build #2366

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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
sha1	origin/pr/1534/merge