rename package from gpkitmodels to gplibrary to match repo name (per issue 170)

README.md

@@ -5,23 +5,23 @@
 This repository contains those GP-/SP-compatible models that we consider well documented and general enough to be useful to multiple projects.
 
 * **Simple models with in-depth explanations** (good for learning GPkit)
-  * [SimPleAC](https://github.com/convexengineering/gplibrary/blob/master/gpkitmodels/SP/SimPleAC/simpleac.pdf): a basic aircraft model that captures the fundamental design tradeoffs
-  * [Economic Order Quantity](https://github.com/convexengineering/gplibrary/blob/master/gpkitmodels/misc/Economic%20Order%20Quantity/eoq.pdf): tradeoff between setup and holding costs
-  * [Cylindrical Beam Moment of Inertia](https://github.com/convexengineering/gplibrary/blob/master/gpkitmodels/misc/Moment%20of%20Inertia%20(cylindrical%20beam)/moi.pdf): GP approximation of cylindrical beam MOI
-  * [Net Present Value](https://github.com/convexengineering/gplibrary/blob/master/gpkitmodels/misc/Net%20Present%20Value/npv.pdf): financial tradeoff between cash and equipment
-  * [Raymer Weights](https://github.com/convexengineering/gplibrary/tree/master/gpkitmodels/misc/Raymer%20Weights): rule-of-thumb weight relations for aircraft design
+  * [SimPleAC](https://github.com/convexengineering/gplibrary/blob/master/gplibrary/SP/SimPleAC/simpleac.pdf): a basic aircraft model that captures the fundamental design tradeoffs
+  * [Economic Order Quantity](https://github.com/convexengineering/gplibrary/blob/master/gplibrary/misc/Economic%20Order%20Quantity/eoq.pdf): tradeoff between setup and holding costs
+  * [Cylindrical Beam Moment of Inertia](https://github.com/convexengineering/gplibrary/blob/master/gplibrary/misc/Moment%20of%20Inertia%20(cylindrical%20beam)/moi.pdf): GP approximation of cylindrical beam MOI
+  * [Net Present Value](https://github.com/convexengineering/gplibrary/blob/master/gplibrary/misc/Net%20Present%20Value/npv.pdf): financial tradeoff between cash and equipment
+  * [Raymer Weights](https://github.com/convexengineering/gplibrary/tree/master/gplibrary/misc/Raymer%20Weights): rule-of-thumb weight relations for aircraft design
 * **GP models**
   * Aircraft
-    * [Wing Structural and Aero Models](https://github.com/convexengineering/gplibrary/tree/master/gpkitmodels/GP/aircraft/wing)
-    * [Empennage](https://github.com/convexengineering/gplibrary/tree/master/gpkitmodels/GP/aircraft/tail): TailBoom, HorizontalTail, and VerticalTail inherit from the Wing model
-    * [Mission](https://github.com/convexengineering/gplibrary/tree/master/gpkitmodels/GP/aircraft/mission): models that unify subsystems and flight profiles
-    * [Fuselage](https://github.com/convexengineering/gplibrary/tree/master/gpkitmodels/GP/aircraft/fuselage): elliptical and cylindrical fuselage models
-    * [IC Gas Engine Model](https://github.com/convexengineering/gplibrary/tree/master/gpkitmodels/GP/aircraft/engine)
-  * [Bending Beam](https://github.com/convexengineering/gplibrary/tree/master/gpkitmodels/GP/beam): discretized beam for distributed loads
+    * [Wing Structural and Aero Models](https://github.com/convexengineering/gplibrary/tree/master/gplibrary/GP/aircraft/wing)
+    * [Empennage](https://github.com/convexengineering/gplibrary/tree/master/gplibrary/GP/aircraft/tail): TailBoom, HorizontalTail, and VerticalTail inherit from the Wing model
+    * [Mission](https://github.com/convexengineering/gplibrary/tree/master/gplibrary/GP/aircraft/mission): models that unify subsystems and flight profiles
+    * [Fuselage](https://github.com/convexengineering/gplibrary/tree/master/gplibrary/GP/aircraft/fuselage): elliptical and cylindrical fuselage models
+    * [IC Gas Engine Model](https://github.com/convexengineering/gplibrary/tree/master/gplibrary/GP/aircraft/engine)
+  * [Bending Beam](https://github.com/convexengineering/gplibrary/tree/master/gplibrary/GP/beam): discretized beam for distributed loads
 * **SP models**
   * Aircraft
-    * [Tail Boom Flexibility](https://github.com/convexengineering/gplibrary/tree/master/gpkitmodels/SP/aircraft/tail/tail_boom_flex.py)
-    * [Wing Spanwise Effectiveness](https://github.com/convexengineering/gplibrary/blob/master/gpkitmodels/SP/aircraft/wing/wing.py)
+    * [Tail Boom Flexibility](https://github.com/convexengineering/gplibrary/tree/master/gplibrary/SP/aircraft/tail/tail_boom_flex.py)
+    * [Wing Spanwise Effectiveness](https://github.com/convexengineering/gplibrary/blob/master/gplibrary/SP/aircraft/wing/wing.py)
   * Atmosphere
-    * [Tony Tao's fits as (efficient) signomial equalities](https://github.com/convexengineering/gplibrary/blob/master/gpkitmodels/SP/atmosphere/atmosphere.py). Valid until 10,000m of altitude. 
+    * [Tony Tao's fits as (efficient) signomial equalities](https://github.com/convexengineering/gplibrary/blob/master/gplibrary/SP/atmosphere/atmosphere.py). Valid until 10,000m of altitude.
 

TESTS

@@ -1,5 +1,5 @@
-gpkitmodels/GP/aircraft/wing/wing_test.py
-gpkitmodels/GP/aircraft/tail/tail_tests.py
-gpkitmodels/GP/aircraft/fuselage/test_fuselage.py
-gpkitmodels/GP/aircraft/prop/prop_test.py
-gpkitmodels/GP/aircraft/motor/motor_test.py
+gplibrary/GP/aircraft/wing/wing_test.py
+gplibrary/GP/aircraft/tail/tail_tests.py
+gplibrary/GP/aircraft/fuselage/test_fuselage.py
+gplibrary/GP/aircraft/prop/prop_test.py
+gplibrary/GP/aircraft/motor/motor_test.py

gpkitmodels/GP/aircraft/engine/DF70/DF35_maxPvh.csv → gplibrary/GP/aircraft/engine/DF70/DF35_maxPvh.csv

@@ -1,9 +1,9 @@
-ft,kW,,RPM,P,BSFC,Q(nm)
-0,2.25,,4000,0.2,0.62,0.477707006
-3280.839895,1.97,,5000,0.38,0.51,0.72611465
-6561.67979,1.69,,6000,0.64,0.405,1.01910828
-9842.519685,1.44,,7000,1.02,0.34,1.392174704
-13123.35958,1.2,,8000,1.5,0.32,1.791401274
-16404.19948,0.99,,9000,2.13,0.32,2.261146497
-19685.03937,0.79,,,,,
-22965.87927,0.61,,,,,
+ft,kW,,RPM,P,BSFC,Q(nm)
+0,2.25,,4000,0.2,0.62,0.477707006
+3280.839895,1.97,,5000,0.38,0.51,0.72611465
+6561.67979,1.69,,6000,0.64,0.405,1.01910828
+9842.519685,1.44,,7000,1.02,0.34,1.392174704
+13123.35958,1.2,,8000,1.5,0.32,1.791401274
+16404.19948,0.99,,9000,2.13,0.32,2.261146497
+19685.03937,0.79,,,,,
+22965.87927,0.61,,,,,

gpkitmodels/GP/aircraft/engine/gas_engine.py → gplibrary/GP/aircraft/engine/gas_engine.py

@@ -2,7 +2,7 @@
 from gpkit import Model, Variable, units
 import os
 import pandas as pd
-# from gpkitmodels.tools.fit_constraintset import FitCS
+# from gplibrary.tools.fit_constraintset import FitCS
 from gpfit.fit_constraintset import FitCS
 
 

gpkitmodels/GP/aircraft/fuselage/elliptical_fuselage.py → gplibrary/GP/aircraft/fuselage/elliptical_fuselage.py

@@ -1,8 +1,8 @@
 " elliptical fuselage.py "
 import numpy as np
 from gpkit import Variable, Model, parse_variables
-from gpkitmodels.GP.materials import cfrpfabric
-from gpkitmodels import g
+from gplibrary.GP.materials import cfrpfabric
+from gplibrary import g
 
 class FuselageAero(Model):
     """ Fuselage Aerodyanmic Model

gpkitmodels/GP/aircraft/fuselage/test_fuselage.py → gplibrary/GP/aircraft/fuselage/test_fuselage.py

@@ -1,6 +1,6 @@
 from gpkit import Model
-from gpkitmodels.GP.aircraft.fuselage.elliptical_fuselage import Fuselage
-from gpkitmodels.GP.aircraft.wing.wing_test import FlightState
+from gplibrary.GP.aircraft.fuselage.elliptical_fuselage import Fuselage
+from gplibrary.GP.aircraft.wing.wing_test import FlightState
 
 def test_ellp():
     "elliptical fuselage test"

gpkitmodels/GP/aircraft/motor/motor.py → gplibrary/GP/aircraft/motor/motor.py

@@ -1,8 +1,8 @@
 "Electric motor model "
 from gpkit import Model, parse_variables
 from gpkit.constraints.tight import Tight as TCS
-from gpkitmodels.GP.aircraft.prop.propeller import Propeller, ActuatorProp
-from gpkitmodels import g
+from gplibrary.GP.aircraft.prop.propeller import Propeller, ActuatorProp
+from gplibrary import g
 
 class MotorPerf(Model):
     """ Electric Motor Performance Model

gpkitmodels/GP/aircraft/motor/motor_test.py → gplibrary/GP/aircraft/motor/motor_test.py

@@ -1,8 +1,8 @@
 from gpkit import Model, parse_variables, SignomialsEnabled, SignomialEquality, units
 from motor import Propulsor, Motor, MotorPerf
-from gpkitmodels.GP.aircraft.prop.propeller import Propeller, ActuatorProp
-from gpkitmodels.SP.aircraft.prop.propeller import BladeElementProp
-from gpkitmodels.GP.aircraft.wing.wing_test import FlightState
+from gplibrary.GP.aircraft.prop.propeller import Propeller, ActuatorProp
+from gplibrary.SP.aircraft.prop.propeller import BladeElementProp
+from gplibrary.GP.aircraft.wing.wing_test import FlightState
 
 class Propulsor_Test(Model):
     """Propulsor Test Model

gpkitmodels/GP/aircraft/prop/prop_test.py → gplibrary/GP/aircraft/prop/prop_test.py

@@ -1,8 +1,8 @@
 " propeller tests "
-from gpkitmodels.GP.aircraft.prop.propeller import Propeller, ActuatorProp
-from gpkitmodels.SP.aircraft.prop.propeller import BladeElementProp
+from gplibrary.GP.aircraft.prop.propeller import Propeller, ActuatorProp
+from gplibrary.SP.aircraft.prop.propeller import BladeElementProp
 
-from gpkitmodels.GP.aircraft.wing.wing_test import FlightState
+from gplibrary.GP.aircraft.wing.wing_test import FlightState
 from gpkit import units, Model
 
 def simpleprop_test():

gpkitmodels/GP/aircraft/tail/horizontal_tail.py → gplibrary/GP/aircraft/tail/horizontal_tail.py

@@ -2,9 +2,9 @@
 import numpy as np
 from gpkit import parse_variables
 from .tail_aero import TailAero
-from gpkitmodels.GP.aircraft.wing.wing import Wing
-from gpkitmodels.GP.aircraft.wing.wing_skin import WingSkin
-from gpkitmodels.GP.aircraft.wing.wing_core import WingCore
+from gplibrary.GP.aircraft.wing.wing import Wing
+from gplibrary.GP.aircraft.wing.wing_skin import WingSkin
+from gplibrary.GP.aircraft.wing.wing_core import WingCore
 
 #pylint: disable=attribute-defined-outside-init, no-member
 #pylint: disable=exec-used, undefined-variable

gpkitmodels/GP/aircraft/tail/tail_boom.py → gplibrary/GP/aircraft/tail/tail_boom.py

@@ -2,8 +2,8 @@
 from numpy import pi
 from gpkit import Model, parse_variables, Variable, VectorVariable, units
 from .tube_spar import TubeSpar
-from gpkitmodels.GP.beam.beam import Beam
-from gpkitmodels import g
+from gplibrary.GP.beam.beam import Beam
+from gplibrary import g
 
 #pylint: disable=exec-used, undefined-variable, invalid-name
 #pylint: disable=attribute-defined-outside-init

gpkitmodels/GP/aircraft/tail/tail_tests.py → gplibrary/GP/aircraft/tail/tail_tests.py

@@ -1,10 +1,10 @@
 " test tail models "
-from gpkitmodels.GP.aircraft.tail.horizontal_tail import HorizontalTail
-from gpkitmodels.GP.aircraft.tail.vertical_tail import VerticalTail
-from gpkitmodels.GP.aircraft.tail.empennage import Empennage
-from gpkitmodels.GP.aircraft.wing.wing_test import FlightState
-from gpkitmodels.GP.aircraft.wing.boxspar import BoxSpar
-from gpkitmodels.GP.aircraft.tail.tail_boom import TailBoom
+from gplibrary.GP.aircraft.tail.horizontal_tail import HorizontalTail
+from gplibrary.GP.aircraft.tail.vertical_tail import VerticalTail
+from gplibrary.GP.aircraft.tail.empennage import Empennage
+from gplibrary.GP.aircraft.wing.wing_test import FlightState
+from gplibrary.GP.aircraft.wing.boxspar import BoxSpar
+from gplibrary.GP.aircraft.tail.tail_boom import TailBoom
 from gpkit import Model, Variable, units
 
 #pylint: disable=no-member

gpkitmodels/GP/aircraft/tail/tube_spar.py → gplibrary/GP/aircraft/tail/tube_spar.py

@@ -1,7 +1,7 @@
 " tube spar "
 from numpy import pi
-from gpkitmodels.GP.materials import cfrpfabric
-from gpkitmodels import g
+from gplibrary.GP.materials import cfrpfabric
+from gplibrary import g
 from gpkit import Model, parse_variables
 
 class TubeSpar(Model):

gpkitmodels/GP/aircraft/tail/vertical_tail.py → gplibrary/GP/aircraft/tail/vertical_tail.py

@@ -1,9 +1,9 @@
 " vertical tail "
 from gpkit import parse_variables
 from .tail_aero import TailAero
-from gpkitmodels.GP.aircraft.wing.wing import Wing
-from gpkitmodels.GP.aircraft.wing.wing_core import WingCore
-from gpkitmodels.GP.aircraft.wing.wing_skin import WingSkin
+from gplibrary.GP.aircraft.wing.wing import Wing
+from gplibrary.GP.aircraft.wing.wing_core import WingCore
+from gplibrary.GP.aircraft.wing.wing_skin import WingSkin
 
 #pylint: disable=attribute-defined-outside-init, no-member, exec-used
 

gpkitmodels/GP/aircraft/wing/boxspar.py → gplibrary/GP/aircraft/wing/boxspar.py

@@ -2,8 +2,8 @@
 from gpkit import Model, parse_variables, SignomialsEnabled
 from .sparloading import SparLoading
 from .gustloading import GustL
-from gpkitmodels.GP.materials import cfrpud, cfrpfabric, foamhd
-from gpkitmodels import g
+from gplibrary.GP.materials import cfrpud, cfrpfabric, foamhd
+from gplibrary import g
 
 #pylint: disable=exec-used, undefined-variable, unused-argument, invalid-name
 

gpkitmodels/GP/aircraft/wing/capspar.py → gplibrary/GP/aircraft/wing/capspar.py

@@ -2,8 +2,8 @@
 from gpkit import Model, parse_variables
 from .sparloading import SparLoading
 from .gustloading import GustL
-from gpkitmodels.GP.materials import cfrpud, cfrpfabric, foamhd
-from gpkitmodels import g
+from gplibrary.GP.materials import cfrpud, cfrpfabric, foamhd
+from gplibrary import g
 
 #pylint: disable=exec-used, undefined-variable, unused-argument, invalid-name
 

gpkitmodels/GP/aircraft/wing/wing_core.py → gplibrary/GP/aircraft/wing/wing_core.py

@@ -1,7 +1,7 @@
 " wing interior "
 from gpkit import Model, parse_variables
-from gpkitmodels.GP.materials import foamhd
-from gpkitmodels import g
+from gplibrary.GP.materials import foamhd
+from gplibrary import g
 
 #pylint: disable=exec-used, no-member, undefined-variable
 

gpkitmodels/GP/aircraft/wing/wing_skin.py → gplibrary/GP/aircraft/wing/wing_skin.py

@@ -1,7 +1,7 @@
 " wing skin "
 from gpkit import Model, parse_variables
-from gpkitmodels.GP.materials import cfrpfabric
-from gpkitmodels import g
+from gplibrary.GP.materials import cfrpfabric
+from gplibrary import g
 
 class WingSkin(Model):
     """ Wing Skin model

gpkitmodels/GP/aircraft/wing/wing_test.py → gplibrary/GP/aircraft/wing/wing_test.py

@@ -1,8 +1,8 @@
 " wing test "
-from gpkitmodels.GP.aircraft.wing.wing import Wing
-from gpkitmodels.GP.aircraft.wing.wing_skin import WingSkin
-from gpkitmodels.GP.aircraft.wing.wing_core import WingCore
-from gpkitmodels.GP.aircraft.wing.boxspar import BoxSpar
+from gplibrary.GP.aircraft.wing.wing import Wing
+from gplibrary.GP.aircraft.wing.wing_skin import WingSkin
+from gplibrary.GP.aircraft.wing.wing_core import WingCore
+from gplibrary.GP.aircraft.wing.boxspar import BoxSpar
 from gpkit import Model, parse_variables
 
 #pylint: disable=no-member, exec-used

gpkitmodels/SP/aircraft/prop/dae51polars/dae51_polarfits.py → gplibrary/SP/aircraft/prop/dae51polars/dae51_polarfits.py

@@ -4,8 +4,8 @@
 import matplotlib.pyplot as plt
 from gpfit.fit import fit
 import sys
-from gpkitmodels.GP.aircraft.wing.wing import Wing
-from gpkitmodels.GP.aircraft.prop.propeller import ActuatorProp
+from gplibrary.GP.aircraft.wing.wing import Wing
+from gplibrary.GP.aircraft.prop.propeller import ActuatorProp
 import inspect
 import os
 
@@ -123,4 +123,4 @@ def plot_fits(re, cnstr, x, y):
         path = sys.argv[1]
         F.savefig(path + "dae51polarfit1.eps", bbox_inches="tight")
     else:
-        F.savefig("dae51polarfit1.eps", bbox_inches="tight")
+        F.savefig("dae51polarfit1.eps", bbox_inches="tight")

gpkitmodels/SP/aircraft/wing/boxspar.py → gplibrary/SP/aircraft/wing/boxspar.py

@@ -1,6 +1,6 @@
 " box spar "
 from gpkit import parse_variables, SignomialsEnabled
-from gpkitmodels.GP.aircraft.wing.boxspar import BoxSpar as BoxSparGP
+from gplibrary.GP.aircraft.wing.boxspar import BoxSpar as BoxSparGP
 
 #pylint: disable=exec-used, undefined-variable, unused-argument, invalid-name
 

gpkitmodels/SP/aircraft/wing/wing.py → gplibrary/SP/aircraft/wing/wing.py

@@ -1,6 +1,6 @@
 " wing.py "
 import numpy as np
-from gpkitmodels.GP.aircraft.wing.wing import Wing as WingGP
+from gplibrary.GP.aircraft.wing.wing import Wing as WingGP
 from gpkit import parse_variables, SignomialsEnabled
 
 #pylint: disable=attribute-defined-outside-init, invalid-name

setup.py

@@ -37,7 +37,7 @@
 SOFTWARE."""
 
 setup(
-    name="gpkitmodels",
+    name="gplibrary",
     description="Library of geometric and signomial programming models "
                 "that can be manipulated and solved using GPkit.",
     author="MIT Department of Aeronautics and Astronautics",
@@ -46,7 +46,7 @@
     install_requires=["numpy>=1.12", "scipy", "pint"],
     version="0.0.0.0",
     packages=find_packages(),
-    package_data={"gpkitmodels": ["GP/aircraft/wing/*.csv",
+    package_data={"gplibrary": ["GP/aircraft/wing/*.csv",
                                   ("GP/aircraft/fuselage/"
                                    "fuselage_profile_drag/*.csv"),
                                   "GP/aircraft/engine/*.csv",