{
    "info": {
        "author": "Junzi Sun",
        "author_email": "junzisun@gmail.com",
        "bugtrack_url": null,
        "classifiers": [
            "Development Status :: 3 - Alpha",
            "Intended Audience :: Developers",
            "License :: OSI Approved :: MIT License",
            "Programming Language :: Python :: 2",
            "Programming Language :: Python :: 2.6",
            "Programming Language :: Python :: 2.7",
            "Programming Language :: Python :: 3",
            "Programming Language :: Python :: 3.3",
            "Programming Language :: Python :: 3.4",
            "Programming Language :: Python :: 3.5",
            "Topic :: Software Development :: Build Tools"
        ],
        "description": "Open Aircraft Performance Model (OpenAP) Toolkit\n========================================================================\n\nThis repository contains all OpenAP databases and a Python implementation which facilitates the data access and aircraft performance computation.\n\n[Download the related research paper](https://www.researchgate.net/publication/332013573_OpenAP_The_open-source_aircraft_performance_model_and_associated_toolkit)\n\nDatabases:\n---------\n\n  - Aircraft\n  - Engines\n  - Drag polar\n  - Kinematic ([WRAP](https://github.com/junzis/wrap))\n  - Navigation\n\nLibraries\n---------\n\n  - `prop`: aircraft and engine properties\n  - `thrust`: model to compute aircraft thrust\n  - `drag`: model to compute aircraft drag\n  - `fuel`: model to compute fuel consumption\n  - `kinematic`: a utility library to access WRAP data\n  - `aero`: common aeronautical conversions\n  - `nav`: model to access navigation information\n  - `segment`: a utility library to determine climb, cruise, descent, level flight\n  - `phase`: a wrapper around `segment`, providing identification of all flight phases\n  - `traj`: package contains a set of tools related with trajectory generation\n\nExamples\n--------\n\nGet the aircraft and engine data:\n\n```python\nfrom openap import prop\n\naircraft = prop.aircraft('A320')\nengine = prop.engine('CFM56-5B4')\n```\n\nCompute maximum aircraft engine thrust:\n\n```python\nfrom openap import Thrust\n\nthrust = Thrust(ac='A320', eng='CFM56-5B4')\n\nT = thrust.takeoff(tas=100, alt=0)\nT = thrust.climb(tas=200, alt=20000, roc=1000)\nT = thrust.cruise(tas=230, alt=32000)\n```\n\nCompute the aircraft drag:\n\n```python\nfrom openap import Drag\n\ndrag = Drag(ac='A320')\n\nD = drag.clean(mass=60000, tas=200, alt=20000, path_angle=5)\nD = drag.initclimb(mass=60000, tas=150, alt=1000, path_angle=10)\nD = drag.approach(mass=50000, tas=150, alt=1000, path_angle=-10)\n```\n\nCompute the fuel flow:\n\n```python\nfrom openap import FuelFlow\n\nff = FuelFlow(ac='A320', eng='CFM56-5B4')\n\nFF = ff.at_thrust(thr=50000)\nFF = ff.takeoff(tas=100, alt=0, throttle=1)\nFF = ff.enroute(mass=60000, tas=200, alt=20000, path_angle=3)\nFF = ff.enroute(mass=60000, tas=230, alt=32000, path_angle=0)\n```\n\nAccessing the WRAP parameters:\n\n```python\nfrom openap import WRAP\n\nwrap = WRAP(ac='A320')\n\nparam = wrap.takeoff_speed()\nparam = wrap.takeoff_distance()\nparam = wrap.takeoff_acceleration()\nparam = wrap.initclimb_vcas()\nparam = wrap.initclimb_vs()\nparam = wrap.climb_range()\nparam = wrap.climb_const_vcas()\nparam = wrap.climb_const_mach()\nparam = wrap.climb_cross_alt_concas()\nparam = wrap.climb_cross_alt_conmach()\nparam = wrap.climb_vs_pre_concas()\nparam = wrap.climb_vs_concas()\nparam = wrap.climb_vs_conmach()\nparam = wrap.cruise_range()\nparam = wrap.cruise_alt()\nparam = wrap.cruise_init_alt()\nparam = wrap.cruise_mach()\nparam = wrap.descent_range()\nparam = wrap.descent_const_mach()\nparam = wrap.descent_const_vcas()\nparam = wrap.descent_cross_alt_conmach()\nparam = wrap.descent_cross_alt_concas()\nparam = wrap.descent_vs_conmach()\nparam = wrap.descent_vs_concas()\nparam = wrap.descent_vs_post_concas()\nparam = wrap.finalapp_vcas()\nparam = wrap.finalapp_vs()\nparam = wrap.landing_speed()\nparam = wrap.landing_distance()\nparam = wrap.landing_acceleration()\n```\n\n\n",
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        "keywords": "OpenAP,Open Aircraft Performance,Open Data",
        "license": "GNU GPL v3",
        "maintainer": "",
        "maintainer_email": "",
        "name": "openap",
        "package_url": "https://pypi.org/project/openap/",
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        "summary": "Open Aircraft Performance Model (OpenAP) in Python",
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