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build #3129

Environment variables

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ALLUSERSPROFILE
C:\ProgramData
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BUILD_DISPLAY_NAME
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BUILD_ID
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BUILD_NUMBER
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CLASSPATH
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buildnode
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ghprbActualCommit
a67033cf65cb738b7b7c25fdeda06207c81e988a
ghprbActualCommitAuthor
Edward Burnell
ghprbActualCommitAuthorEmail
eburn@mit.edu
ghprbAuthorRepoGitUrl
https://github.com/convexengineering/gpkit.git
ghprbCommentBody
null
ghprbCredentialsId
2a2b74d8-fbb8-4038-938a-85796af1b79f
ghprbGhRepository
convexengineering/gpkit
ghprbPullAuthorEmail
eburn@mit.edu
ghprbPullAuthorLogin
bqpd
ghprbPullAuthorLoginMention
@bqpd
ghprbPullDescription
GitHub pull request #1534 of commit a67033cf65cb738b7b7c25fdeda06207c81e988a, no merge conflicts.
ghprbPullId
1534
ghprbPullLink
https://github.com/convexengineering/gpkit/pull/1534
ghprbPullLongDescription
Closes #1521\r\n\r\nExample output: \r\n```\r\nOptimal Cost\r\n------------\r\n [ 0.873     1.09      1.61      ]\r\n\r\nSwept Variables\r\n---------------\r\n    | Aircraft.Wing\r\nrho : [ 0.5       1         2        ]  [lbf/ft²] areal density\r\n\r\nModel Sensitivities (sorts models in sections below)\r\n-------------------\r\n +2.79 + [   -     -   +0.1 ] : Mission.FlightSegment.AircraftP.WingAero\r\n +2.51 + [   -     -     -  ] : Mission\r\n +2.43 + [ -0.2    -   +0.3 ] : Mission.FlightSegment.AircraftP\r\n +1.64 + [ -0.5    -   +0.6 ] : Aircraft.Wing\r\n +1.43 + [ -0.6    -   +0.7 ] : Mission.FlightSegment.FlightState\r\n +1.42 + [ -0.2    -   +0.3 ] : Aircraft\r\n +0.97 + [   -     -     -  ] : Aircraft.Fuselage\r\n\r\nFree Variables\r\n--------------\r\n      | Mission.FlightSegment.AircraftP.WingAero\r\n   CD : [ 0.014     0.014     0.0139    0.0139            drag coefficient\r\n          0.019     0.0189    0.0189    0.0188\r\n          0.0352    0.0351    0.0349    0.0348    ]\r\n   CL : [ 0.797     0.796     0.795     0.793             lift coefficient\r\n          1.01      1         1         1\r\n          1.5       1.49      1.49      1.49      ]\r\n    D : [ 2.19      2.19      2.18      2.18        [lbf] drag force\r\n          2.74      2.73      2.72      2.72\r\n          4.04      4.02      4.01      3.99      ]\r\n   Re : [ 3.79e+05  3.79e+05  3.79e+05  3.79e+05          Reynold's number\r\n          3.65e+05  3.65e+05  3.65e+05  3.65e+05\r\n          3.25e+05  3.25e+05  3.25e+05  3.25e+05  ]\r\n\r\n      | Mission.FlightSegment.AircraftP\r\nWburn : [ 0.219     0.219     0.218     0.218       [lbf] segment fuel burn\r\n          0.274     0.273     0.272     0.272\r\n          0.404     0.402     0.401     0.399     ]\r\nWfuel : [ 0.873     0.654     0.436     0.218       [lbf] fuel weight\r\n          1.09      0.817     0.544     0.272\r\n          1.61      1.2       0.8       0.399     ]\r\n\r\n      | Aircraft.Wing\r\n    S : [ 47.8      44.1      35.1     ]            [ft²] surface area\r\n    W : [ 23.9      44.1      70.1     ]            [lbf] weight\r\n    c : [ 1.33      1.28      1.14     ]            [ft]  mean chord\r\n\r\n      | Aircraft\r\n    W : [ 124       144       170      ]            [lbf] weight\r\n\r\nFixed Variables\r\n---------------\r\n    | Mission.FlightSegment.AircraftP.WingAero\r\n  e : [ 0.9       0.9       0.9       0.9      ]           Oswald efficiency\r\n\r\n    | Aircraft.Wing\r\n  A : 27                                                   aspect ratio\r\n\r\n    | Mission.FlightSegment.FlightState\r\n  V : [ 40        40        40        40       ]  [kt]     true airspeed\r\n mu : [ 1.63e-05  1.63e-05  1.63e-05  1.63e-05 ]  [N·s/m²] dynamic viscosity\r\nrho : [ 0.74      0.74      0.74      0.74     ]  [kg/m³]  air density\r\n\r\n    | Aircraft.Fuselage\r\n  W : 100                                         [lbf]    weight\r\n\r\nVariable Sensitivities\r\n----------------------\r\n    | Aircraft.Fuselage\r\n  W : [ +0.96     +0.97     +0.98    ]           weight\r\n\r\n    | Aircraft.Wing\r\n  A : [ -0.56     -0.67     -0.82    ]           aspect ratio\r\nrho : [ +0.23     +0.43     +0.69    ]           areal density\r\n\r\n    | Mission.FlightSegment.AircraftP.WingAero\r\n  e : [ -0.15     -0.15     -0.15     -0.15      Oswald efficiency\r\n        -0.18     -0.18     -0.18     -0.18\r\n        -0.21     -0.21     -0.21     -0.21     ]\r\n\r\n    | Mission.FlightSegment.FlightState\r\n  V : [ -0.12     -0.12     -0.11     -0.11      true airspeed\r\n        -0.22     -0.21     -0.21     -0.21\r\n        -0.35     -0.34     -0.34     -0.34     ]\r\nrho : [ -0.068    -0.068    -0.067    -0.067     air density\r\n        -0.12     -0.11     -0.11     -0.11\r\n        -0.18     -0.18     -0.18     -0.18     ]\r\n mu : [ +0.02     +0.02     +0.02     +0.02      dynamic viscosity\r\n        +0.015    +0.015    +0.015    +0.015\r\n        +0.0084   +0.0084   +0.0085   +0.0085   ]\r\n\r\nMost Sensitive Constraints (in last sweep)\r\n------------------------------------------\r\n       | Aircraft\r\n  +1.7 : .W ≥ .Fuselage.W + .Wing.W\r\n\r\n       | Mission\r\n    +1 : Wfuel[0] ≥ Wfuel[1] + Wburn[0]\r\n +0.75 : Wfuel[1] ≥ Wfuel[2] + Wburn[1]\r\n  +0.5 : Wfuel[2] ≥ Wfuel[3] + Wburn[2]\r\n\r\n       | Aircraft.Wing\r\n +0.69 : .W ≥ S·.rho\r\n```
ghprbPullTitle
Sort solution tables (that aren't already sorted by values) by model sensitivity, an print a model sensitivity table
ghprbSourceBranch
sortbymodelsenss
ghprbTargetBranch
master
optimizer
mosek
sha1
origin/pr/1534/merge
windir
C:\WINDOWS