[:]
           M_{takeoff}*\eta_{HPshaft}*fp1[:]*([[h_{t_{4.1}}[0,0] - h_{t_{4.5}}[0,0]], [h_{t_{4.1}}[1,0] - h_{t_{4.5}}[1,0]], [h_{t_{4.1}}[2,0] - h_{t_{4.5}}[2,0]], [h_{t_{4.1}}[3,0] - h_{t_{4.5}}[3,0]], [h_{t_{4.1}}[4,0] - h_{t_{4.5}}[4,0]]]) >= [[h_{t_3}[0,0] - h_{t_{2.5}}[0,0]], [h_{t_3}[1,0] - h_{t_{2.5}}[1,0]], [h_{t_3}[2,0] - h_{t_{2.5}}[2,0]], [h_{t_3}[3,0] - h_{t_{2.5}}[3,0]], [h_{t_3}[4,0] - h_{t_{2.5}}[4,0]]]
           M_{takeoff}*\eta_{LPshaft}*fp1[:]*([[h_{t_{4.5}}[0,0] - h_{t_{4.9}}[0,0]], [h_{t_{4.5}}[1,0] - h_{t_{4.9}}[1,0]], [h_{t_{4.5}}[2,0] - h_{t_{4.9}}[2,0]], [h_{t_{4.5}}[3,0] - h_{t_{4.9}}[3,0]], [h_{t_{4.5}}[4,0] - h_{t_{4.9}}[4,0]]]) >= [[h_{t_{2.5}}[0,0] - h_{t_{1.8}}[0,0]], [h_{t_{2.5}}[1,0] - h_{t_{1.8}}[1,0]], [h_{t_{2.5}}[2,0] - h_{t_{1.8}}[2,0]], [h_{t_{2.5}}[3,0] - h_{t_{1.8}}[3,0]], [h_{t_{2.5}}[4,0] - h_{t_{1.8}}[4,0]]] + \alpha[:]*([[h_{t_{2.1}}[0,0] - h_{T_{2}}[0,0]], [h_{t_{2.1}}[1,0] - h_{T_{2}}[1,0]], [h_{t_{2.1}}[2,0] - h_{T_{2}}[2,0]], [h_{t_{2.1}}[3,0] - h_{T_{2}}[3,0]], [h_{t_{2.1}}[4,0] - h_{T_{2}}[4,0]]])
           P_{t_{4.5}}[:] = \pi_{HPT}[:]*P_{t_{4.1}}[:]
           \pi_{HPT}[:] = (T_{t_{4.5}}[:]/T_{t_{4.1}}[:])^3.77163522013
           \pi_{f}[:]*1.7/\pi_{f_D} = (1.05*N_{f}[:]^0.0871)^10
           \pi_{f}[:]*1.7/\pi_{f_D} <= 1.1*(1.06*m_{tild_f}[:]^0.137)^10
           \pi_{f}[:]*1.7/\pi_{f_D} >= 0.9*(1.06*m_{tild_f}[:]^0.137)^10
           m_{f}[:] = m_{fan}[:]*(T_{T_{2}}[:]/T_{ref})^0.5/(P_{T_{2}}[:]/P_{ref})
           \pi_{f}[:] >= 1
           \pi_{lc}[:]*26/\pi_{lc_D} = (1.38*N_{1}[:]^0.566)^10
           \pi_{lc}[:]*26/\pi_{lc_D} <= 1.1*(1.38*m_{tild_lc}[:]^0.122)^10
           \pi_{lc}[:]*26/\pi_{lc_D} >= 0.9*(1.38*m_{tild_lc}[:]^0.122)^10
           \pi_{lc}[:] >= 1
           m_{lc}[:] = m_{core}[:]*(T_{T_{2}}[:]/T_{ref})^0.5/(P_{T_{2}}[:]/P_{ref})
           \pi_{hc}[:]*26/\pi_{hc_D} = (1.38*N_{2}[:]^0.566)^10
           \pi_{hc}[:]*26/\pi_{hc_D} >= 0.9*(1.38*m_{tild_{hc}}[:]^0.122)^10
           \pi_{hc}[:]*26/\pi_{hc_D} <= 1.1*(1.38*m_{tild_{hc}}[:]^0.122)^10
           m_{hc}[:] = m_{core}[:]*(T_{t_{2.5}}[:]/T_{ref})^0.5/(P_{t_{2.5}}[:]/P_{ref})
           \pi_{hc}[:] >= 1
         OPR[:] = \pi_{hc}[:]*\pi_{lc}[:]*\pi_{f}[:]
           P_{t_8}[:] = P_{t_7}[:]
           T_{t_8}[:] = T_{t_7}[:]
           P_{t_6}[:] = P_{t_5}[:]
           T_{t_6}[:] = T_{t_5}[:]
           F_{6}[:]/(M_{takeoff}*m_{core}[:]) + fp1[:]*V[:] <= fp1[:]*u_{6}[:]
           I_{sp}[:] = F_{sp}[:]*a[:]*\alpha_{+1}[:]/(f[:]*g)
           N_{f}[:]*G_{f} = N_{1}[:]
           N_{1}[:] <= 1.1
           N_{2}[:] <= 1.1
         fp1[:]*m_{hc}[:]*M_{takeoff}*P_{t_{2.5}}[:]/P_{t_{4.1}}[:]*(T_{t_{4.1}}[:]/T_{t_{2.5}}[:])^0.5 = m_{htD}
         fp1[:]*m_{lc}[:]*M_{takeoff}*P_{t_{1.8}}[:]/P_{t_{4.5}}[:]*(T_{t_{4.5}}[:]/T_{t_{1.8}}[:])^0.5 = m_{ltD}
           P_{7}[:]/P_{t_7}[:] = (T_{7}[:]/T_{t_7}[:])^3.5
           (T_{7}[:]/T_{t_7}[:])^-1 >= 1 + 0.2*M_7[:]^2
           P_{5}[:]/P_{t_5}[:] = (T_{5}[:]/T_{t_5}[:])^3.583979
           (T_{5}[:]/T_{t_5}[:])^-1 >= 1 + 0.2*M_5[:]^2
           M_{takeoff}*m_{core}[:] = \rho_5[:]*A_{5}*u_{5}[:]/fp1[:]
           m_{fan}[:] = \rho_7[:]*A_{7}*u_{7}[:]
           m_{total}[:] = m_{fan}[:] + m_{core}[:]
           P_{2}[:] = P_{T_{2}}[:]*hold_{2}[:]^-3.512
           T_{2}[:] = T_{T_{2}}[:]*hold_{2}[:]^-1
           m_{fan}[:]/(\rho_{2}[:]*u_{2}[:]) = A_{2}
           P_{2.5}[:] = P_{t_{2.5}}[:]*hold_{2.5}[:]^-3.824857
           T_{2.5}[:] = T_{t_{2.5}}[:]*hold_{2.5}[:]^-1
           m_{core}[:]/(\rho_{2.5}[:]*u_{2.5}[:]) = A_{2.5}
           1.3*fp1[:]*M_{takeoff}*m_{coreD}*2.2/14.1 >= m_{htD}
           0.7*fp1[:]*M_{takeoff}*m_{coreD}*2.2/14.1 <= m_{htD}
           1.3*fp1[:]*M_{takeoff}*m_{coreD}*1.97/6.98 >= m_{ltD}
           0.7*fp1[:]*M_{takeoff}*m_{coreD}*1.97/6.98 <= m_{ltD}
           m_{lc_D} >= 0.7*m_{coreD}/0.649
           m_{lc_D} <= 1.3*m_{coreD}/0.649
           m_{hc_D} >= 0.7*m_{coreD}*1.29/3.23
           m_{hc_D} <= 1.3*m_{coreD}*1.29/3.23
           \bar{m}_{fan_{D}} >= 0.7*\alpha_{OD}*m_{coreD}*0.932/0.405
           \bar{m}_{fan_{D}} <= 1.3*\alpha_{OD}*m_{coreD}*0.932/0.405
           F[:] = F_{spec}[:]
           T_{t_{4.1}}[:] <= T_{t_{4.1_{max}}}
           OPR[:] <= OPR_{max}
     
     VerticalTail
       VerticalTailNoStruct
         C_{L_{vt,yaw}} = 0.85*C_{L_{vt,max}}
         L_{vt,EO} = 0.5*\rho_{TO}*V_1^2*S_{vt}*C_{L_{vt,EO}}
         c_{l_{vt,EO}} >= C_{L_{vt,EO}}*(1 + c_{l_{vt,EO}}/(PI*e_{vt}*A_{vt}))
         A_{vt} = b_{vt}^2/S_{vt}
         b_{vt}*(c_{root_{vt}} + c_{tip_{vt}})/2 >= S_{vt}
         p_{vt} >= 1 + 2*\lambda_{vt}
         2*q_{vt} >= 1 + p_{vt}
         y_{\bar{c}_{vt}} = b_{vt}/3*q_{vt}/p_{vt}
         z_{\bar{c}_{vt}} = b_{vt}/3*q_{vt}/p_{vt}
         0.667*(1 + \lambda_{vt} + \lambda_{vt}^2)*c_{root_{vt}}/q_{vt} = \bar{c}_{vt}
         \lambda_{vt} = c_{tip_{vt}}/c_{root_{vt}}
         \Delta x_{trail_{vt}} >= \Delta x_{lead_{vt}} + c_{root_{vt}}
         \Delta x_{lead_{vt}} + y_{\bar{c}_{vt}}*\tan(\Lambda_{vt}) + 0.25*\bar{c}_{vt} >= l_{vt}
         \lambda_{vt} >= 0.25
         V_{vt} >= V_{vt_{min}}
       
       WingBox
         AR_{vt} = (2*b_{vt})^2/(2*S_{vt})
         0.423*Mission1.Aircraft.VerticalTail.WingBox.r_{w/c}*\tau_{vt}^2*t_{cap} >= 0.92*Mission1.Aircraft.VerticalTail.WingBox.r_{w/c}*\tau_{vt}*t_{cap}^2 + I_{cap}
         \nu^3.94 >= 0.86*p_{vt}^-2.38 + 0.14*p_{vt}^0.56
         W_{web} >= 8*\rho_{web}*g*r_h*\tau_{vt}*t_{web}*(2*S_{vt})^1.5*\nu/(3*AR_{vt}^0.5)
         \tau_{vt} <= 0.14
         W_{struct} >= 0.5*(W_{web} + W_{cap})
         Mission1.Aircraft.VerticalTail.WingBox.M_r >= 2*L_{vt_{max}}*AR_{vt}*p_{vt}/24
         AR_{vt}*2*L_{vt_{max}}*Mission1.Aircraft.VerticalTail.WingBox.N_{lift}*q_{vt}^2/(\tau_{vt}*2*S_{vt}*t_{web}*\sigma_{max,shear}) <= 12
         W_{cap} >= 8*\rho_{cap}*g*Mission1.Aircraft.VerticalTail.WingBox.r_{w/c}*t_{cap}*(2*S_{vt})^1.5*\nu/(3*AR_{vt}^0.5)
         Mission1.Aircraft.VerticalTail.WingBox.N_{lift} = 1
         Mission1.Aircraft.VerticalTail.WingBox.N_{lift}*Mission1.Aircraft.VerticalTail.WingBox.M_r*AR_{vt}*q_{vt}^2*\tau_{vt}/(2*S_{vt}*I_{cap}*\sigma_{max}) <= 8
         \lambda_{vt} = taper
         W_{vt} >= N_{spar}*C_{VT}*(W_{struct} + W_{struct}*f_{VT})
     
     HorizontalTail
       HorizontalTailNoStruct
         \Delta x_{lead_{ht}} + y_{\bar{c}_{ht}}*\tan(\Lambda_{ht}) + 0.25*\bar{c}_{ht} >= l_{ht}
         \Delta x_{trail_{ht}} >= \Delta x_{lead_{ht}} + c_{root_{ht}}
         p_{ht} >= 1 + 2*\lambda_{ht}
         2*q_{ht} >= 1 + p_{ht}
         y_{\bar{c}_{ht}} = b_{ht}/3*q_{ht}/p_{ht}
         0.667*(1 + \lambda_{ht} + \lambda_{ht}^2)*c_{root_{ht}}/q_{ht} = \bar{c}_{ht}
         \lambda_{ht} = c_{tip_{ht}}/c_{root_{ht}}
         S_{ht} = b_{ht}*(c_{root_{ht}} + c_{tip_{ht}})/2
         0.0524*\lambda_{ht}^4 - 0.15*\lambda_{ht}^3 + 0.166*\lambda_{ht}^2 - 0.0706*\lambda_{ht} + 0.0119 <= f(\lambda_{ht})
         e_{ht}*(1 + f(\lambda_{ht})*AR_{ht}) <= 1
         AR_{ht} = b_{ht}^2/S_{ht}
         \lambda_{ht} >= 0.2
         \lambda_{ht} <= 1
       
       WingBox
         AR_{ht} = b_{ht}^2/S_{ht}
         0.423*Mission1.Aircraft.HorizontalTail.WingBox.r_{w/c}*\tau_{ht}^2*t_{cap} >= 0.92*Mission1.Aircraft.HorizontalTail.WingBox.r_{w/c}*\tau_{ht}*t_{cap}^2 + I_{cap}
         \nu^3.94 >= 0.86*p_{ht}^-2.38 + 0.14*p_{ht}^0.56
         W_{web} >= 8*\rho_{web}*g*r_h*\tau_{ht}*t_{web}*S_{ht}^1.5*\nu/(3*AR_{ht}^0.5)
         \tau_{ht} <= 0.14
         W_{struct} >= W_{web} + W_{cap}
         L_{ht_{tri_{out}}} >= L_{ht_{tri}}*b_{ht_{out}}^2/(0.5*b_{ht})^2
         L_{ht_{rect_{out}}} >= L_{ht_{rect}}*b_{ht_{out}}/(0.5*b_{ht})
         2*AR_{ht}*L_{shear}*Mission1.Aircraft.HorizontalTail.WingBox.N_{lift}*q_{ht}^2/(\tau_{ht}*S_{ht}*t_{web}*\sigma_{max,shear}) <= 12
         W_{cap} >= \pi_{M-fac}*8*\rho_{cap}*g*Mission1.Aircraft.HorizontalTail.WingBox.r_{w/c}*t_{cap}*S_{ht}^1.5*\nu/(3*AR_{ht}^0.5)
         Mission1.Aircraft.HorizontalTail.WingBox.N_{lift} = 1
         Mission1.Aircraft.HorizontalTail.WingBox.N_{lift}*Mission1.Aircraft.HorizontalTail.WingBox.M_r*AR_{ht}*q_{ht}^2*\tau_{ht}/(S_{ht}*I_{cap}*\sigma_{max}) <= 8
         L_{ht_{rect}} >= L_{ht_{max}}/2*c_{tip_{ht}}*b_{ht}/S_{ht}
         L_{ht_{max}}/4*(1 - taper)*c_{root_{ht}}*b_{ht}/S_{ht} <= L_{ht_{tri}}
         W_{ht} >= C_{ht}*(W_{struct} + W_{struct}*f_{ht})
     
     LandingGear
       l_n + z_{wing} + y_m*\tan(\gamma) >= l_m
       T = 2*y_m
       x_m >= x_n + B
       x_n >= 5
       \tan(\phi) = \tan(\phi_{min})
       (z_{CG} + l_m)^0*(y_m^2 + B^2)/(\Delta x_n*y_m*\tan(\psi))^2 <= 1
       \tan(\psi) <= \tan(\psi_{max})
       x_{up} - x_m <= l_m/\tan(\theta_{max})
       y_m >= l_m
       S_{sa} = 1/\eta_s*E_{land}/(L_m*\lambda_{LG})
       l_{oleo} = 2.5*S_{sa}
       d_{oleo} = 1.3*(4*\lambda_{LG}*L_m/n_{mg}/(PI*p_{oleo}))^0.5
       l_m >= l_{oleo} + d_{t_m}/2
       F_{w_m} = L_{w_m}*d_{t_m}/(1e+03 [N*in])
       W_{wa,m} = 1.2*F_{w_m}^0.609
       F_{w_n} = L_{w_n}*d_{t_n}/1e+03
       W_{wa,n} = 1.2*F_{w_n}^0.609
       L_{w_m} = L_m/(n_{mg}*n_{wps})
       L_{w_n} = L_n/n_{wps}
       d_{t_m} = 1.63*(L_{w_m}/4.44)^0.315
       w_{t_m} = 0.104*(L_{w_m}/4.44)^0.48
       d_{t_n} = 0.8*d_{t_m}
       w_{t_n} = 0.8*w_{t_m}
       W_{ms} >= 2PI*r_m*t_m*l_m*\rho_{st}*g
       N_s*\lambda_{LG}*L_m/n_{mg} <= \sigma_{y_c}*2PI*r_m*t_m
       W_{mw} = n_{wps}*W_{wa,m}
       W_{ns} >= 2PI*r_n*t_n*l_n*\rho_{st}*g
       \sigma_{y_c}*2PI*r_n*t_n >= N_s*(L_n + L_{n_{dyn}})
       W_{nw} >= n_{wps}*W_{wa,n}
       L_m <= 9.87*E*I_m/(K*l_m)^2
       I_m = PI*r_m^3*t_m
       L_n <= 9.87*E*I_n/(K*l_n)^2
       I_n = PI*r_n^3*t_n
       2*r_m/t_m <= 40
       2*r_m/t_n <= 40
       h_{hold} >= 2*w_{t_m} + 2*r_m
       0.8 >= 2*w_{t_n} + 2*r_n
       W_{mg} >= n_{mg}*(W_{ms} + W_{mw}*(1 + f_{add,m}))
       W_{ng} >= W_{ns} + W_{nw}*(1 + f_{add,n})
       W_{lg} >= C_{lg}*(W_{mg} + W_{ng})
       W_{lg}*x_{CG_{lg}} >= W_{ng}*x_n + W_{mg}*x_m
       x_m >= x_{CG_{lg}}
     c_{root} = c_0
     Mission1.Aircraft.Wing.WingBox.r_{w/c} = Mission1.Aircraft.Fuselage.r_{w/c}
     x_w = x_{wing}
     Mission1.Aircraft.Fuselage.N_{lift} = Mission1.Aircraft.Wing.WingBox.N_{lift}
     f_{L_{total/wing}}*L_{max} >= Mission1.Aircraft.Wing.WingBox.N_{lift}*W_{total, max} + L_{ht_{max}}
     W_{dry}[:] >= W_{fuse} + n_{eng}*W_{engsys} + W_{tail} + W_{wing} + W_{misc}
     W_{f_{total}}[:] + W_{dry}[:] + W_{payload}[:] <= W_{total}[:]
     W_{f_{total}}[:] + W_{dry}[:] + W_{payload}[:] <= W_{total}[:]
     W_{f_{total}}[:] >= W_{f_{primary}}[:] + f_{fuel_{res}}*W_{f_{primary}}[:]
     W_{f_{primary}}[:] >= W_{f_{climb}}[:] + W_{f_{cruise}}[:]
     W_{total}[:] <= W_{total, max}
     f_{wingfuel}*W_{f_{total}}[:]/FuelFrac <= W_{fuel_{wing}}
     W_{misc} >= W_{lg} + W_{hpesys}
     W_{hpesys} = f_{hpesys}*W_{total, max}
     x_n <= l_{nose}
     x_m >= x_{wing}
     \Delta x_{AC_{wing}} + x_{wing} >= x_m
     x_{hpesys} = 1.1*l_{nose}
     x_{misc}*W_{misc} >= x_{hpesys}*W_{hpesys}
     d_{nacelle} >= d_{f} + 2*t_{nacelle}
     E_{land} >= W_{total, max}/(2*g)*w_{ult}^2
     x_{up} = x_{shell2}
     L_n = W_{total, max}*\Delta x_m/B
     L_m = W_{total, max}*\Delta x_n/B
     L_{n_{dyn}} >= 0.31*(z_{CG} + l_m)/B*W_{total, max}
     y_{eng} >= y_m
     3*n_{vt}*Mission1.Aircraft.VerticalTail.WingBox.M_r*c_{root_{vt}}*(p_{\lambda_{vt}} - 1) >= n_{vt}*L_{vt_{max}}*b_{vt}*p_{\lambda_{vt}}
     V_{cone}*(1 + \lambda_{cone})*(PI + 4*\theta_{db}) >= n_{vt}*Mission1.Aircraft.VerticalTail.WingBox.M_r*c_{root_{vt}}/\tau_{cone}*(PI + 2*\theta_{db})*l_{cone}/R_{fuse}
     W_{tail} >= n_{vt}*W_{vt} + W_{ht}
     2*w_{fuse} >= SPR*w_{seat} + n_{aisle}*w_{aisle} + 2*w_{sys} + t_{db}
     B_{1v} = r_{M_v}*n_{vt}*L_{vt_{max}}/(w_{fuse}*\sigma_{M_v})
     m_{ratio}*(1 + 2/AR) = 1 + 2/AR_{ht}
     x_{CG_{ht}} <= l_{fuse}
     V_{ht} = S_{ht}*l_{ht}/(S*mac)
     L_{ht_{max}} >= 0.5*\rho_{T/O}*V_{ne}^2*S_{ht}*C_{L_{ht,max}}
     L_{vt_{max}} >= 0.5*\rho_{T/O}*V_{ne}^2*S_{vt}*C_{L_{vt,max}}
     x_{CG_{vt}} <= l_{fuse}
     V_{vt} = n_{vt}*S_{vt}*l_{vt}/(S*b)
     n_{vt}*0.5*\rho_{TO}*V_{land}^2*S_{vt}*l_{vt}*C_{L_{vt,yaw}} >= \dot{r}_{req}*I_{z, max}
     n_{vt}*L_{vt,EO}*l_{vt} >= T_e*y_{eng} + D_{wm}*y_{eng}
     D_{wm} >= 0.5*\rho_{TO}*V_1^2.0*A_{2}*C_{D_{wm}}
     I_{z}[:] >= I_{z_{wing}}[:] + I_{z_{tail}}[:] + I_{z_{fuse}}[:]
     I_{z}[:] <= I_{z, max}
     S_{nacelle} = r_{S_{nacelle}}*PI*0.25*d_{f}^2
     l_{nacelle} = 0.15*d_{f}*r_{S_{nacelle}}
     f_{S_{nacelle}} = S_{nacelle}*S^-1
     A_{inlet} = 0.4*S_{nacelle}
     A_{fancowl} = 0.2*S_{nacelle}
     A_{exh} = 0.4*S_{nacelle}
     A_{corecowl} = 3PI*d_{LPC}^2
       W_{nacelle} >= ((2.5 + 0.238*d_{f})*A_{inlet} + 1.9*A_{fancowl} + (2.5 + 0.0363*d_{f})*A_{exh} + 1.9*A_{corecowl})
       W_{eadd} = f_{eadd}*W_{engine}
     W_{pylon} >= (W_{nacelle} + W_{eadd} + W_{engine})*f_{pylon}
     W_{engsys} >= C_{engsys}*(W_{pylon} + W_{nacelle} + W_{eadd} + W_{engine})
     y_{eng} = 0.5*w_{fuse}
     (L_{max} - Mission1.Aircraft.Wing.WingBox.N_{lift}*(W_{wing} + f_{wingfuel}*W_{f_{total}}[:]))*b^2/(12*S)*(c_{root} + 2*c_{tip}) <= Mission1.Aircraft.Wing.WingBox.M_r*c_{root}
     A_{1h_{Land}} >= N_{land}*(W_{tail} + n_{eng}*W_{engsys} + W_{apu})/(h_{fuse}*\sigma_{bend})
     A_{1h_{MLF}} >= (Mission1.Aircraft.Fuselage.N_{lift}*(W_{tail} + n_{eng}*W_{engsys} + W_{apu}) + r_{M_h}*L_{ht_{max}})/(h_{fuse}*\sigma_{M_h})
     I_{z_{wing}}[:] >= (W_{fuel_{wing}} + W_{wing})/(S*9.81)*c_{root}*b^3.0*(0.0833 - (1 - \lambda)/16)
     I_{z_{tail}}[:] >= (W_{apu} + W_{vt} + n_{eng}*W_{engsys})*l_{vt}^2.0/9.81 + W_{ht}*l_{ht}^2.0/9.81
     I_{z_{fuse}}[:] >= (W_{fuse} + W_{payload_{max}})/l_{fuse}*(x_{wing}^3.0 + l_{vt}^3.0)/(3*9.81)
     x_{shell2} + l_{cone} >= x_{eng}
     x_{eng} >= x_{shell2} + 0.75*l_{cone}
     S_{floor} = 0.312*P_{floor}
     M_{floor} = 0.0352*P_{floor}*w_{floor}
     \Delta R_{fuse} = R_{fuse}*0.43/1.75
     b_{ht}/4*L_{ht_{rect}} + b_{ht}/3*L_{ht_{tri}} = b_{ht_{out}}*L_{ht_{max}}/2
     b_{ht_{out}} = 0.5*b_{ht} - w_{fuse}
     L_{ht_{rect}}*b_{ht}/4 + L_{ht_{tri}}*b_{ht}/6 - w_{fuse}*L_{ht_{max}}/2 <= Mission1.Aircraft.HorizontalTail.WingBox.M_r*c_{root_{ht}}
     M_{r_{out}}*c_{attach} >= L_{ht_{rect_{out}}}*0.5*b_{ht_{out}} + L_{ht_{tri_{out}}}*0.333*b_{ht_{out}}
     L_{shear} >= L_{ht_{rect_{out}}} + L_{ht_{tri_{out}}}
     c_{tip_{ht}} + (1 - \lambda_{ht})*2*b_{ht_{out}}/b_{ht}*c_{root_{ht}} = c_{attach}
     \pi_{M-fac} >= (0.5*(M_{r_{out}}*c_{attach} + Mission1.Aircraft.HorizontalTail.WingBox.M_r*c_{root_{ht}})*w_{fuse}/(0.5*M_{r_{out}}*c_{attach}*b_{ht_{out}}) + 1)*b_{ht_{out}}/(0.5*b_{ht})
 
 FlightSegment
   FlightState
       V[:] = V[:]
       a[:] = (\gamma[:]*R[:]*T_{atm}[:])^0.5
       V[:] = M[:]*a[:]
     
     Altitude
       h[:] = hft[:]
     
     Atmosphere
       (P_{atm}[:]/p_{sl}[:])^0.190222560396 = T_{atm}[:]/T_{sl}[:]
       \rho[:] = P_{atm}[:]/(R_{atm}[:]/M_{atm}[:]*T_{atm}[:])
       T_{sl}[:] = T_{atm}[:] + L_{atm}[:]*h[:]
       \mu[:] = C_1[:]*T_{atm}[:]^1.5/(6.64*T_s[:]^0.72)
   
   FlightP
     P_{excess}[:] + V[:]*D[:] <= V[:]*n_{eng}*F[:]
     RC[:] = P_{excess}[:]/W_{avg}[:]
     \theta[:]*V[:] = RC[:]
     dhft[:] = tmin[:]*RC[:]
     R_{segment}[:] = thr[:]*V[:]
       WingPerformance
         0.5*\rho[:]*V[:]^2*S*C_{L}[:] >= L_w[:] + \Delta L_{o}[:] + 2*\Delta L_{t}[:]
         \Delta L_{o}[:] = \eta_{o}[:]*f_{L_{o}}[:]*b/2*p_{o}[:]
         \Delta L_{t}[:] = f_{L_{t}}[:]*p_{o}[:]*c_{root}*taper^2
         (AR/\eta)^2*(1 + \tan(\Lambda)^2 - M[:]^2) + 8PI*AR/C_{L_{\alpha,w}}[:] = (2PI*AR/C_{L_{\alpha,w}}[:])^2
         C_{L}[:] = C_{L_{\alpha,w}}[:]*\alpha_w[:]
         \alpha_w[:] <= \alpha_{max,w}[:]
         D_{wing}[:] = 0.5*\rho[:]*V[:]^2*S*C_{d_w}[:]
         C_{d_w}[:] >= C_{D_{p_w}}[:] + C_{D_{i_w}}[:]
         C_{D_{i_w}}[:] >= TipReduct*C_{L}[:]^2/(PI*e*AR)
         Re_w[:] = \rho[:]*V[:]*mac/\mu[:]
         C_{D_{p_w}}[:]^1.6515 >= 1.61*(Re_w[:]/1e+03)^-0.550434*\tau^1.29151*(\cos(\Lambda)*M[:])^3.03609*C_{L}[:]^1.77743 + 0.0466*(Re_w[:]/1e+03)^-0.389048*\tau^0.784123*(\cos(\Lambda)*M[:])^-0.340157*C_{L}[:]^0.950763 + 191*(Re_w[:]/1e+03)^-0.218621*\tau^3.94654*(\cos(\Lambda)*M[:])^19.2524*C_{L}[:]^1.15233 + 2.82e-12*(Re_w[:]/1e+03)^1.18147*\tau^-1.75664*(\cos(\Lambda)*M[:])^0.10563*C_{L}[:]^-1.44114
       
       FuselagePerformance
         (no constraints)
       
       VerticalTailPerformance
         D_{vt}[:] >= 0.5*\rho[:]*V[:]^2*S_{vt}*C_{D_{vis}}[:]
         Re_{vt}[:] = \rho[:]*V[:]*\bar{c}_{vt}/\mu[:]
         C_{D_{vis}}[:]^1.18909 >= 2.44e-77*Re_{vt}[:]^-0.52841*\tau_{vt}^133.796*M[:]^1022.7 + 0.00304*Re_{vt}[:]^-0.409988*\tau_{vt}^1.22062*M[:]^1.55119 + 0.000197*Re_{vt}[:]^0.214479*\tau_{vt}^-0.0383195*M[:]^-0.137561 + 6.59e-50*Re_{vt}[:]^-0.498092*\tau_{vt}^1.55922*M[:]^-114.577
       
       HorizontalTailPerformance
         L_{ht}[:] = 0.5*\rho[:]*V[:]^2*S_{ht}*C_{L_{ht}}[:]
         C_{L_{ht}}[:] = C_{L_{\alpha,ht}}[:]*\alpha_{ht}[:]
         \alpha_{ht}[:] <= \alpha_{ht,max}
         C_{L_{\alpha,ht_0}}[:] = 6.28
         D_{ht}[:] = 0.5*\rho[:]*V[:]^2*S_{ht}*C_{D_{ht}}[:]
         C_{D_{ht}}[:] >= C_{D_{0,ht}}[:] + C_{L_{ht}}[:]^2/(PI*e_{ht}*AR_{ht})
         Re_{c_h}[:] = \rho[:]*V[:]*\bar{c}_{ht}/\mu[:]
         C_{D_{0,ht}}[:]^6.48983 >= 5.29e-20*Re_{c_h}[:]^0.900672*\tau_{ht}^0.912222*M[:]^8.64547 + 1.68e-28*Re_{c_h}[:]^0.350958*\tau_{ht}^6.29187*M[:]^10.2559 + 7.1e-25*Re_{c_h}[:]^1.39489*\tau_{ht}^1.96239*M[:]^0.567066 + 3.73e-14*Re_{c_h}[:]^-2.57406*\tau_{ht}^3.12793*M[:]^0.448159 + 1.44e-12*Re_{c_h}[:]^-3.91046*\tau_{ht}^4.66279*M[:]^7.68852
       W_{burn}[:] = W_{burn}[:]
       F_{fuel}[:] = F_{fuel}[:]
       \rho_{cabin}[:] = P_{cabin}[:]/(R[:]*T_{cabin}[:])
       P_{cabin}[:] = 7.5e+04
       T_{cabin}[:] = 297
       V[:] >= V_{stall}[:]
       W_{avg}[:] >= (W_{start}[:]*W_{end}[:])^0.5 + W_{buoy}[:]
       tmin[:] = thr[:]
       L_{fuse}[:] = (f_{L_{total/wing}} - 1)*L_w[:]
       L_{total}[:] = f_{L_{total/wing}}*L_w[:]
       L_{total}[:] >= W_{avg}[:] + L_{ht}[:]
       D_{fuse}[:] = 0.5*\rho[:]*V[:]^2*C_{D_{fuse}}[:]*l_{fuse}*R_{fuse}*M[:]^2/M_{fuseD}^2
       D[:] >= D_{reduct}*(D_{wing}[:] + D_{fuse}[:] + n_{vt}*D_{vt}[:] + D_{ht}[:] + n_{eng}*D_{nacelle}[:])
       C_D[:] = D[:]/(0.5*\rho[:]*V[:]^2*S)
       L/D[:] = W_{avg}[:]/D[:]
       W_{Load}[:] <= W_{Load_{max}}[:]
       W_{Load}[:] = 0.5*C_{L}[:]*S*\rho[:]*V[:]^2/S
       p_{o}[:] >= L_w[:]*c_{root}/S
       \eta_{o}[:] = w_{fuse}/(b/2)
       x_{AC}[:] <= x_{wing} + 0.25*\Delta x_{AC_{wing}} + x_{NP}[:]
       c_{m_{w}}[:] = 1.9
       x_{NP}[:]/mac/V_{ht}*(AR + 2)*(1 + 2/AR_{ht}) = (1 + 2/AR)*(AR - 2)
       x_{CG}[:] + \Delta x_{trail_{vt}} <= l_{fuse}
       x_{CG}[:] + 0.5*(\Delta x_{lead_{vt}} + \Delta x_{trail_{vt}}) <= x_{CG_{vt}}
       x_{CG}[:] + 0.5*(\Delta x_{lead_{ht}} + \Delta x_{trail_{ht}}) <= x_{CG_{ht}}
       C_{L_{\alpha,ht}}[:] + 2*C_{L_{\alpha,w}}[:]/(PI*AR)*\eta_{ht}*C_{L_{\alpha,ht_0}}[:] <= C_{L_{\alpha,ht_0}}[:]*\eta_{ht}
       AR_{ht} >= 4
       C_{L_{ht}}[:] >= 0.01
       SM[:] <= ([[x_{AC}[0,0] - x_{CG}[0,0]], [x_{AC}[1,0] - x_{CG}[1,0]], [x_{AC}[2,0] - x_{CG}[2,0]], [x_{AC}[3,0] - x_{CG}[3,0]], [x_{AC}[4,0] - x_{CG}[4,0]]])/mac
       SM[:] >= SM_{min}
       SM_{min} + \Delta x_{CG}/mac + c_{m_{w}}[:]/C_{L_{w,max}} <= V_{ht}*m_{ratio} + V_{ht}*C_{L_{ht,max}}/C_{L_{w,max}}
       x_{AC}[:]/mac <= x_{CG}[:]/mac + c_{m_{w}}[:]/C_{L}[:] + V_{ht}*C_{L_{ht}}[:]/C_{L}[:]
       R_{e_{nacelle}}[:] = \rho[:]*V[:]*l_{nacelle}/\mu[:]
       C_{f_{nacelle}}[:] = 0.279/R_{e_{nacelle}}[:]^0.2
       V_{nacelle}[:] = r_{v_{nacelle}}*V[:]
       V_{nacelle_ratio}[:] >= [[V_{nacelle}[0,0]*2/V[0,0] - V_2[0,0]/V[0,0]], [V_{nacelle}[1,0]*2/V[1,0] - V_2[1,0]/V[1,0]], [V_{nacelle}[2,0]*2/V[2,0] - V_2[2,0]/V[2,0]], [V_{nacelle}[3,0]*2/V[3,0] - V_2[3,0]/V[3,0]], [V_{nacelle}[4,0]*2/V[4,0] - V_2[4,0]/V[4,0]]]
       r_{v_{nsurf}}[:]^3.0 >= 0.25*(V_{nacelle_ratio}[:] + r_{v_{nacelle}})*(V_{nacelle_ratio}[:]^2.0 + r_{v_{nacelle}}^2.0)
       C_{d_{nacelle}}[:] = f_{S_{nacelle}}*C_{f_{nacelle}}[0]*r_{v_{nsurf}}[:]^3.0
       D_{nacelle}[:] = C_{d_{nacelle}}[:]*0.5*\rho[:]*V[:]^2.0*S
       \Delta x_{lead_{vt}} + b_{vt}/\tan(\Lambda_{vt}) + w_{fuse}/\tan(\Lambda_{ht}) + c_{root_{ht}} >= \Delta x_{trail_{ht}}
   M_2[:3] = M[:3]
   M_{2.5}[:3] = 0.6
   hold_{2}[:3] = 1.07164
   hold_{2.5}[:3] = 1.06372
   P_{excess}[:] + V[:]*D[:] <= V[:]*n_{eng}*F_{spec}[:]
   c1[:] = 1 + 0.201*M[:]^2.0
   M_2[3:] = M[3:]
   M_{2.5}[3:] = 0.6
   hold_{2}[3:] = 1.07164
   hold_{2.5}[3:] = 1.06372
Beginning signomial solve.
Using solver 'mosek'
Solving for 1768 variables.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Problem
  Name                   :                 
  Objective sense        : max             
  Type                   : GECO (general convex optimization problem)
  Constraints            : 1769            
  Cones                  : 0               
  Scalar variables       : 6131            
  Matrix variables       : 0               
  Integer variables      : 0               

Optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Freed constraints in eliminator : 476
Eliminator terminated.
Eliminator started.
Freed constraints in eliminator : 6
Eliminator terminated.
Eliminator - tries                  : 2                 time                   : 0.00            
Lin. dep.  - tries                  : 1                 time                   : 0.00            
Lin. dep.  - number                 : 0               
Presolve terminated. Time: 0.01    
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Problem
  Name                   :                 
  Objective sense        : max             
  Type                   : GECO (general convex optimization problem)
  Constraints            : 1769            
  Cones                  : 0               
  Scalar variables       : 6131            
  Matrix variables       : 0               
  Integer variables      : 0               

Optimizer  - threads                : 8               
Optimizer  - solved problem         : the primal      
Optimizer  - Constraints            : 878
Optimizer  - Cones                  : 0
Optimizer  - Scalar variables       : 3466              conic                  : 0               
Optimizer  - Semi-definite variables: 0                 scalarized             : 0               
Factor     - setup time             : 0.03              dense det. time        : 0.00            
Factor     - ML order time          : 0.00              GP order time          : 0.02            
Factor     - nonzeros before factor : 1.49e+04          after factor           : 1.55e+05        
Factor     - dense dim.             : 0                 flops                  : 3.17e+07        
Factor     - GP saved nzs           : 3.36e+04          GP saved flops         : 9.32e+05        
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+03  3.0e+03  1.2e+05  0.00e+00   -1.223083000e+05  2.000000000e+00   1.0e+00  0.04  
1   1.6e+03  2.0e+03  8.4e+04  -9.71e-01  -1.214169755e+05  2.778937242e+00   6.8e-01  0.05  
2   8.2e+02  1.1e+03  4.4e+04  -9.56e-01  -1.189685922e+05  5.116623673e+00   3.6e-01  0.06  
3   2.9e+02  3.8e+02  1.6e+04  -9.15e-01  -1.102962345e+05  2.170095046e+01   1.3e-01  0.06  
4   2.9e+02  3.8e+02  1.6e+04  -7.69e-01  -1.083159562e+05  1.743975991e+03   1.3e-01  0.07  
5   1.1e+02  1.5e+02  6.0e+03  -7.60e-01  -8.473424866e+04  6.747984694e+03   5.0e-02  0.08  
6   3.8e+01  4.9e+01  2.0e+03  -4.14e-01  -4.537005734e+04  1.080379792e+04   1.7e-02  0.09  
7   2.0e+01  2.7e+01  1.1e+03  2.54e-01   -2.836625497e+04  7.045474557e+03   9.0e-03  0.10  
8   9.4e+00  1.2e+01  5.0e+02  5.72e-01   -1.387003547e+04  4.245870985e+03   4.2e-03  0.11  
9   4.7e+00  6.2e+00  2.6e+02  8.29e-01   -6.980052804e+03  2.517162242e+03   2.1e-03  0.12  
10  1.4e+00  1.9e+00  7.8e+01  9.33e-01   -2.014621384e+03  9.508454525e+02   6.5e-04  0.13  
11  6.4e-01  8.4e-01  3.5e+01  9.93e-01   -6.678945647e+02  6.594956157e+02   2.9e-04  0.14  
12  4.8e-01  6.4e-01  2.7e+01  9.96e-01   -4.499444859e+02  5.609447906e+02   2.2e-04  0.15  
13  3.5e-01  7.8e-01  1.9e+01  9.80e-01   -2.667764900e+02  4.766170471e+02   1.6e-04  0.16  
14  1.7e-01  3.9e-01  9.5e+00  9.96e-01   3.398903189e-01   3.641145682e+02   8.0e-05  0.16  
15  5.8e-02  1.6e-01  3.3e+00  9.94e-01   1.652792674e+02   2.911850936e+02   2.8e-05  0.17  
16  3.3e-02  1.4e-01  1.9e+00  1.00e+00   2.032349806e+02   2.745517815e+02   1.6e-05  0.19  
17  4.6e-03  2.1e-01  2.9e-01  1.00e+00   2.458601979e+02   2.569052088e+02   2.6e-06  0.20  
18  1.3e-03  1.4e-01  8.6e-02  1.00e+00   2.513276389e+02   2.546006416e+02   7.8e-07  0.21  
19  4.6e-04  1.1e-01  3.0e-02  1.00e+00   2.528755707e+02   2.540040947e+02   2.7e-07  0.22  
20  1.8e-04  9.1e-02  1.2e-02  1.00e+00   2.533597014e+02   2.538150010e+02   1.1e-07  0.23  
21  1.7e-04  8.2e-02  1.1e-02  1.00e+00   2.533933866e+02   2.538031620e+02   9.9e-08  0.24  
22  1.5e-04  7.5e-02  9.7e-03  1.00e+00   2.534228246e+02   2.537915997e+02   8.9e-08  0.25  
23  1.3e-04  6.8e-02  8.7e-03  1.00e+00   2.534493464e+02   2.537812275e+02   8.0e-08  0.26  
24  1.2e-04  6.2e-02  7.8e-03  1.00e+00   2.534731930e+02   2.537718722e+02   7.2e-08  0.26  
25  1.1e-04  5.6e-02  7.1e-03  1.00e+00   2.534946426e+02   2.537634424e+02   6.5e-08  0.28  
26  9.8e-05  5.2e-02  6.4e-03  1.00e+00   2.535139347e+02   2.537558453e+02   5.8e-08  0.29  
27  8.8e-05  4.7e-02  5.7e-03  1.00e+00   2.535312881e+02   2.537490000e+02   5.3e-08  0.30  
28  7.9e-05  4.3e-02  5.1e-03  1.00e+00   2.535468982e+02   2.537428327e+02   4.7e-08  0.30  
29  7.1e-05  4.0e-02  4.6e-03  1.00e+00   2.535609408e+02   2.537372768e+02   4.3e-08  0.31  
30  6.4e-05  3.6e-02  4.2e-03  1.00e+00   2.535735736e+02   2.537322719e+02   3.8e-08  0.32  
31  5.8e-05  3.4e-02  3.8e-03  1.00e+00   2.535849385e+02   2.537277637e+02   3.5e-08  0.33  
32  5.2e-05  3.1e-02  3.4e-03  1.00e+00   2.535951630e+02   2.537237031e+02   3.1e-08  0.34  
33  4.7e-05  2.9e-02  3.0e-03  1.00e+00   2.536043618e+02   2.537200458e+02   2.8e-08  0.35  
34  4.2e-05  2.7e-02  2.7e-03  1.00e+00   2.536126378e+02   2.537167517e+02   2.5e-08  0.36  
35  3.8e-05  2.5e-02  2.5e-03  1.00e+00   2.536200838e+02   2.537137851e+02   2.3e-08  0.37  
36  3.4e-05  2.3e-02  2.2e-03  1.00e+00   2.536267832e+02   2.537111133e+02   2.0e-08  0.38  
37  3.1e-05  2.1e-02  2.0e-03  1.00e+00   2.536328109e+02   2.537087072e+02   1.8e-08  0.40  
38  2.8e-05  2.0e-02  1.8e-03  1.00e+00   2.536382344e+02   2.537065405e+02   1.7e-08  0.41  
39  2.5e-05  1.9e-02  1.6e-03  1.00e+00   2.536431143e+02   2.537045893e+02   1.5e-08  0.41  
40  2.2e-05  1.8e-02  1.5e-03  1.00e+00   2.536475051e+02   2.537028323e+02   1.3e-08  0.42  
41  2.0e-05  1.7e-02  1.3e-03  1.00e+00   2.536514561e+02   2.537012503e+02   1.2e-08  0.44  
42  1.8e-05  1.6e-02  1.2e-03  1.00e+00   2.536550112e+02   2.536998258e+02   1.1e-08  0.45  
43  1.6e-05  1.5e-02  1.1e-03  1.00e+00   2.536582102e+02   2.536985432e+02   9.8e-09  0.46  
44  1.5e-05  1.4e-02  9.5e-04  1.00e+00   2.536610889e+02   2.536973885e+02   8.8e-09  0.48  
45  1.3e-05  1.4e-02  8.6e-04  1.00e+00   2.536636793e+02   2.536963489e+02   7.9e-09  0.49  
46  1.2e-05  1.3e-02  7.7e-04  1.00e+00   2.536660103e+02   2.536954129e+02   7.1e-09  0.50  
47  1.1e-05  1.2e-02  7.0e-04  1.00e+00   2.536681080e+02   2.536945703e+02   6.4e-09  0.51  
48  9.6e-06  1.2e-02  6.3e-04  1.00e+00   2.536699957e+02   2.536938118e+02   5.8e-09  0.52  
49  8.7e-06  1.2e-02  5.6e-04  1.00e+00   2.536716945e+02   2.536931290e+02   5.2e-09  0.53  
50  7.8e-06  1.1e-02  5.1e-04  1.00e+00   2.536732232e+02   2.536925143e+02   4.7e-09  0.54  
51  7.0e-06  1.1e-02  4.6e-04  1.00e+00   2.536745990e+02   2.536919610e+02   4.2e-09  0.55  
52  6.3e-06  1.0e-02  4.1e-04  1.00e+00   2.536758371e+02   2.536914629e+02   3.8e-09  0.56  
53  5.7e-06  1.0e-02  3.7e-04  1.00e+00   2.536769513e+02   2.536910146e+02   3.4e-09  0.57  
54  5.1e-06  9.9e-03  3.3e-04  1.00e+00   2.536779540e+02   2.536906110e+02   3.1e-09  0.58  
55  4.6e-06  9.7e-03  3.0e-04  1.00e+00   2.536788564e+02   2.536902477e+02   2.8e-09  0.59  
56  4.1e-06  9.5e-03  2.7e-04  1.00e+00   2.536796685e+02   2.536899207e+02   2.5e-09  0.61  
57  3.7e-06  9.3e-03  2.4e-04  1.00e+00   2.536803993e+02   2.536896263e+02   2.2e-09  0.61  
58  3.4e-06  9.1e-03  2.2e-04  1.00e+00   2.536810570e+02   2.536893613e+02   2.0e-09  0.63  
59  3.0e-06  8.9e-03  2.0e-04  1.00e+00   2.536816489e+02   2.536891228e+02   1.8e-09  0.64  
60  1.2e-06  3.4e-03  7.6e-05  1.00e+00   2.536849211e+02   2.536878032e+02   7.0e-10  0.65  
61  1.0e-06  3.1e-03  6.8e-05  1.00e+00   2.536851269e+02   2.536877209e+02   6.3e-10  0.66  
62  3.7e-07  1.1e-03  2.4e-05  1.00e+00   2.536863131e+02   2.536872421e+02   2.2e-10  0.68  
63  3.4e-07  1.0e-03  2.2e-05  1.00e+00   2.536863794e+02   2.536872155e+02   2.0e-10  0.69  
64  3.0e-07  9.0e-04  2.0e-05  1.00e+00   2.536864389e+02   2.536871914e+02   1.8e-10  0.70  
65  2.7e-07  8.1e-04  1.8e-05  1.00e+00   2.536864925e+02   2.536871697e+02   1.6e-10  0.71  
66  2.5e-07  7.3e-04  1.6e-05  1.00e+00   2.536865407e+02   2.536871503e+02   1.5e-10  0.71  
67  2.2e-07  6.6e-04  1.4e-05  1.00e+00   2.536865841e+02   2.536871327e+02   1.3e-10  0.73  
68  2.0e-07  5.9e-04  1.3e-05  1.00e+00   2.536866232e+02   2.536871169e+02   1.2e-10  0.74  
69  1.8e-07  5.3e-04  1.2e-05  1.00e+00   2.536866583e+02   2.536871027e+02   1.1e-10  0.75  
70  1.6e-07  4.8e-04  1.1e-05  1.00e+00   2.536866900e+02   2.536870899e+02   9.7e-11  0.75  
71  1.5e-07  4.3e-04  9.5e-06  1.00e+00   2.536867185e+02   2.536870784e+02   8.7e-11  0.76  
72  1.3e-07  3.9e-04  8.5e-06  1.00e+00   2.536867441e+02   2.536870680e+02   7.8e-11  0.77  
73  1.2e-07  3.5e-04  7.7e-06  1.00e+00   2.536867672e+02   2.536870587e+02   7.1e-11  0.78  
74  1.1e-07  3.1e-04  6.9e-06  1.00e+00   2.536867879e+02   2.536870503e+02   6.3e-11  0.79  
75  9.5e-08  2.8e-04  6.2e-06  1.00e+00   2.536868066e+02   2.536870427e+02   5.7e-11  0.80  
76  8.6e-08  2.5e-04  5.6e-06  1.00e+00   2.536868234e+02   2.536870359e+02   5.1e-11  0.81  
77  7.7e-08  2.3e-04  5.0e-06  1.00e+00   2.536868385e+02   2.536870298e+02   4.6e-11  0.82  
78  6.9e-08  2.1e-04  4.5e-06  1.00e+00   2.536868521e+02   2.536870243e+02   4.2e-11  0.83  
79  6.3e-08  1.9e-04  4.1e-06  1.00e+00   2.536868644e+02   2.536870193e+02   3.7e-11  0.84  
80  5.6e-08  1.7e-04  3.7e-06  1.00e+00   2.536868754e+02   2.536870149e+02   3.4e-11  0.86  
81  5.1e-08  1.5e-04  3.3e-06  1.00e+00   2.536868854e+02   2.536870109e+02   3.0e-11  0.86  
82  4.6e-08  1.3e-04  3.0e-06  1.00e+00   2.536868943e+02   2.536870072e+02   2.7e-11  0.87  
83  4.1e-08  1.2e-04  2.7e-06  1.00e+00   2.536869023e+02   2.536870040e+02   2.5e-11  0.89  
84  3.7e-08  1.1e-04  2.4e-06  1.00e+00   2.536869096e+02   2.536870010e+02   2.2e-11  0.90  
85  3.3e-08  9.8e-05  2.2e-06  1.00e+00   2.536869161e+02   2.536869984e+02   2.0e-11  0.90  
86  3.0e-08  8.8e-05  1.9e-06  1.00e+00   2.536869219e+02   2.536869960e+02   1.8e-11  0.91  
87  2.7e-08  8.0e-05  1.8e-06  1.00e+00   2.536869272e+02   2.536869939e+02   1.6e-11  0.92  
88  2.4e-08  7.2e-05  1.6e-06  1.00e+00   2.536869319e+02   2.536869920e+02   1.5e-11  0.94  
89  2.2e-08  6.5e-05  1.4e-06  1.00e+00   2.536869362e+02   2.536869902e+02   1.3e-11  0.94  
90  2.0e-08  5.8e-05  1.3e-06  1.00e+00   2.536869401e+02   2.536869887e+02   1.2e-11  0.95  
91  1.8e-08  5.2e-05  1.1e-06  1.00e+00   2.536869435e+02   2.536869873e+02   1.1e-11  0.96  
92  1.6e-08  4.7e-05  1.0e-06  1.00e+00   2.536869466e+02   2.536869860e+02   9.5e-12  0.97  
93  1.4e-08  4.2e-05  9.3e-07  1.00e+00   2.536869494e+02   2.536869849e+02   8.6e-12  0.98  
94  1.3e-08  3.8e-05  8.4e-07  1.00e+00   2.536869520e+02   2.536869839e+02   7.7e-12  0.99  
95  1.2e-08  3.4e-05  7.5e-07  1.00e+00   2.536869542e+02   2.536869829e+02   6.9e-12  1.00  
96  1.0e-08  3.1e-05  6.8e-07  1.00e+00   2.536869563e+02   2.536869821e+02   6.2e-12  1.01  
97  9.4e-09  2.8e-05  6.1e-07  1.00e+00   2.536869581e+02   2.536869814e+02   5.6e-12  1.02  
Optimizer terminated. Time: 1.02    

solsta = 1, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : OPTIMAL
  Primal.  obj: 2.5368695810e+02    nrm: 4e+01    Viol.  con: 2e-07    var: 0e+00  
  Dual.    obj: 2.5368698136e+02    nrm: 8e+02    Viol.  con: 0e+00    var: 2e-04  
* End solution on dual form. *
Transforming to primal solution.
Solving took 1.04 seconds.
Using solver 'mosek'
Solving for 1768 variables.
MOSEK warning 710: #1 (nearly) zero elements are specified in sparse col '' (450) of matrix 'A'.
Number of Hessian non-zeros: 2054
* Solving exponential optimization problem on dual form. *
* The following log information refers to the solution of the dual problem. *
Problem
  Name                   :                 
  Objective sense        : max             
  Type                   : GECO (general convex optimization problem)
  Constraints            : 1769            
  Cones                  : 0               
  Scalar variables       : 6131            
  Matrix variables       : 0               
  Integer variables      : 0               

Optimizer started.
Presolve started.
Linear dependency checker started.
Linear dependency checker terminated.
Eliminator started.
Freed constraints in eliminator : 476
Eliminator terminated.
Eliminator started.
Freed constraints in eliminator : 6
Eliminator terminated.
Eliminator - tries                  : 2                 time                   : 0.00            
Lin. dep.  - tries                  : 1                 time                   : 0.00            
Lin. dep.  - number                 : 0               
Presolve terminated. Time: 0.01    
Matrix reordering started.
Local matrix reordering started.
Local matrix reordering terminated.
Matrix reordering terminated.
Problem
  Name                   :                 
  Objective sense        : max             
  Type                   : GECO (general convex optimization problem)
  Constraints            : 1769            
  Cones                  : 0               
  Scalar variables       : 6131            
  Matrix variables       : 0               
  Integer variables      : 0               

Optimizer  - threads                : 8               
Optimizer  - solved problem         : the primal      
Optimizer  - Constraints            : 879
Optimizer  - Cones                  : 0
Optimizer  - Scalar variables       : 3468              conic                  : 0               
Optimizer  - Semi-definite variables: 0                 scalarized             : 0               
Factor     - setup time             : 0.03              dense det. time        : 0.00            
Factor     - ML order time          : 0.00              GP order time          : 0.02            
Factor     - nonzeros before factor : 1.49e+04          after factor           : 1.56e+05        
Factor     - dense dim.             : 0                 flops                  : 3.19e+07        
Factor     - GP saved nzs           : 3.36e+04          GP saved flops         : 9.32e+05        
ITE PFEAS    DFEAS    GFEAS    PRSTATUS   POBJ              DOBJ              MU       TIME  
0   2.3e+03  3.0e+03  1.2e+05  0.00e+00   -1.219705586e+05  2.000000000e+00   1.0e+00  0.04  
1   1.6e+03  2.1e+03  8.4e+04  -9.71e-01  -1.211031020e+05  2.765533663e+00   6.9e-01  0.05  
2   7.8e+02  1.0e+03  4.2e+04  -9.57e-01  -1.183621946e+05  5.379607955e+00   3.4e-01  0.05  
3   2.9e+02  3.8e+02  1.6e+04  -9.11e-01  -1.100271642e+05  2.234927157e+01   1.3e-01  0.06  
4   2.9e+02  3.8e+02  1.6e+04  -7.69e-01  -1.081090538e+05  1.691198782e+03   1.3e-01  0.07  
5   1.2e+02  1.6e+02  6.6e+03  -7.61e-01  -8.730500726e+04  6.170178286e+03   5.4e-02  0.08  
6   3.9e+01  5.1e+01  2.1e+03  -4.57e-01  -4.641557494e+04  1.102767695e+04   1.7e-02  0.09  
7   2.3e+01  3.0e+01  1.2e+03  2.33e-01   -3.095362448e+04  7.311515434e+03   1.0e-02  0.10  
8   9.3e+00  1.2e+01  5.0e+02  5.26e-01   -1.383958025e+04  4.015287293e+03   4.1e-03  0.11  
9   6.1e+00  7.9e+00  3.2e+02  8.28e-01   -9.007628044e+03  2.852555853e+03   2.7e-03  0.12  
10  2.1e+00  2.7e+00  1.1e+02  9.03e-01   -3.047258165e+03  1.195224977e+03   9.4e-04  0.14  
11  1.6e+00  2.0e+00  8.5e+01  9.77e-01   -2.209373100e+03  9.993568394e+02   7.0e-04  0.14  
12  1.0e+00  1.4e+00  5.6e+01  9.78e-01   -1.412745572e+03  7.362078430e+02   4.7e-04  0.15  
13  4.1e-01  7.0e-01  2.2e+01  9.86e-01   -4.532334049e+02  3.966890953e+02   1.9e-04  0.16  
14  2.4e-01  4.3e-01  1.3e+01  1.00e+00   -1.803313668e+02  3.208030866e+02   1.1e-04  0.17  
15  7.5e-02  4.3e-01  4.2e+00  1.00e+00   5.907667930e+01   2.194258788e+02   3.6e-05  0.18  
16  2.7e-02  1.8e-01  1.5e+00  1.01e+00   1.312032677e+02   1.889662771e+02   1.3e-05  0.19  
17  8.9e-03  1.1e-01  5.2e-01  1.01e+00   1.583140177e+02   1.780792062e+02   4.6e-06  0.20  
18  3.5e-03  9.8e-02  2.1e-01  1.01e+00   1.668085083e+02   1.746024948e+02   1.8e-06  0.21  
19  9.2e-04  1.2e-01  5.6e-02  1.01e+00   1.708677782e+02   1.729897946e+02   5.1e-07  0.21  
20  3.1e-04  1.0e-01  1.9e-02  1.00e+00   1.718819279e+02   1.726108386e+02   1.8e-07  0.23  
21  1.1e-04  1.0e-01  7.1e-03  9.98e-01   1.722145287e+02   1.724820216e+02   6.5e-08  0.24  
22  3.7e-05  1.0e-01  2.4e-03  9.99e-01   1.723408997e+02   1.724300134e+02   2.2e-08  0.25  
23  3.4e-05  9.2e-02  2.1e-03  1.00e+00   1.723477057e+02   1.724279165e+02   1.9e-08  0.26  
24  3.0e-05  8.4e-02  1.9e-03  1.00e+00   1.723534337e+02   1.724256231e+02   1.8e-08  0.27  
25  2.7e-05  7.6e-02  1.7e-03  1.00e+00   1.723585613e+02   1.724235306e+02   1.6e-08  0.28  
26  2.5e-05  7.0e-02  1.6e-03  1.00e+00   1.723631653e+02   1.724216358e+02   1.4e-08  0.29  
27  2.2e-05  6.3e-02  1.4e-03  1.00e+00   1.723673034e+02   1.724199249e+02   1.3e-08  0.30  
28  2.0e-05  5.8e-02  1.3e-03  1.00e+00   1.723710236e+02   1.724183812e+02   1.2e-08  0.31  
29  1.8e-05  5.3e-02  1.1e-03  1.00e+00   1.723743688e+02   1.724169890e+02   1.0e-08  0.32  
30  1.6e-05  4.8e-02  1.0e-03  1.00e+00   1.723773770e+02   1.724157339e+02   9.3e-09  0.33  
31  1.5e-05  4.4e-02  9.2e-04  1.00e+00   1.723800823e+02   1.724146024e+02   8.4e-09  0.34  
32  1.3e-05  4.1e-02  8.2e-04  1.00e+00   1.723825154e+02   1.724135826e+02   7.6e-09  0.35  
33  1.2e-05  3.7e-02  7.4e-04  1.00e+00   1.723847038e+02   1.724126634e+02   6.8e-09  0.36  
34  1.1e-05  3.4e-02  6.7e-04  1.00e+00   1.723866721e+02   1.724118351e+02   6.1e-09  0.36  
35  9.5e-06  3.2e-02  6.0e-04  1.00e+00   1.723884426e+02   1.724110887e+02   5.5e-09  0.38  
36  8.6e-06  2.9e-02  5.4e-04  1.00e+00   1.723900351e+02   1.724104163e+02   5.0e-09  0.39  
37  7.7e-06  2.7e-02  4.9e-04  1.00e+00   1.723914678e+02   1.724098104e+02   4.5e-09  0.40  
38  6.9e-06  2.5e-02  4.4e-04  1.00e+00   1.723927565e+02   1.724092646e+02   4.0e-09  0.41  
39  6.3e-06  2.4e-02  3.9e-04  1.00e+00   1.723939159e+02   1.724087729e+02   3.6e-09  0.42  
40  5.6e-06  2.2e-02  3.5e-04  1.00e+00   1.723949589e+02   1.724083301e+02   3.3e-09  0.44  
41  5.1e-06  2.1e-02  3.2e-04  1.00e+00   1.723958973e+02   1.724079312e+02   2.9e-09  0.45  
42  4.6e-06  1.9e-02  2.9e-04  1.00e+00   1.723967416e+02   1.724075719e+02   2.6e-09  0.46  
43  4.1e-06  1.8e-02  2.6e-04  1.00e+00   1.723975012e+02   1.724072484e+02   2.4e-09  0.47  
44  3.7e-06  1.7e-02  2.3e-04  1.00e+00   1.723981846e+02   1.724069570e+02   2.1e-09  0.49  
45  3.3e-06  1.6e-02  2.1e-04  1.00e+00   1.723987995e+02   1.724066946e+02   1.9e-09  0.50  
46  3.0e-06  1.5e-02  1.9e-04  1.00e+00   1.723993528e+02   1.724064584e+02   1.7e-09  0.50  
47  2.7e-06  1.5e-02  1.7e-04  1.00e+00   1.723998506e+02   1.724062456e+02   1.6e-09  0.52  
48  2.4e-06  1.4e-02  1.5e-04  1.00e+00   1.724002985e+02   1.724060540e+02   1.4e-09  0.53  
49  2.2e-06  1.3e-02  1.4e-04  1.00e+00   1.724007016e+02   1.724058815e+02   1.3e-09  0.54  
50  2.0e-06  1.3e-02  1.2e-04  1.00e+00   1.724010643e+02   1.724057262e+02   1.1e-09  0.55  
51  1.8e-06  1.2e-02  1.1e-04  1.00e+00   1.724013906e+02   1.724055863e+02   1.0e-09  0.56  
52  1.6e-06  1.2e-02  1.0e-04  1.00e+00   1.724016843e+02   1.724054604e+02   9.2e-10  0.58  
53  1.4e-06  1.1e-02  9.0e-05  1.00e+00   1.724019485e+02   1.724053470e+02   8.3e-10  0.59  
54  1.3e-06  1.1e-02  8.1e-05  1.00e+00   1.724021863e+02   1.724052450e+02   7.4e-10  0.60  
55  1.2e-06  1.1e-02  7.3e-05  1.00e+00   1.724024003e+02   1.724051531e+02   6.7e-10  0.60  
56  1.0e-06  1.0e-02  6.6e-05  1.00e+00   1.724025928e+02   1.724050703e+02   6.0e-10  0.62  
57  9.4e-07  1.0e-02  5.9e-05  1.00e+00   1.724027661e+02   1.724049959e+02   5.4e-10  0.63  
58  8.4e-07  9.8e-03  5.3e-05  1.00e+00   1.724029220e+02   1.724049288e+02   4.9e-10  0.64  
59  7.6e-07  9.6e-03  4.8e-05  1.00e+00   1.724030623e+02   1.724048684e+02   4.4e-10  0.65  
60  6.8e-07  9.4e-03  4.3e-05  1.00e+00   1.724031886e+02   1.724048141e+02   4.0e-10  0.66  
61  6.2e-07  9.2e-03  3.9e-05  1.00e+00   1.724033022e+02   1.724047651e+02   3.6e-10  0.66  
62  5.5e-07  9.1e-03  3.5e-05  1.00e+00   1.724034044e+02   1.724047211e+02   3.2e-10  0.68  
63  5.0e-07  8.9e-03  3.1e-05  1.00e+00   1.724034964e+02   1.724046814e+02   2.9e-10  0.69  
64  4.5e-07  8.8e-03  2.8e-05  1.00e+00   1.724035792e+02   1.724046457e+02   2.6e-10  0.70  
65  4.0e-07  8.7e-03  2.5e-05  1.00e+00   1.724036537e+02   1.724046135e+02   2.3e-10  0.71  
66  3.6e-07  8.6e-03  2.3e-05  1.00e+00   1.724037207e+02   1.724045846e+02   2.1e-10  0.73  
67  3.3e-07  8.5e-03  2.1e-05  1.00e+00   1.724037810e+02   1.724045585e+02   1.9e-10  0.74  
68  2.9e-07  8.4e-03  1.9e-05  1.00e+00   1.724038353e+02   1.724045351e+02   1.7e-10  0.75  
69  2.7e-07  8.3e-03  1.7e-05  1.00e+00   1.724038842e+02   1.724045140e+02   1.5e-10  0.76  
70  2.4e-07  8.2e-03  1.5e-05  1.00e+00   1.724039281e+02   1.724044949e+02   1.4e-10  0.77  
71  2.1e-07  8.1e-03  1.4e-05  1.00e+00   1.724039677e+02   1.724044778e+02   1.2e-10  0.78  
72  1.9e-07  8.1e-03  1.2e-05  1.00e+00   1.724040033e+02   1.724044624e+02   1.1e-10  0.79  
73  1.7e-07  8.0e-03  1.1e-05  1.00e+00   1.724040353e+02   1.724044485e+02   1.0e-10  0.80  
74  1.6e-07  8.0e-03  9.9e-06  9.99e-01   1.724040642e+02   1.724044360e+02   9.0e-11  0.81  
75  1.4e-07  7.9e-03  8.9e-06  1.00e+00   1.724040901e+02   1.724044248e+02   8.1e-11  0.82  
76  1.3e-07  7.9e-03  8.0e-06  1.00e+00   1.724041135e+02   1.724044147e+02   7.3e-11  0.83  
77  1.1e-07  7.8e-03  7.2e-06  1.00e+0E
======================================================================
ERROR [32.960s]: test_SPaircraft_py_mosek (gpkit.tests.from_paths.TestFiles)
----------------------------------------------------------------------
Traceback (most recent call last):
  File "/Users/jenkins/workspace/gpkit_ResearchModel_SPaircraft_PR/mosek/gpkit/gpkit/tests/helpers.py", line 64, in test
    testfn(name, import_dict, path)(self)
  File "/Users/jenkins/workspace/gpkit_ResearchModel_SPaircraft_PR/mosek/gpkit/gpkit/tests/from_paths.py", line 51, in <lambda>
    lambda self: getattr(self, name)()))  # pylint:disable=undefined-variable
  File "/Users/jenkins/workspace/gpkit_ResearchModel_SPaircraft_PR/mosek/gpkit/gpkit/tests/from_paths.py", line 40, in test_fn
    mod.test()
  File "SPaircraft.py", line 89, in test
    sol = optimize_aircraft(m, substitutions, fixedBPR, pRatOpt, mutategparg)
  File "SPaircraft.py", line 64, in optimize_aircraft
    sol = m_relax.localsolve(verbosity=4, iteration_limit=200, reltol=0.01, mutategp=mutategparg, x0 = x0)
  File "/Users/jenkins/workspace/gpkit_ResearchModel_SPaircraft_PR/mosek/gpkit/gpkit/constraints/prog_factories.py", line 124, in solvefn
    result = progsolve(solver, verbosity, **kwargs)
  File "/Users/jenkins/workspace/gpkit_ResearchModel_SPaircraft_PR/mosek/gpkit/gpkit/constraints/sgp.py", line 149, in localsolve
    feas_constrs, None)
  File "/Users/jenkins/workspace/gpkit_ResearchModel_SPaircraft_PR/mosek/gpkit/gpkit/constraints/gp.py", line 112, in __init__
    + boundstrs)
ValueError: Geometric Program is not fully bounded:
  Mission1.Aircraft.Engine.EngineConstants.Relax1.R has no lower bound
  Mission1.Aircraft.Engine.EngineConstants.Relax1.g has no lower bound

----------------------------------------------------------------------
Ran 1 test in 32.961s

FAILED (errors=1)

Generating XML reports...
0   1.724041344e+02   1.724044056e+02   6.6e-11  0.84  
78  1.0e-07  7.8e-03  6.5e-06  1.00e+00   1.724041534e+02   1.724043974e+02   5.9e-11  0.85  
79  9.2e-08  7.0e-03  5.8e-06  1.01e+00   1.724041707e+02   1.724043898e+02   5.4e-11  0.86  
80  8.3e-08  6.3e-03  5.2e-06  9.98e-01   1.724041860e+02   1.724043831e+02   4.8e-11  0.87  
81  7.5e-08  5.7e-03  4.7e-06  9.95e-01   1.724041998e+02   1.724043771e+02   4.3e-11  0.88  
82  6.8e-08  5.1e-03  4.3e-06  9.94e-01   1.724042122e+02   1.724043717e+02   3.9e-11  0.89  
83  6.1e-08  4.6e-03  3.8e-06  9.99e-01   1.724042233e+02   1.724043669e+02   3.5e-11  0.90  
84  5.5e-08  4.1e-03  3.4e-06  9.99e-01   1.724042333e+02   1.724043626e+02   3.2e-11  0.91  
85  4.9e-08  3.7e-03  3.1e-06  9.94e-01   1.724042423e+02   1.724043586e+02   2.8e-11  0.91  
86  4.5e-08  3.4e-03  2.8e-06  9.91e-01   1.724042504e+02   1.724043551e+02   2.6e-11  0.93  
87  4.0e-08  3.0e-03  2.5e-06  9.74e-01   1.724042578e+02   1.724043519e+02   2.3e-11  0.94  
88  3.7e-08  2.7e-03  2.3e-06  9.78e-01   1.724042644e+02   1.724043489e+02   2.1e-11  0.95  
89  3.2e-08  2.4e-03  2.0e-06  1.01e+00   1.724042705e+02   1.724043464e+02   1.9e-11  0.96  
90  3.0e-08  2.2e-03  1.8e-06  1.05e+00   1.724042770e+02   1.724043434e+02   1.7e-11  0.97  
91  2.7e-08  2.0e-03  1.6e-06  9.74e-01   1.724042816e+02   1.724043414e+02   1.6e-11  0.98  
92  2.6e-08  1.8e-03  1.5e-06  1.01e+00   1.724042860e+02   1.724043393e+02   1.4e-11  0.99  
93  2.5e-08  1.6e-03  1.3e-06  9.93e-01   1.724042898e+02   1.724043376e+02   1.3e-11  1.00  
94  5.6e-08  2.3e-04  1.9e-07  7.69e-01   1.724043192e+02   1.724043264e+02   2.2e-12  1.01  
95  2.7e-08  2.3e-04  1.9e-07  -1.73e+00  1.724043193e+02   1.724043245e+02   2.0e-12  1.02  
96  4.0e-08  2.3e-04  2.1e-07  1.00e+00   1.724043188e+02   1.724043245e+02   2.0e-12  1.04  
97  4.0e-08  2.3e-04  2.1e-07  1.03e+01   1.724043188e+02   1.724043245e+02   2.0e-12  1.05  
Optimizer terminated. Time: 1.05    

solsta = 7, prosta = 1

Interior-point solution summary
  Problem status  : PRIMAL_AND_DUAL_FEASIBLE
  Solution status : NEAR_OPTIMAL
  Primal.  obj: 1.7240431885e+02    nrm: 4e+01    Viol.  con: 8e-07    var: 0e+00  
  Dual.    obj: 1.7240432452e+02    nrm: 8e+02    Viol.  con: 0e+00    var: 1e-03  
* End solution on dual form. *
Transforming to primal solution.
Solving took 1.08 seconds.
Found no installed solvers, beginning a build.
# Moving to the directory from which GPkit was imported.
Started building gpkit...

Attempting to find and build solvers:

# Looking for mosek
#     Found /Users/jenkins/mosek/8/tools/platform/osx64x86/h/mosek.h
#     Found /Users/jenkins/mosek/8/tools/platform/osx64x86/bin/libmosek64.8.1.dylib
#     Found /Users/jenkins/mosek/8/tools/examples/c/scopt-ext.c
#     Found /Users/jenkins/mosek/8/tools/examples/c/expopt.c
#     Found /Users/jenkins/mosek/8/tools/examples/c/dgopt.c
#     Found /Users/jenkins/mosek/8/tools/examples/c/scopt-ext.h
#     Found /Users/jenkins/mosek/8/tools/examples/c/expopt.h
#     Found /Users/jenkins/mosek/8/tools/examples/c/dgopt.h
#     Found /Users/jenkins/mosek/8/tools/platform/osx64x86/h/mosek.h
# Found mosek version 8, installed to /Users/jenkins/mosek
#
# Building mosek...
#     Replacing directory _mosek/lib
#     Replacing directory _mosek/build
#     Replacing directory /Users/jenkins/workspace/gpkit_ResearchModel_SPaircraft_PR/mosek/build_gpkit
#
#   Copying expopt library files to _mosek/build
#     Copying /Users/jenkins/mosek/8/tools/examples/c/scopt-ext.c
#     Copying /Users/jenkins/mosek/8/tools/examples/c/expopt.c
#     Copying /Users/jenkins/mosek/8/tools/examples/c/dgopt.c
#     Copying /Users/jenkins/mosek/8/tools/examples/c/scopt-ext.h
#     Copying /Users/jenkins/mosek/8/tools/examples/c/expopt.h
#     Copying /Users/jenkins/mosek/8/tools/examples/c/dgopt.h
#     Copying /Users/jenkins/mosek/8/tools/platform/osx64x86/h/mosek.h
#
#   Applying expopt patches...
#
#     Change in _mosek/build/dgopt.con line 651
#     --         printf("Number of Hessian non-zeros: %d\n",nlh[0]->numhesnz);
#     ++ MSK_echotask(task,MSK_STREAM_MSG,"Number of Hessian non-zeros: %d\n",n
#
#     Change in _mosek/build/expopt.con line 566
#     --         printf("Warning: The variable with index '%d' has only positiv
#     ++ MSK_echotask(expopttask,MSK_STREAM_MSG, "Warning: The variable with in
#
#     Change in _mosek/build/expopt.con line 579
#     --         printf("Warning: The variable with index '%d' has only negativ
#     ++ MSK_echotask(expopttask,MSK_STREAM_MSG, "Warning: The variable with in
#
#     Change in _mosek/build/expopt.con line 1115
#     --     printf ("solsta = %d, prosta = %d\n", (int)*solsta,(int)*prosta);
#     ++ MSK_echotask(expopttask,MSK_STREAM_MSG, "solsta = %d, prosta = %d\n", 
#
#   Building expopt library...
#     Calling 'gcc -fpic -shared -Wl,-rpath "/Users/jenkins/mosek/8/tools/platform/osx64x86/bin"    _mosek/build/scopt-ext.c _mosek/build/expopt.c _mosek/build/dgopt.c   "/Users/jenkins/mosek/8/tools/platform/osx64x86/bin/libmosek64.8.1.dylib" -o /Users/jenkins/workspace/gpkit_ResearchModel_SPaircraft_PR/mosek/build_gpkit/expopt.so'
##
### CALL BEGINS
### CALL ENDS
##
#     Calling 'install_name_tool -change libmosek64.8.1.dylib /Users/jenkins/mosek/8/tools/platform/osx64x86/bin/libmosek64.8.1.dylib /Users/jenkins/workspace/gpkit_ResearchModel_SPaircraft_PR/mosek/build_gpkit/expopt.so'
##
### CALL BEGINS
### CALL ENDS
##
#     Calling 'install_name_tool -change libmosek64.8.1.dylib @executable_path/libmosek64.8.1.dylib /Users/jenkins/mosek/8/tools/platform/osx64x86/bin/mskexpopt'
##
### CALL BEGINS
### CALL ENDS
##
#
#   Building Python bindings for expopt and Mosek...
#   (if this fails on Windows, verify the mingw version)
#     Calling 'python modified_ctypesgen.py -a -l /Users/jenkins/workspace/gpkit_ResearchModel_SPaircraft_PR/mosek/build_gpkit/expopt.so -l "/Users/jenkins/mosek/8/tools/platform/osx64x86/bin/libmosek64.8.1.dylib" -o _mosek/lib/expopt_h.py    _mosek/build/expopt.h'
##
### CALL BEGINS
### CALL ENDS
##
# Done building mosek
# Looking for mosek_cli
#   Trying to run mskexpopt...
#     Calling 'mskexpopt'
##
### CALL BEGINS
### CALL ENDS
##
# Found mosek_cli in system path
# Looking for cvxopt
#   Trying to import cvxopt...
# Did not find cvxopt
...finished building gpkit.
Replaced found solvers ([u'mosek', u'mosek_cli']) with environment var GPKITSOLVERS (mosek, mosek_cli)

Found the following solvers: mosek, mosek_cli
#     Replacing directory env
x[:] <= w

GPkit is now installed with solver(s) [u'mosek', u'mosek_cli']
To incorporate new solvers at a later date, run `gpkit.build()`.

If any tests didn't pass, please post the output above
(starting from "Found no installed solvers, beginning a build.")
to gpkit@mit.edu or https://github.com/convexengineering/gpkit/issues/new
so we can prevent others from having these errors.

The same goes for any other bugs you encounter with GPkit:
send 'em our way, along with any interesting models, speculative features,
comments, discussions, or clarifications you feel like sharing.

Finally, we hope you find our documentation (https://gpkit.readthedocs.io/)
and engineering-design models (https://github.com/convexengineering/gplibrary/)
to be useful resources for your own applications.

Enjoy!


SETTINGS
defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt, mosek_cli', 'pip install': 'git+https://github.com/hoburg/turbofan.git', 'gpkit-models branch': 'master'})

calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/gplibrary.git']
  attempt 1
calling ['python', '/Users/jenkins/workspace/gpkit_ResearchModel_SPaircraft_PR/mosek/venv2_gpkit/bin/pip', 'install', '--no-cache-dir', '--no-deps', '-e', 'gplibrary']
  attempt 1
calling ['python', '/Users/jenkins/workspace/gpkit_ResearchModel_SPaircraft_PR/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/hoburg/turbofan.git']
  attempt 1
calling ['python', '/Users/jenkins/workspace/gpkit_ResearchModel_SPaircraft_PR/mosek/venv2_gpkit/bin/pip', 'install', '.']
  attempt 1
[Execution node] check if [macys] is in [[windows10x64, windows7x64]]
Run condition [Execution node ] preventing perform for step [Execute Windows batch command]
Build step 'Console output (build log) parsing' changed build result to FAILURE
[Cobertura] Publishing Cobertura coverage report...

INFO: Starting to record.
INFO: Processing JUnit
INFO: [JUnit] - 1 test report file(s) were found with the pattern '**/test_reports/*.xml' relative to '/Users/jenkins/workspace/gpkit_ResearchModel_SPaircraft_PR/mosek' for the testing framework 'JUnit'.
INFO: Check 'Failed Tests' threshold.
INFO: The total number of tests for the threshold 'Failed Tests' exceeds the specified "failure threshold" value.
INFO: Setting the build status to FAILURE
INFO: Stopping recording.
[WS-CLEANUP] Deleting project workspace...
[WS-CLEANUP] Deferred wipeout is used...
[WS-CLEANUP] done
Finished: FAILURE