index int64 0 731k | package stringlengths 2 98 ⌀ | name stringlengths 1 76 | docstring stringlengths 0 281k ⌀ | code stringlengths 4 8.19k | signature stringlengths 2 42.8k ⌀ | embed_func_code listlengths 768 768 |
|---|---|---|---|---|---|---|
722,041 | apprise.plugins.base | parse_url | Parses the URL and returns it broken apart into a dictionary.
This is very specific and customized for Apprise.
Args:
url (str): The URL you want to fully parse.
verify_host (:obj:`bool`, optional): a flag kept with the parsed
URL which some child classes will... | @staticmethod
def parse_url(url, verify_host=True, plus_to_space=False):
"""Parses the URL and returns it broken apart into a dictionary.
This is very specific and customized for Apprise.
Args:
url (str): The URL you want to fully parse.
verify_host (:obj:`bool`, optional): a flag kept with ... | (url, verify_host=True, plus_to_space=False) | [
-0.03148898854851723,
-0.05951026827096939,
-0.01195052731782198,
0.032216086983680725,
-0.01786985993385315,
0.0053087561391294,
0.010253962129354477,
-0.0042414115741848946,
0.0150826470926404,
0.0013062149519100785,
0.02017234079539776,
0.042209040373563766,
0.04261919856071472,
0.03437... |
722,046 | apprise.plugins.base | send |
Should preform the actual notification itself.
| def send(self, body, title='', notify_type=NotifyType.INFO, **kwargs):
"""
Should preform the actual notification itself.
"""
raise NotImplementedError(
"send() is not implimented by the child class.")
| (self, body, title='', notify_type='info', **kwargs) | [
-0.009546549059450626,
-0.0012357429368421435,
0.01663031429052353,
0.006096041761338711,
0.02180825173854828,
-0.08597985655069351,
-0.023809807375073433,
0.08235965669155121,
0.015142201445996761,
0.006644293665885925,
0.04389498010277748,
-0.03045845218002796,
0.013010109774768353,
-0.0... |
722,051 | apprise.plugins.base | url_parameters |
Provides a default set of parameters to work with. This can greatly
simplify URL construction in the acommpanied url() function in all
defined plugin services.
| def url_parameters(self, *args, **kwargs):
"""
Provides a default set of parameters to work with. This can greatly
simplify URL construction in the acommpanied url() function in all
defined plugin services.
"""
params = {
'format': self.notify_format,
'overflow': self.overflow_mo... | (self, *args, **kwargs) | [
-0.028539404273033142,
-0.031036145985126495,
0.027172574773430824,
-0.023126758635044098,
-0.03517308458685875,
0.032967932522296906,
-0.03987497836351395,
-0.001039360067807138,
0.04698249325156212,
-0.010105427354574203,
-0.007102958392351866,
-0.004232615698128939,
-0.03746935725212097,
... |
722,053 | apprise.common | NotifyFormat |
A list of pre-defined text message formats that can be passed via the
apprise library.
| class NotifyFormat:
"""
A list of pre-defined text message formats that can be passed via the
apprise library.
"""
TEXT = 'text'
HTML = 'html'
MARKDOWN = 'markdown'
| () | [
0.020743779838085175,
-0.0662240982055664,
0.03127352148294449,
-0.04847024381160736,
0.021040914580225945,
-0.049621645361185074,
0.023882273584604263,
-0.011049729771912098,
0.04765312373638153,
-0.0010243053548038006,
0.015144630335271358,
0.017531000077724457,
-0.011486148461699486,
0.... |
722,054 | apprise.common | NotifyImageSize |
A list of pre-defined image sizes to make it easier to work with defined
plugins.
| class NotifyImageSize:
"""
A list of pre-defined image sizes to make it easier to work with defined
plugins.
"""
XY_32 = '32x32'
XY_72 = '72x72'
XY_128 = '128x128'
XY_256 = '256x256'
| () | [
0.06604856997728348,
-0.11401621252298355,
-0.06682853400707245,
-0.016033530235290527,
0.005300194025039673,
0.0004301421868149191,
0.01925087161362171,
0.0008397882338613272,
0.004114740993827581,
0.014429289847612381,
0.04250790923833847,
0.012904820032417774,
0.0321202389895916,
0.0003... |
722,055 | apprise.common | NotifyType |
A simple mapping of notification types most commonly used with
all types of logging and notification services.
| class NotifyType:
"""
A simple mapping of notification types most commonly used with
all types of logging and notification services.
"""
INFO = 'info'
SUCCESS = 'success'
WARNING = 'warning'
FAILURE = 'failure'
| () | [
0.03530154377222061,
-0.023414866998791695,
-0.02490541897714138,
-0.05147119611501694,
0.041622236371040344,
-0.07664076238870621,
-0.005334853660315275,
-0.010396125726401806,
0.030792152509093285,
-0.04079205542802811,
-0.013282889500260353,
0.0011509321630001068,
0.012207427993416786,
... |
722,056 | apprise.common | OverflowMode |
A list of pre-defined modes of how to handle the text when it exceeds the
defined maximum message size.
| class OverflowMode:
"""
A list of pre-defined modes of how to handle the text when it exceeds the
defined maximum message size.
"""
# Send the data as is; untouched. Let the upstream server decide how the
# content is handled. Some upstream services might gracefully handle this
# with exp... | () | [
-0.001744267763569951,
-0.005088373553007841,
-0.021046755835413933,
-0.020157957449555397,
0.019909093156456947,
-0.009332387708127499,
0.0009604582446627319,
-0.03828945383429527,
0.02421087957918644,
-0.08688897639513016,
0.01770487241446972,
-0.019909093156456947,
-0.03620966523885727,
... |
722,057 | apprise.url | PrivacyMode | null | class PrivacyMode:
# Defines different privacy modes strings can be printed as
# Astrisk sets 4 of them: e.g. ****
# This is used for passwords
Secret = '*'
# Outer takes the first and last character displaying them with
# 3 dots between. Hence, 'i-am-a-token' would become 'i...n'
Outer = ... | () | [
-0.011449174955487251,
0.007990946061909199,
0.029164697974920273,
-0.017959313467144966,
0.07490722090005875,
-0.04229332506656647,
0.03709243983030319,
-0.04153486341238022,
0.020153436809778214,
-0.022808056324720383,
-0.027413008734583855,
0.029218873009085655,
-0.038175955414772034,
0... |
722,058 | apprise.url | URLBase |
This is the base class for all URL Manipulation
| class URLBase:
"""
This is the base class for all URL Manipulation
"""
# The default descriptive name associated with the URL
service_name = None
# The default simple (insecure) protocol
# all inheriting entries must provide their protocol lookup
# protocol:// (in this example they wou... | (asset=None, **kwargs) | [
-0.00764715438708663,
-0.0629815012216568,
-0.05051947385072708,
-0.008947905153036118,
0.018567165359854698,
-0.00906853936612606,
-0.03449086844921112,
0.02546953409910202,
-0.055093079805374146,
-0.06516340374946594,
0.01653211936354637,
0.059331007301807404,
0.02023506350815296,
-0.004... |
722,060 | apprise.url | __init__ |
Initialize some general logging and common server arguments that will
keep things consistent when working with the children that
inherit this class.
| def __init__(self, asset=None, **kwargs):
"""
Initialize some general logging and common server arguments that will
keep things consistent when working with the children that
inherit this class.
"""
# Prepare our Asset Object
self.asset = \
asset if isinstance(asset, AppriseAsset) el... | (self, asset=None, **kwargs) | [
-0.019438376650214195,
-0.07440546154975891,
-0.02761155553162098,
0.032869961112737656,
0.007503568194806576,
-0.05085095390677452,
0.005361801479011774,
0.032476071268320084,
-0.036789149045944214,
-0.014849580824375153,
0.01292937621474266,
0.05104789510369301,
0.005932939238846302,
-0.... |
722,067 | apprise.url | parse_url | Parses the URL and returns it broken apart into a dictionary.
This is very specific and customized for Apprise.
Args:
url (str): The URL you want to fully parse.
verify_host (:obj:`bool`, optional): a flag kept with the parsed
URL which some child classes will... | @staticmethod
def parse_url(url, verify_host=True, plus_to_space=False,
strict_port=False, sanitize=True):
"""Parses the URL and returns it broken apart into a dictionary.
This is very specific and customized for Apprise.
Args:
url (str): The URL you want to fully parse.
verify... | (url, verify_host=True, plus_to_space=False, strict_port=False, sanitize=True) | [
-0.03843243047595024,
-0.025767197832465172,
-0.021581847220659256,
0.0394514724612236,
-0.018797680735588074,
0.008880220353603363,
0.03381034731864929,
-0.022218748927116394,
0.00557288434356451,
0.001662766677327454,
-0.001230583875440061,
0.02715018205344677,
0.044510286301374435,
0.02... |
722,097 | pytest_socket | SocketBlockedError | null | class SocketBlockedError(RuntimeError):
def __init__(self, *_args, **_kwargs):
super().__init__("A test tried to use socket.socket.")
| (*_args, **_kwargs) | [
-0.017240887507796288,
-0.04419936612248421,
-0.02681915834546089,
0.05130470171570778,
-0.03486490622162819,
-0.022831115871667862,
-0.014733122661709785,
0.06060433387756348,
-0.009595685638487339,
-0.0551011823117733,
0.054857369512319565,
0.07272519916296005,
-0.021803628653287888,
-0.... |
722,098 | pytest_socket | __init__ | null | def __init__(self, *_args, **_kwargs):
super().__init__("A test tried to use socket.socket.")
| (self, *_args, **_kwargs) | [
-0.03096008487045765,
-0.03720858693122864,
0.015162322670221329,
0.012073374353349209,
-0.006897179875522852,
-0.021869752556085587,
0.004545166622847319,
0.07808861136436462,
0.0004473458684515208,
-0.04832879826426506,
0.025152863934636116,
0.09192709624767303,
-0.023211238905787468,
-0... |
722,099 | pytest_socket | SocketConnectBlockedError | null | class SocketConnectBlockedError(RuntimeError):
def __init__(self, allowed, host, *_args, **_kwargs):
if allowed:
allowed = ",".join(allowed)
super().__init__(
"A test tried to use socket.socket.connect() "
f'with host "{host}" (allowed: "{allowed}").'
)
| (allowed, host, *_args, **_kwargs) | [
-0.05022284761071205,
-0.036785878241062164,
-0.017145222052931786,
0.037274494767189026,
-0.04271908476948738,
-0.010836826637387276,
0.006194965448230505,
0.037379201501607895,
0.023767726495862007,
-0.06236846745014191,
0.05043225362896919,
0.06973262131214142,
0.008092719130218029,
-0.... |
722,100 | pytest_socket | __init__ | null | def __init__(self, allowed, host, *_args, **_kwargs):
if allowed:
allowed = ",".join(allowed)
super().__init__(
"A test tried to use socket.socket.connect() "
f'with host "{host}" (allowed: "{allowed}").'
)
| (self, allowed, host, *_args, **_kwargs) | [
-0.03896871209144592,
-0.015216103754937649,
0.014283248223364353,
-0.007414440158754587,
-0.03284354880452156,
-0.013262387365102768,
0.014758476056158543,
0.03140026330947876,
0.033952414989471436,
-0.04213690012693405,
0.0199595857411623,
0.08645633608102798,
-0.0200123880058527,
0.0106... |
722,101 | pytest_socket | _is_unix_socket | null | def _is_unix_socket(family) -> bool:
try:
is_unix_socket = family == socket.AF_UNIX
except AttributeError:
# AF_UNIX not supported on Windows https://bugs.python.org/issue33408
is_unix_socket = False
return is_unix_socket
| (family) -> bool | [
0.03481482341885567,
-0.0007833119016140699,
0.007727954536676407,
0.012689110822975636,
0.0009697888744994998,
0.025326181203126907,
0.010911073535680771,
0.04825851693749428,
-0.0027364417910575867,
-0.03396483510732651,
0.04170146584510803,
0.0019482511561363935,
-0.008551922626793385,
... |
722,102 | pytest_socket | _remove_restrictions | restore socket.socket.* to allow access to the Internet. useful in testing. | def _remove_restrictions():
"""restore socket.socket.* to allow access to the Internet. useful in testing."""
socket.socket = _true_socket
socket.socket.connect = _true_connect
| () | [
-0.009200992994010448,
0.032577428966760635,
0.02160233072936535,
0.01781061664223671,
-0.05464937537908554,
-0.009009667672216892,
-0.04723987728357315,
0.013366659171879292,
0.03186430782079697,
0.00722251832485199,
-0.03289050608873367,
0.0037003993056714535,
-0.035395123064517975,
-0.0... |
722,103 | pytest_socket | _resolve_allow_hosts | Resolve `allow_hosts` behaviors. | def _resolve_allow_hosts(item):
"""Resolve `allow_hosts` behaviors."""
mark_restrictions = item.get_closest_marker("allow_hosts")
cli_restrictions = item.config.__socket_allow_hosts
hosts = None
if mark_restrictions:
hosts = mark_restrictions.args[0]
elif cli_restrictions:
hosts ... | (item) | [
0.04195360094308853,
-0.020095568150281906,
-0.026177803054451942,
-0.008890085853636265,
-0.0021566450595855713,
0.02216905727982521,
0.07340152561664581,
-0.041227880865335464,
0.025693990290164948,
-0.012544610537588596,
0.03317582979798317,
0.000819676264654845,
-0.0180739164352417,
-0... |
722,124 | pytest_socket | disable_socket | disable socket.socket to disable the Internet. useful in testing. | def disable_socket(allow_unix_socket=False):
"""disable socket.socket to disable the Internet. useful in testing."""
class GuardedSocket(socket.socket):
"""socket guard to disable socket creation (from pytest-socket)"""
def __new__(cls, family=-1, type=-1, proto=-1, fileno=None):
i... | (allow_unix_socket=False) | [
0.04706377536058426,
0.009702351875603199,
0.0008144903695210814,
0.006199447438120842,
-0.036797840148210526,
0.0026141726411879063,
-0.06551472097635269,
0.03763021156191826,
-0.02230066992342472,
-0.026531901210546494,
0.027763118967413902,
-0.0021535493433475494,
-0.04106375202536583,
... |
722,125 | pytest_socket | enable_socket | re-enable socket.socket to enable the Internet. useful in testing. | def enable_socket():
"""re-enable socket.socket to enable the Internet. useful in testing."""
socket.socket = _true_socket
| () | [
-0.012418699450790882,
-0.006651971489191055,
0.02809172309935093,
0.005530663300305605,
0.008683815598487854,
0.013354528695344925,
-0.05105746537446976,
0.04495349898934364,
-0.009299270808696747,
-0.017772313207387924,
0.018497370183467865,
-0.06023027002811432,
-0.035848140716552734,
-... |
722,126 | pytest_socket | host_from_address | null | def host_from_address(address):
host = address[0]
if isinstance(host, str):
return host
| (address) | [
0.042899083346128464,
0.06654290854930878,
-0.02321857586503029,
-0.03541470691561699,
-0.0027194649446755648,
-0.03451317921280861,
0.04800206422805786,
0.01319121289998293,
0.04330731928348541,
-0.07219021022319794,
0.03196168690919876,
0.049056682735681534,
-0.06195022165775299,
-0.0400... |
722,127 | pytest_socket | host_from_connect_args | null | def host_from_connect_args(args):
address = args[0]
if isinstance(address, tuple):
return host_from_address(address)
| (args) | [
-0.015050341375172138,
-0.010927893221378326,
-0.006026098504662514,
-0.026659630239009857,
0.006009063683450222,
0.008398209698498249,
0.015510283410549164,
0.04272354766726494,
0.05205867812037468,
-0.08640105277299881,
0.016149092465639114,
0.08299407362937927,
-0.02952149510383606,
0.0... |
722,129 | pytest_socket | is_ipaddress |
Determine if the address is a valid IPv4 or IPv6 address.
| def is_ipaddress(address: str) -> bool:
"""
Determine if the address is a valid IPv4 or IPv6 address.
"""
try:
ipaddress.ip_address(address)
return True
except ValueError:
return False
| (address: str) -> bool | [
0.0316341407597065,
0.007638381328433752,
-0.018143879249691963,
-0.01222663838416338,
-0.04099366068840027,
-0.012331214733421803,
0.011172167025506496,
-0.01243579015135765,
0.05239241197705269,
-0.06434889137744904,
0.033202774822711945,
0.029420621693134308,
0.008596991188824177,
-0.02... |
722,131 | pytest_socket | normalize_allowed_hosts | Map all items in `allowed_hosts` to IP addresses. | def normalize_allowed_hosts(
allowed_hosts: typing.List[str],
) -> typing.Dict[str, typing.Set[str]]:
"""Map all items in `allowed_hosts` to IP addresses."""
ip_hosts = defaultdict(set)
for host in allowed_hosts:
host = host.strip()
if is_ipaddress(host):
ip_hosts[host].add(h... | (allowed_hosts: List[str]) -> Dict[str, Set[str]] | [
0.03194284439086914,
-0.017779167741537094,
-0.07118897885084152,
-0.04280738905072212,
-0.06638038158416748,
-0.007592527195811272,
0.06685039401054382,
-0.03984269127249718,
0.03154514357447624,
0.012184198014438152,
-0.0005101229180581868,
-0.011605720035731792,
-0.006083060521632433,
-... |
722,133 | pytest_socket | pytest_addoption | null | def pytest_addoption(parser):
group = parser.getgroup("socket")
group.addoption(
"--disable-socket",
action="store_true",
dest="disable_socket",
help="Disable socket.socket by default to block network calls.",
)
group.addoption(
"--force-enable-socket",
ac... | (parser) | [
-0.01751701533794403,
0.013992195948958397,
0.017276078462600708,
0.010047967545688152,
-0.0026592311915010214,
0.008704965934157372,
-0.004774122964590788,
0.021202459931373596,
-0.05928836017847061,
-0.03606916964054108,
0.05161406844854355,
-0.028109321370720863,
-0.02684217132627964,
-... |
722,134 | pytest_socket | pytest_configure | null | def pytest_configure(config):
config.addinivalue_line(
"markers", "disable_socket(): Disable socket connections for a specific test"
)
config.addinivalue_line(
"markers", "enable_socket(): Enable socket connections for a specific test"
)
config.addinivalue_line(
"markers",
... | (config) | [
0.024208011105656624,
-0.032787371426820755,
0.033352043479681015,
-0.05409916490316391,
-0.02923540771007538,
0.04542872682213783,
-0.06612119823694229,
0.015655970200896263,
-0.03641219809651375,
-0.005141242407262325,
0.013069410808384418,
-0.03612075746059418,
-0.02400764264166355,
0.0... |
722,135 | pytest_socket | pytest_runtest_setup | During each test item's setup phase,
choose the behavior based on the configurations supplied.
This is the bulk of the logic for the plugin.
As the logic can be extensive, this method is allowed complexity.
It may be refactored in the future to be more readable.
If the given item is not a function... | def pytest_runtest_setup(item) -> None:
"""During each test item's setup phase,
choose the behavior based on the configurations supplied.
This is the bulk of the logic for the plugin.
As the logic can be extensive, this method is allowed complexity.
It may be refactored in the future to be more rea... | (item) -> NoneType | [
0.020459966734051704,
-0.0031048734672367573,
0.0031163732055574656,
-0.031186729669570923,
0.008325660601258278,
0.02927320823073387,
0.010919955559074879,
0.015878552570939064,
-0.01119594369083643,
0.015777356922626495,
0.015308177098631859,
0.03508737310767174,
0.007235505152493715,
0.... |
722,136 | pytest_socket | pytest_runtest_teardown | null | def pytest_runtest_teardown():
_remove_restrictions()
| () | [
0.03460219129920006,
0.04156278446316719,
0.009420228190720081,
-0.009612648747861385,
-0.03187483921647072,
0.009169246070086956,
-0.04407261312007904,
-0.003227223176509142,
0.03247720003128052,
0.017585542052984238,
-0.007362167816609144,
0.009763238951563835,
0.008303354494273663,
-0.0... |
722,137 | pytest_socket | resolve_hostnames | null | def resolve_hostnames(hostname: str) -> typing.Set[str]:
try:
return {
addr_struct[0] for *_, addr_struct in socket.getaddrinfo(hostname, None)
}
except socket.gaierror:
return set()
| (hostname: str) -> Set[str] | [
0.005202753935009241,
0.004642796702682972,
-0.013068612664937973,
-0.029893791303038597,
-0.04306822270154953,
0.019135553389787674,
0.028447601944208145,
-0.026049043983221054,
0.06652470678091049,
-0.022169023752212524,
-0.024673400446772575,
-0.01012332458049059,
-0.03573145717382431,
... |
722,139 | pytest_socket | socket_allow_hosts | disable socket.socket.connect() to disable the Internet. useful in testing. | def socket_allow_hosts(allowed=None, allow_unix_socket=False):
"""disable socket.socket.connect() to disable the Internet. useful in testing."""
if isinstance(allowed, str):
allowed = allowed.split(",")
if not isinstance(allowed, list):
return
allowed_ip_hosts_by_host = normalize_allow... | (allowed=None, allow_unix_socket=False) | [
0.013178679160773754,
-0.02092721313238144,
-0.01718958094716072,
-0.01824740320444107,
-0.04340589791536331,
0.021244559437036514,
0.006373368203639984,
0.006809718906879425,
-0.015532329678535461,
-0.01988702453672886,
0.01004047878086567,
0.0253347996622324,
0.012702660635113716,
-0.046... |
722,143 | itables.javascript | JavascriptCode | A class that explicitly states that a string is a Javascript code | class JavascriptCode(str):
"""A class that explicitly states that a string is a Javascript code"""
pass
| null | [
-0.008659771643579006,
-0.02728421427309513,
0.027448466047644615,
-0.024875173345208168,
0.0051602753810584545,
-0.027119960635900497,
-0.017109666019678116,
0.033215563744306564,
0.04478625953197479,
-0.05343690887093544,
0.023469898849725723,
0.06727064400911331,
-0.009909918531775475,
... |
722,144 | itables.javascript | JavascriptFunction | A class that explicitly states that a string is a Javascript function | class JavascriptFunction(str):
"""A class that explicitly states that a string is a Javascript function"""
def __init__(self, value):
assert value.lstrip().startswith(
"function"
), "A Javascript function is expected to start with 'function'"
| (value) | [
-0.03307228162884712,
0.006827181205153465,
0.03378136456012726,
-0.058108311146497726,
0.003674950683489442,
-0.020236091688275337,
0.010672584176063538,
0.04759936034679413,
0.028108714148402214,
-0.02909051813185215,
-0.0014954344369471073,
0.08392614871263504,
0.008772609755396843,
0.0... |
722,145 | itables.javascript | __init__ | null | def __init__(self, value):
assert value.lstrip().startswith(
"function"
), "A Javascript function is expected to start with 'function'"
| (self, value) | [
-0.02537257969379425,
0.023428644984960556,
0.04070431366562843,
-0.03705309331417084,
-0.020369060337543488,
-0.017224956303834915,
0.014097755774855614,
0.0503394678235054,
0.022127052769064903,
-0.01710662990808487,
-0.006609379779547453,
0.07187488675117493,
0.008443440310657024,
0.017... |
722,148 | itables.javascript | init_notebook_mode | Load the DataTables library and the corresponding css (if connected=False),
and (if all_interactive=True), activate the DataTables representation for all the Pandas DataFrames and Series.
Warning: make sure you keep the output of this cell when 'connected=False',
otherwise the interactive tables will stop ... | def init_notebook_mode(
all_interactive=False,
connected=GOOGLE_COLAB,
dt_bundle=None,
):
"""Load the DataTables library and the corresponding css (if connected=False),
and (if all_interactive=True), activate the DataTables representation for all the Pandas DataFrames and Series.
Warning: make ... | (all_interactive=False, connected=False, dt_bundle=None) | [
-0.020795131102204323,
-0.05859784036874771,
-0.03192107379436493,
-0.029826993122696877,
0.0026631243526935577,
0.04993016645312309,
-0.00019048736430704594,
0.005854321178048849,
-0.07356596738100052,
-0.011216988787055016,
-0.027933215722441673,
-0.004670710302889347,
-0.06322302669286728... |
722,151 | itables.javascript | show | Show a dataframe | def show(df=None, caption=None, **kwargs):
"""Show a dataframe"""
connected = kwargs.pop("connected", ("dt_url" in kwargs) or _CONNECTED)
html = to_html_datatable(df, caption=caption, connected=connected, **kwargs)
display(HTML(html))
| (df=None, caption=None, **kwargs) | [
0.01502242498099804,
-0.03430120274424553,
0.012617047876119614,
-0.03008061647415161,
0.03387198969721794,
0.028578374534845352,
0.012268313206732273,
-0.0061967503279447556,
-0.035535186529159546,
-0.024447208270430565,
-0.016900228336453438,
-0.0201729703694582,
-0.033013567328453064,
-... |
722,152 | itables.javascript | to_html_datatable | null | def to_html_datatable(
df=None,
caption=None,
tableId=None,
connected=True,
use_to_html=False,
**kwargs,
):
check_table_id(tableId)
if "import_jquery" in kwargs:
raise TypeError(
"The argument 'import_jquery' was removed in ITables v2.0. "
"Please pass a c... | (df=None, caption=None, tableId=None, connected=True, use_to_html=False, **kwargs) | [
0.009043131954967976,
-0.06929387897253036,
-0.01238537672907114,
-0.0824621170759201,
-0.021759722381830215,
0.014282327145338058,
-0.005510188173502684,
0.007211420685052872,
-0.06463681161403656,
-0.05443945154547691,
-0.004386069253087044,
-0.003447631374001503,
-0.04649033024907112,
-... |
722,155 | openap.drag | Drag | Compute the drag of aircraft. | class Drag(object):
"""Compute the drag of aircraft."""
def __init__(self, ac, wave_drag=False, **kwargs):
"""Initialize Drag object.
Args:
ac (string): ICAO aircraft type (for example: A320).
wave_drag (bool): enable wave_drag model (experimental).
"""
... | (ac, wave_drag=False, **kwargs) | [
0.03306078910827637,
-0.01429296750575304,
-0.02576616406440735,
0.036023590713739395,
-0.00032980332616716623,
-0.03320382162928581,
-0.06134022772312164,
0.0073508149944245815,
-0.035900991410017014,
-0.011963591910898685,
-0.02425411343574524,
0.0069932350888848305,
0.01148341316729784,
... |
722,156 | openap.drag | __init__ | Initialize Drag object.
Args:
ac (string): ICAO aircraft type (for example: A320).
wave_drag (bool): enable wave_drag model (experimental).
| def __init__(self, ac, wave_drag=False, **kwargs):
"""Initialize Drag object.
Args:
ac (string): ICAO aircraft type (for example: A320).
wave_drag (bool): enable wave_drag model (experimental).
"""
if not hasattr(self, "np"):
self.np = importlib.import_module("numpy")
if not ... | (self, ac, wave_drag=False, **kwargs) | [
0.02630849927663803,
0.011639242991805077,
0.002673941431567073,
0.03581584617495537,
-0.01952272094786167,
-0.03824711591005325,
-0.060491401702165604,
0.030390851199626923,
-0.04144041985273361,
0.005511176772415638,
-0.008491294458508492,
0.05025830492377281,
-0.026743950322270393,
0.03... |
722,157 | openap.drag | _calc_drag | null | """OpenAP drag model."""
import glob
import importlib
import os
import warnings
import pandas as pd
import yaml
from . import prop
from .extra import ndarrayconvert
curr_path = os.path.dirname(os.path.realpath(__file__))
dir_dragpolar = curr_path + "/data/dragpolar/"
file_synonym = curr_path + "/data/dragpolar/_syn... | (self, mass, tas, alt, cd0, k, path_angle) | [
0.031659211963415146,
-0.004102557431906462,
-0.017001038417220116,
0.024997331202030182,
-0.004624608438462019,
-0.030946167185902596,
-0.05728809908032417,
0.003050815314054489,
-0.04229377582669258,
-0.012926492840051651,
-0.031068403273820877,
0.004336843732744455,
0.013272829353809357,
... |
722,159 | openap.drag | clean | Compute drag at clean configuration (considering compressibility).
Args:
mass (int or ndarray): Mass of the aircraft (unit: kg).
tas (int or ndarray): True airspeed (unit: kt).
alt (int or ndarray): Altitude (unit: ft).
path_angle (float or ndarray): Path angle (... | """OpenAP drag model."""
import glob
import importlib
import os
import warnings
import pandas as pd
import yaml
from . import prop
from .extra import ndarrayconvert
curr_path = os.path.dirname(os.path.realpath(__file__))
dir_dragpolar = curr_path + "/data/dragpolar/"
file_synonym = curr_path + "/data/dragpolar/_syn... | (self, mass, tas, alt, path_angle=0) | [
0.031659211963415146,
-0.004102557431906462,
-0.017001038417220116,
0.024997331202030182,
-0.004624608438462019,
-0.030946167185902596,
-0.05728809908032417,
0.003050815314054489,
-0.04229377582669258,
-0.012926492840051651,
-0.031068403273820877,
0.004336843732744455,
0.013272829353809357,
... |
722,160 | openap.drag | dragpolar | Find and construct the drag polar model.
Returns:
dict: drag polar model parameters.
| def dragpolar(self):
"""Find and construct the drag polar model.
Returns:
dict: drag polar model parameters.
"""
polar_files = glob.glob(dir_dragpolar + "*.yml")
ac_polar_available = [s[-8:-4].lower() for s in polar_files]
if self.ac in ac_polar_available:
ac = self.ac
else:
... | (self) | [
0.02568015642464161,
-0.03286709636449814,
0.0007274583913385868,
0.023313725367188454,
-0.01610049419105053,
0.0031552412547171116,
-0.020842120051383972,
0.0007647077436558902,
0.01922944188117981,
0.012498260475695133,
-0.017047066241502762,
-0.009272903203964233,
0.00045110087376087904,
... |
722,161 | openap.drag | nonclean | Compute drag at at non-clean configuration.
Args:
mass (int or ndarray): Mass of the aircraft (unit: kg).
tas (int or ndarray): True airspeed (unit: kt).
alt (int or ndarray): Altitude (unit: ft).
flap_angle (int or ndarray): flap deflection angle (unit: degree).... | """OpenAP drag model."""
import glob
import importlib
import os
import warnings
import pandas as pd
import yaml
from . import prop
from .extra import ndarrayconvert
curr_path = os.path.dirname(os.path.realpath(__file__))
dir_dragpolar = curr_path + "/data/dragpolar/"
file_synonym = curr_path + "/data/dragpolar/_syn... | (self, mass, tas, alt, flap_angle, path_angle=0, landing_gear=False) | [
0.031659211963415146,
-0.004102557431906462,
-0.017001038417220116,
0.024997331202030182,
-0.004624608438462019,
-0.030946167185902596,
-0.05728809908032417,
0.003050815314054489,
-0.04229377582669258,
-0.012926492840051651,
-0.031068403273820877,
0.004336843732744455,
0.013272829353809357,
... |
722,162 | openap.emission | Emission | Emission model based on ICAO emmision databank. | class Emission(object):
"""Emission model based on ICAO emmision databank."""
def __init__(self, ac, eng=None, **kwargs):
"""Initialize Emission object.
Args:
ac (string): ICAO aircraft type (for example: A320).
eng (string): Engine type (for example: CFM56-5A3).
... | (ac, eng=None, **kwargs) | [
0.03340556100010872,
-0.05153419077396393,
-0.03969965875148773,
0.002464678604155779,
0.0017466627759858966,
-0.043753139674663544,
-0.07068128138780594,
-0.043264277279376984,
-0.044079046696424484,
-0.014635302126407623,
0.00875877495855093,
-0.014472348615527153,
0.006828789599239826,
... |
722,163 | openap.emission | __init__ | Initialize Emission object.
Args:
ac (string): ICAO aircraft type (for example: A320).
eng (string): Engine type (for example: CFM56-5A3).
Leave empty to use the default engine specified
by in the aircraft database.
| def __init__(self, ac, eng=None, **kwargs):
"""Initialize Emission object.
Args:
ac (string): ICAO aircraft type (for example: A320).
eng (string): Engine type (for example: CFM56-5A3).
Leave empty to use the default engine specified
by in the aircraft database.
"""
... | (self, ac, eng=None, **kwargs) | [
0.0393601730465889,
0.0030059372074902058,
-0.01705072820186615,
-0.0006500979652628303,
0.012505055405199528,
-0.05108978971838951,
-0.01968008652329445,
-0.022122271358966827,
-0.028058385476469994,
-0.022407490760087967,
0.008708082139492035,
0.05141066387295723,
-0.03199796751141548,
0... |
722,164 | openap.emission | _fl2sl | Convert to sea-level equivalent | def _fl2sl(self, ffac, tas, alt):
"""Convert to sea-level equivalent"""
M = self.aero.tas2mach(tas * self.aero.kts, alt * self.aero.ft)
beta = self.np.exp(0.2 * (M ** 2))
theta = (self.aero.temperature(alt * self.aero.ft) / 288.15) / beta
delta = (1 - 0.0019812 * alt / 288.15) ** 5.255876 / self.np.... | (self, ffac, tas, alt) | [
-0.013660362921655178,
0.011595847085118294,
0.04059910774230957,
0.007294015493243933,
-0.01849878765642643,
-0.013978679664433002,
-0.02615659311413765,
-0.057551782578229904,
-0.06049849092960358,
0.042636338621377945,
-0.008212587796151638,
-0.03237742558121681,
-0.006830181460827589,
... |
722,165 | openap.emission | co | Compute CO emission with given fuel flow, speed, and altitude.
Args:
ffac (float or ndarray): Fuel flow for all engines (unit: kg/s).
tas (float or ndarray): Speed (unit: kt).
alt (int or ndarray): Aircraft altitude (unit: ft).
Returns:
float: CO emissio... | """OpenAP FuelFlow model."""
import importlib
from openap import prop
from openap.extra import ndarrayconvert
class Emission(object):
"""Emission model based on ICAO emmision databank."""
def __init__(self, ac, eng=None, **kwargs):
"""Initialize Emission object.
Args:
ac (string... | (self, ffac, tas, alt=0) | [
0.03498595207929611,
-0.047566309571266174,
-0.02923261746764183,
-0.007996934466063976,
-0.012560099363327026,
-0.039118632674217224,
-0.06247636303305626,
-0.06211171671748161,
-0.05838420242071152,
-0.009723947383463383,
0.008255226537585258,
-0.035208795219659805,
0.010493759997189045,
... |
722,166 | openap.emission | co2 | Compute CO2 emission with given fuel flow.
Args:
ffac (float or ndarray): Fuel flow for all engines (unit: kg/s).
Returns:
float: CO2 emission from all engines (unit: g/s).
| """OpenAP FuelFlow model."""
import importlib
from openap import prop
from openap.extra import ndarrayconvert
class Emission(object):
"""Emission model based on ICAO emmision databank."""
def __init__(self, ac, eng=None, **kwargs):
"""Initialize Emission object.
Args:
ac (string... | (self, ffac) | [
0.034948911517858505,
-0.04761156067252159,
-0.029255783185362816,
-0.007982533425092697,
-0.012591738253831863,
-0.039061740040779114,
-0.062482573091983795,
-0.062036849558353424,
-0.05830896645784378,
-0.009724914096295834,
0.008256047032773495,
-0.035232555121183395,
0.01047454308718443,... |
722,167 | openap.emission | h2o | Compute H2O emission with given fuel flow.
Args:
ffac (float or ndarray): Fuel flow for all engines (unit: kg/s).
Returns:
float: H2O emission from all engines (unit: g/s).
| """OpenAP FuelFlow model."""
import importlib
from openap import prop
from openap.extra import ndarrayconvert
class Emission(object):
"""Emission model based on ICAO emmision databank."""
def __init__(self, ac, eng=None, **kwargs):
"""Initialize Emission object.
Args:
ac (string... | (self, ffac) | [
0.03498595207929611,
-0.047566309571266174,
-0.02923261746764183,
-0.007996934466063976,
-0.012560099363327026,
-0.039118632674217224,
-0.06247636303305626,
-0.06211171671748161,
-0.05838420242071152,
-0.009723947383463383,
0.008255226537585258,
-0.035208795219659805,
0.010493759997189045,
... |
722,168 | openap.emission | hc | Compute HC emission with given fuel flow, speed, and altitude.
Args:
ffac (float or ndarray): Fuel flow for all engines (unit: kg/s).
tas (float or ndarray): Speed (unit: kt).
alt (int or ndarray): Aircraft altitude (unit: ft).
Returns:
float: HC emissio... | """OpenAP FuelFlow model."""
import importlib
from openap import prop
from openap.extra import ndarrayconvert
class Emission(object):
"""Emission model based on ICAO emmision databank."""
def __init__(self, ac, eng=None, **kwargs):
"""Initialize Emission object.
Args:
ac (string... | (self, ffac, tas, alt=0) | [
0.034948911517858505,
-0.04761156067252159,
-0.029255783185362816,
-0.007982533425092697,
-0.012591738253831863,
-0.039061740040779114,
-0.062482573091983795,
-0.062036849558353424,
-0.05830896645784378,
-0.009724914096295834,
0.008256047032773495,
-0.035232555121183395,
0.01047454308718443,... |
722,169 | openap.emission | nox | Compute NOx emission with given fuel flow, speed, and altitude.
Args:
ffac (float or ndarray): Fuel flow for all engines (unit: kg/s).
tas (float or ndarray): Speed (unit: kt).
alt (int or ndarray): Aircraft altitude (unit: ft).
Returns:
float: NOx emiss... | """OpenAP FuelFlow model."""
import importlib
from openap import prop
from openap.extra import ndarrayconvert
class Emission(object):
"""Emission model based on ICAO emmision databank."""
def __init__(self, ac, eng=None, **kwargs):
"""Initialize Emission object.
Args:
ac (string... | (self, ffac, tas, alt=0) | [
0.034985434263944626,
-0.047565605491399765,
-0.029211927205324173,
-0.008032266981899738,
-0.012600429356098175,
-0.03907753527164459,
-0.06247543916106224,
-0.06211079657077789,
-0.058423854410648346,
-0.009728868491947651,
0.008255104534327984,
-0.035228531807661057,
0.010463218204677105,... |
722,170 | openap.emission | soot | Compute soot emission with given fuel flow.
Args:
ffac (float or ndarray): Fuel flow for all engines (unit: kg/s).
Returns:
float: Soot emission from all engines (unit: g/s).
| """OpenAP FuelFlow model."""
import importlib
from openap import prop
from openap.extra import ndarrayconvert
class Emission(object):
"""Emission model based on ICAO emmision databank."""
def __init__(self, ac, eng=None, **kwargs):
"""Initialize Emission object.
Args:
ac (string... | (self, ffac) | [
0.034985434263944626,
-0.047565605491399765,
-0.029211927205324173,
-0.008032266981899738,
-0.012600429356098175,
-0.03907753527164459,
-0.06247543916106224,
-0.06211079657077789,
-0.058423854410648346,
-0.009728868491947651,
0.008255104534327984,
-0.035228531807661057,
0.010463218204677105,... |
722,171 | openap.emission | sox | Compute SOx emission with given fuel flow.
Args:
ffac (float or ndarray): Fuel flow for all engines (unit: kg/s).
Returns:
float: SOx emission from all engines (unit: g/s).
| """OpenAP FuelFlow model."""
import importlib
from openap import prop
from openap.extra import ndarrayconvert
class Emission(object):
"""Emission model based on ICAO emmision databank."""
def __init__(self, ac, eng=None, **kwargs):
"""Initialize Emission object.
Args:
ac (string... | (self, ffac) | [
0.034985434263944626,
-0.047565605491399765,
-0.029211927205324173,
-0.008032266981899738,
-0.012600429356098175,
-0.03907753527164459,
-0.06247543916106224,
-0.06211079657077789,
-0.058423854410648346,
-0.009728868491947651,
0.008255104534327984,
-0.035228531807661057,
0.010463218204677105,... |
722,172 | openap.phase | FlightPhase | Fuzzy logic flight phase identification. | class FlightPhase(object):
"""Fuzzy logic flight phase identification."""
def __init__(self):
"""Initialize of the FlightPhase object."""
super(FlightPhase, self).__init__()
# logic states
self.alt_range = np.arange(0, 40000, 1)
self.roc_range = np.arange(-4000, 4000, 0... | () | [
0.04640013724565506,
-0.014611680991947651,
-0.004335733596235514,
0.010286333039402962,
-0.03167422115802765,
-0.060731422156095505,
-0.04239153116941452,
-0.03441585600376129,
-0.04394927993416786,
-0.023947788402438164,
-0.06014986336231232,
0.05072029307484627,
0.03208962082862854,
0.0... |
722,173 | openap.phase | __init__ | Initialize of the FlightPhase object. | def __init__(self):
"""Initialize of the FlightPhase object."""
super(FlightPhase, self).__init__()
# logic states
self.alt_range = np.arange(0, 40000, 1)
self.roc_range = np.arange(-4000, 4000, 0.1)
self.spd_range = np.arange(0, 600, 1)
self.states = np.arange(0, 6, 0.01)
self.alt_gnd =... | (self) | [
0.04665512964129448,
-0.011370856314897537,
-0.017744217067956924,
0.008312885649502277,
-0.0535433292388916,
-0.06646758317947388,
-0.04100964590907097,
-0.02235114574432373,
-0.08429168909788132,
0.008175299502909184,
-0.052868712693452835,
0.06415968388319016,
-0.010145893320441246,
0.0... |
722,174 | openap.phase | _get_cl | null | def _get_cl(self):
labels = np.array(self.phaselabel())
if "CL" not in labels:
return None
idx = np.where(np.array(labels) == "CL")[0]
istart = idx[0]
iend = idx[-1]
return istart, iend
| (self) | [
0.01422116905450821,
-0.009367236867547035,
-0.006301595829427242,
0.024252628907561302,
-0.023963095620274544,
0.00678698904812336,
0.054772790521383286,
0.007463984657078981,
0.04635930806398392,
-0.06046125665307045,
-0.030383910983800888,
-0.053750909864902496,
-0.015260080806910992,
-... |
722,175 | openap.phase | _get_cr | null | def _get_cr(self):
# CR start = CL end, CR end = DE start
ttCL = self._get_cl()
if not ttCL:
return None
ttDE = self._get_de()
if not ttDE:
return None
ttDE = ttDE[0:2]
istart = ttCL[-1]
iend = ttDE[0]
if iend - istart < 200:
# too few samples
return N... | (self) | [
0.00866581592708826,
-0.008919554762542248,
-0.010424782522022724,
0.03860266134142876,
0.0040533654391765594,
-0.008386272937059402,
0.03005296364426613,
-0.011001070030033588,
0.05277761444449425,
-0.05625254288315773,
0.00278897350654006,
-0.0017213363898918033,
-0.00819704495370388,
0.... |
722,176 | openap.phase | _get_de | null | def _get_de(self):
labels = np.array(self.phaselabel())
if "DE" not in labels:
return None
idx = np.where(np.array(labels) == "DE")[0]
istart = idx[0]
iend = idx[-1]
if "LVL" in labels[istart:iend]:
isCDA = False
else:
isCDA = True
return istart, iend, isCDA
| (self) | [
0.059581272304058075,
0.052743494510650635,
0.011627785861492157,
0.0024617784656584263,
-0.019836680963635445,
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0.03361907973885536,
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0.00510162441059947,
-0.06367681920528412,
-0.03438476845622063,
-0.016302049160003662,
-0.025659477338194847,
-0... |
722,177 | openap.phase | _get_fa_ld | null | def _get_fa_ld(self):
# get the approach + landing data chunk (h=0)
istart = 0
iend = 0
for i in reversed(list(range(0, self.ndata))):
if self.alt[i] < 1500: # ft
istart = i
else:
break
# keep only the chunk in landing deceleration states, break at taxing poi... | (self) | [
0.022493014112114906,
-0.0017689120722934604,
-0.016110118478536606,
0.01645410805940628,
-0.0018226603278890252,
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0.017954278737306595,
-0.059242431074380875,
-0.06272053718566895,
-0.01117006503045559,
-0.017008310183882713,
0.011189175769686699,
-0.042692773044109344... |
722,178 | openap.phase | _get_to_ic | null | def _get_to_ic(self):
# get the data chunk up to certain ft
istart = 0
iend = 0
for i in range(0, self.ndata):
if self.alt[i] < 1500: # ft
iend = i
continue
else:
break
# keep only the chunk in taking-off states, break at starting point
spdtmp... | (self) | [
0.02714134007692337,
-0.03436867147684097,
-0.034873805940151215,
-0.010199859738349915,
0.021235136315226555,
-0.04107143357396126,
0.040838293731212616,
-0.04736620560288429,
0.007810178212821484,
-0.03063843585550785,
-0.010384428314864635,
-0.020613430067896843,
-0.03324182704091072,
-... |
722,179 | openap.phase | flight_phase_indices | Get the indices of data, of which different flight phase start.
Returns:
dict: Indices for takeoff (TO), initial climb (IC), climb (CL),
cruise (CR), descent (DE), final approach (FA), landing (LD).
| def flight_phase_indices(self):
"""Get the indices of data, of which different flight phase start.
Returns:
dict: Indices for takeoff (TO), initial climb (IC), climb (CL),
cruise (CR), descent (DE), final approach (FA), landing (LD).
"""
# Process the data and get the phase index
... | (self) | [
0.0024993191473186016,
0.010494477115571499,
-0.0934736505150795,
0.009766433387994766,
-0.04506765305995941,
-0.007910811342298985,
-0.008780911564826965,
0.006499117705971003,
-0.047944311052560806,
-0.025126369670033455,
-0.030737631022930145,
-0.0029587855096906424,
-0.02660021372139454,... |
722,180 | openap.phase | phaselabel | Fuzzy logic for determining phase label.
Args:
twindow (int): Time window in number of seconds. Default to 60.
Returns:
list: Labels could be: ground [GND], climb [CL], descent [DE],
cruise [CR], leveling [LVL].
| def phaselabel(self, twindow=60):
"""Fuzzy logic for determining phase label.
Args:
twindow (int): Time window in number of seconds. Default to 60.
Returns:
list: Labels could be: ground [GND], climb [CL], descent [DE],
cruise [CR], leveling [LVL].
"""
if self.ts is None:... | (self, twindow=60) | [
0.029212459921836853,
-0.023361841216683388,
-0.014860163442790508,
-0.009299028664827347,
-0.024052539840340614,
-0.03849625214934349,
-0.027221623808145523,
-0.02291492000222206,
-0.006480372045189142,
-0.03266594931483269,
-0.07069496810436249,
0.030959518626332283,
0.03380357101559639,
... |
722,181 | openap.phase | plot_logics | Visualize fuzzy logic membership functions. | def plot_logics(self):
"""Visualize fuzzy logic membership functions."""
plt.figure(figsize=(10, 8))
plt.subplot(411)
plt.plot(self.alt_range, self.alt_gnd, lw=2, label="Ground")
plt.plot(self.alt_range, self.alt_lo, lw=2, label="Low")
plt.plot(self.alt_range, self.alt_hi, lw=2, label="High")
... | (self) | [
0.03358882665634155,
-0.039007555693387985,
0.05046534165740013,
0.04740019887685776,
-0.07082662731409073,
-0.03537682443857193,
-0.030852094292640686,
-0.014979047700762749,
-0.0367816798388958,
0.038752127438783646,
-0.016119351610541344,
0.04572167247533798,
0.06473283469676971,
0.0178... |
722,182 | openap.phase | set_trajectory | Set trajectory data.
Args:
ts (list): Time (unit: second).
alt (list): Altitude (unit: ft).
spd (list): True airspeed (unit: kt).
roc (list): Rate of climb (unit: ft/min). Negative for descent.
| def set_trajectory(self, ts, alt, spd, roc):
"""Set trajectory data.
Args:
ts (list): Time (unit: second).
alt (list): Altitude (unit: ft).
spd (list): True airspeed (unit: kt).
roc (list): Rate of climb (unit: ft/min). Negative for descent.
"""
self.ts = ts - ts[0]
s... | (self, ts, alt, spd, roc) | [
-0.013638879172503948,
0.09190619736909866,
-0.01742541417479515,
-0.013684832490980625,
-0.04771769791841507,
-0.032442886382341385,
-0.06312117725610733,
0.010964409448206425,
0.01968630775809288,
0.022278061136603355,
-0.04337972402572632,
0.002103503094986081,
0.013519401662051678,
-0.... |
722,183 | openap.fuel | FuelFlow | Fuel flow model based on ICAO emission databank. | class FuelFlow(object):
"""Fuel flow model based on ICAO emission databank."""
def __init__(self, ac, eng=None, **kwargs):
"""Initialize FuelFlow object.
Args:
ac (string): ICAO aircraft type (for example: A320).
eng (string): Engine type (for example: CFM56-5A3).
... | (ac, eng=None, **kwargs) | [
0.05831855162978172,
-0.050640758126974106,
-0.018592100590467453,
0.03146669641137123,
-0.01916385069489479,
-0.04855795204639435,
-0.065097875893116,
-0.03097662515938282,
-0.08380229026079178,
-0.021971555426716805,
-0.00671806838363409,
-0.026586398482322693,
-0.008290382102131844,
0.0... |
722,184 | openap.fuel | __init__ | Initialize FuelFlow object.
Args:
ac (string): ICAO aircraft type (for example: A320).
eng (string): Engine type (for example: CFM56-5A3).
Leave empty to use the default engine specified
by in the aircraft database.
polydeg (int): Order of the... | def __init__(self, ac, eng=None, **kwargs):
"""Initialize FuelFlow object.
Args:
ac (string): ICAO aircraft type (for example: A320).
eng (string): Engine type (for example: CFM56-5A3).
Leave empty to use the default engine specified
by in the aircraft database.
p... | (self, ac, eng=None, **kwargs) | [
0.04939153790473938,
-0.038122233003377914,
-0.010460368357598782,
0.029977092519402504,
-0.03780609741806984,
-0.04314320906996727,
-0.044630907475948334,
-0.03680190071463585,
-0.08517064899206161,
-0.01963759958744049,
0.018661297857761383,
-0.002619741251692176,
-0.03656015172600746,
0... |
722,185 | openap.fuel | at_thrust | Compute the fuel flow at a given total thrust.
Args:
acthr (int or ndarray): The total net thrust of the aircraft (unit: N).
alt (int or ndarray): Aircraft altitude (unit: ft).
Returns:
float: Fuel flow (unit: kg/s).
| """OpenAP FuelFlow model."""
import importlib
from openap import prop
from openap.extra import ndarrayconvert
def func_fuel2(a, b):
return lambda x: a * (x + b) ** 2
| (self, acthr, alt=0, limit=True) | [
0.02575569599866867,
-0.07577159255743027,
0.033085454255342484,
0.0064620026387274265,
-0.018001291900873184,
-0.027214262634515762,
-0.05734565481543541,
-0.06550624221563339,
-0.030666816979646683,
-0.014521042816340923,
0.014428728260099888,
-0.029392879456281662,
0.03747961297631264,
... |
722,186 | openap.fuel | enroute | Compute the fuel flow during climb, cruise, or descent.
The net thrust is first estimated based on the dynamic equation.
Then FuelFlow.at_thrust() is called to compted the thrust. Assuming
no flap deflection and no landing gear extended.
Args:
mass (int or ndarray): Aircraf... | """OpenAP FuelFlow model."""
import importlib
from openap import prop
from openap.extra import ndarrayconvert
def func_fuel2(a, b):
return lambda x: a * (x + b) ** 2
| (self, mass, tas, alt, path_angle=0, limit=True) | [
0.02575569599866867,
-0.07577159255743027,
0.033085454255342484,
0.0064620026387274265,
-0.018001291900873184,
-0.027214262634515762,
-0.05734565481543541,
-0.06550624221563339,
-0.030666816979646683,
-0.014521042816340923,
0.014428728260099888,
-0.029392879456281662,
0.03747961297631264,
... |
722,187 | openap.fuel | plot_model | Plot the engine fuel model, or return the pyplot object.
Args:
plot (bool): Display the plot or return an object.
Returns:
None or pyplot object.
| def plot_model(self, plot=True):
"""Plot the engine fuel model, or return the pyplot object.
Args:
plot (bool): Display the plot or return an object.
Returns:
None or pyplot object.
"""
import matplotlib.pyplot as plt
x = [0.07, 0.3, 0.85, 1.0]
y = [
self.engine["ff_i... | (self, plot=True) | [
0.11342854797840118,
-0.055629368871450424,
0.013720289804041386,
0.026467908173799515,
-0.003002190263941884,
-0.006766618695110083,
-0.04522925987839699,
-0.024877963587641716,
-0.038794659078121185,
0.008819518610835075,
0.0063878376968204975,
-0.023512480780482292,
0.011943292804062366,
... |
722,188 | openap.fuel | takeoff | Compute the fuel flow at takeoff.
The net thrust is first estimated based on the maximum thrust model
and throttle setting. Then FuelFlow.at_thrust() is called to compted
the thrust.
Args:
tas (int or ndarray): Aircraft true airspeed (unit: kt).
alt (int or ndar... | """OpenAP FuelFlow model."""
import importlib
from openap import prop
from openap.extra import ndarrayconvert
def func_fuel2(a, b):
return lambda x: a * (x + b) ** 2
| (self, tas, alt=None, throttle=1) | [
0.025829507037997246,
-0.07577148079872131,
0.033085402101278305,
0.006475839763879776,
-0.01796433888375759,
-0.02726960927248001,
-0.05730864405632019,
-0.06550614535808563,
-0.03074062243103981,
-0.014502557925879955,
0.014456400647759438,
-0.029374372214078903,
0.03740570694208145,
0.0... |
722,189 | openap.thrust | Thrust | Simplified two-shaft turbonfan model. | class Thrust(object):
"""Simplified two-shaft turbonfan model."""
def __init__(self, ac, eng=None, **kwargs):
"""Initialize Thrust object.
Args:
ac (string): ICAO aircraft type (for example: A320).
eng (string): Engine type (for example: CFM56-5A3).
"""
... | (ac, eng=None, **kwargs) | [
-0.01929096132516861,
-0.002909201430156827,
-0.015930600464344025,
0.026841402053833008,
-0.0009062084718607366,
-0.05700168013572693,
-0.07732979208230972,
-0.0398472435772419,
-0.08861396461725235,
-0.023377327248454094,
0.003860785160213709,
0.040386561304330826,
-0.003570383647456765,
... |
722,190 | openap.thrust | __init__ | Initialize Thrust object.
Args:
ac (string): ICAO aircraft type (for example: A320).
eng (string): Engine type (for example: CFM56-5A3).
| def __init__(self, ac, eng=None, **kwargs):
"""Initialize Thrust object.
Args:
ac (string): ICAO aircraft type (for example: A320).
eng (string): Engine type (for example: CFM56-5A3).
"""
if not hasattr(self, "np"):
self.np = importlib.import_module("numpy")
if not hasattr(se... | (self, ac, eng=None, **kwargs) | [
0.01288728415966034,
-0.0051413001492619514,
-0.03116544708609581,
0.020746711641550064,
-0.018250934779644012,
-0.062403496354818344,
-0.07986485958099365,
-0.009502103552222252,
-0.06937351822853088,
-0.026046834886074066,
0.018577655777335167,
0.04962512105703354,
-0.05724858492612839,
... |
722,191 | openap.thrust | _dfunc | null | def _dfunc(self, mratio):
d = -0.4204 * mratio + 1.0824
return d
| (self, mratio) | [
0.01283914316445589,
-0.00965355709195137,
0.06304292380809784,
0.052447766065597534,
0.01205594651401043,
0.0012418944388628006,
0.022369500249624252,
-0.032014258205890656,
-0.09686996787786484,
0.06209252402186394,
0.01198554690927267,
0.017221523448824883,
0.051426973193883896,
0.02891... |
722,192 | openap.thrust | _mfunc | null | def _mfunc(self, vratio, roc):
m = -1.2043e-1 * vratio - 8.8889e-9 * roc**2 + 2.4444e-5 * roc + 4.7379e-1
return m
| (self, vratio, roc) | [
0.020328842103481293,
0.01908494345843792,
0.030120093375444412,
0.05842765048146248,
0.03054657205939293,
-0.035753171890974045,
-0.010972954332828522,
-0.05657957121729851,
-0.052172619849443436,
0.04463815689086914,
-0.006170620676130056,
0.036748290061950684,
0.05835656821727753,
0.051... |
722,193 | openap.thrust | _nfunc | null | def _nfunc(self, roc):
# n = self.np.where(roc<1500, 0.89, self.np.where(roc<2500, 0.93, 0.97))
n = 2.667e-05 * roc + 0.8633
return n
| (self, roc) | [
-0.06991326063871384,
0.018797604367136955,
0.037158481776714325,
0.03337348252534866,
0.04632981866598129,
0.004940513055771589,
-0.061906538903713226,
-0.036066655069589615,
0.020762892439961433,
-0.047421645373106,
0.013292982243001461,
0.01660485379397869,
0.060996681451797485,
-0.0306... |
722,194 | openap.thrust | climb | Calculate thrust during the climb.
Args:
tas (float or ndarray): True airspeed (kt).
alt (float or ndarray): Altitude(ft)
roc (float or ndarray): Vertical rate (ft/min).
Returns:
float or ndarray: Total thrust (unit: N).
| """OpenAP thrust model.
Simplified two-shaft turbonfan model base on:
- M. Bartel, T. M. Young, Simplified Thrust and Fuel Consumption
Models for Modern Two-Shaft Turbonfan Engines
- C. Svoboda, Turbofan engine database as a preliminary desgin (cruise thrust)
"""
import importlib
from openap import pr... | (self, tas, alt, roc) | [
-0.02900388278067112,
-0.010782808996737003,
-0.01144101470708847,
0.012104572728276253,
0.0010294505627825856,
-0.06233159080147743,
-0.07209230959415436,
-0.0468343123793602,
-0.08938761055469513,
-0.026114197447896004,
-0.0003678998036775738,
0.024230550974607468,
0.0043372041545808315,
... |
722,195 | openap.thrust | cruise | Calculate thrust at the cruise.
Args:
tas (float or ndarray): True airspeed (kt).
alt (float or ndarray): Altitude (ft).
Returns:
float or ndarray: Total thrust (unit: N).
| """OpenAP thrust model.
Simplified two-shaft turbonfan model base on:
- M. Bartel, T. M. Young, Simplified Thrust and Fuel Consumption
Models for Modern Two-Shaft Turbonfan Engines
- C. Svoboda, Turbofan engine database as a preliminary desgin (cruise thrust)
"""
import importlib
from openap import pr... | (self, tas, alt) | [
-0.029005305841565132,
-0.010788689367473125,
-0.011420170776546001,
0.012105166912078857,
0.001048900419846177,
-0.062291838228702545,
-0.07205303758382797,
-0.04683661460876465,
-0.08930637687444687,
-0.026094073429703712,
-0.00039099634159356356,
0.02425314486026764,
0.004356147721409798,... |
722,196 | openap.thrust | descent_idle | Idle thrust during the descent.
Note: The idle thrust at the descent is taken as 7% of the maximum
avaiable thrust. This may (likely) differ from actual idle thrust.
Args:
tas (float or ndarray): True airspeed (kt).
alt (float or ndarray): Altitude(ft)
Returns:... | def descent_idle(self, tas, alt):
"""Idle thrust during the descent.
Note: The idle thrust at the descent is taken as 7% of the maximum
avaiable thrust. This may (likely) differ from actual idle thrust.
Args:
tas (float or ndarray): True airspeed (kt).
alt (float or ndarray): Altitude(ft... | (self, tas, alt) | [
-0.008280395530164242,
0.0062927184626460075,
0.09150960296392441,
-0.035988423973321915,
0.01972387358546257,
-0.060050785541534424,
-0.023718340322375298,
-0.07797810435295105,
-0.060012560337781906,
-0.00082720338832587,
-0.015547840856015682,
-0.026738081127405167,
-0.031057456508278847,... |
722,197 | openap.thrust | takeoff | Calculate thrust at takeoff condition.
Args:
tas (float or ndarray): True airspeed (kt).
alt (float or ndarray): Altitude of the runway (ft). Defaults to 0.
Returns:
float or ndarray: Total thrust (unit: N).
| """OpenAP thrust model.
Simplified two-shaft turbonfan model base on:
- M. Bartel, T. M. Young, Simplified Thrust and Fuel Consumption
Models for Modern Two-Shaft Turbonfan Engines
- C. Svoboda, Turbofan engine database as a preliminary desgin (cruise thrust)
"""
import importlib
from openap import pr... | (self, tas, alt=None) | [
-0.02900388278067112,
-0.010782808996737003,
-0.01144101470708847,
0.012104572728276253,
0.0010294505627825856,
-0.06233159080147743,
-0.07209230959415436,
-0.0468343123793602,
-0.08938761055469513,
-0.026114197447896004,
-0.0003678998036775738,
0.024230550974607468,
0.0043372041545808315,
... |
722,198 | openap.kinematic | WRAP | Construct the kinematic model of the aicraft. | class WRAP(object):
"""Construct the kinematic model of the aicraft."""
def __init__(self, ac, **kwargs):
"""Initialize WRAP object.
Args:
ac (string): ICAO aircraft type (for example: A320).
"""
super(WRAP, self).__init__()
self.ac = ac.lower()
s... | (ac, **kwargs) | [
0.05496084317564964,
-0.03791225329041481,
-0.045741092413663864,
0.01792287826538086,
0.009145238436758518,
-0.0470922626554966,
-0.061994876712560654,
-0.051106035709381104,
-0.00938864704221487,
-0.03143458068370819,
-0.06930709630250931,
0.01893625594675541,
-0.026029901579022408,
0.01... |
722,199 | openap.kinematic | __init__ | Initialize WRAP object.
Args:
ac (string): ICAO aircraft type (for example: A320).
| def __init__(self, ac, **kwargs):
"""Initialize WRAP object.
Args:
ac (string): ICAO aircraft type (for example: A320).
"""
super(WRAP, self).__init__()
self.ac = ac.lower()
self.use_synonym = kwargs.get("use_synonym", False)
wrap_files = glob.glob(dir_wrap + "*.txt")
ac_wrap_ava... | (self, ac, **kwargs) | [
0.03679367154836655,
-0.021762222051620483,
0.011061560362577438,
0.02658022567629814,
-0.0032706488855183125,
-0.04760260507464409,
-0.03024335205554962,
0.009663076139986515,
0.03181326389312744,
-0.007150315213948488,
-0.03246288374066353,
0.014093113131821156,
-0.0182975884526968,
0.00... |
722,200 | openap.kinematic | _get_var | null | def _get_var(self, var):
r = self.df[self.df["variable"] == var]
if r.shape[0] == 0:
raise RuntimeError("variable not found")
v = r.values[0]
res = {
"default": v[3],
"minimum": v[4],
"maximum": v[5],
"statmodel": v[6],
"statmodel_params": [float(i) for i ... | (self, var) | [
0.12189515680074692,
0.03488787263631821,
0.028959333896636963,
-0.033188726752996445,
0.03512796759605408,
0.023529458791017532,
0.02698315493762493,
-0.00876352284103632,
0.021091556176543236,
-0.01268817763775587,
-0.010102522559463978,
0.03145264461636543,
-0.05673665553331375,
-0.0727... |
722,201 | openap.kinematic | climb_const_mach | Get speed during constant Mach climb. | def climb_const_mach(self):
"""Get speed during constant Mach climb."""
return self._get_var("cl_v_mach_const")
| (self) | [
0.06194981932640076,
-0.005386035423725843,
-0.014196139760315418,
0.04178863763809204,
0.027725793421268463,
-0.008872587233781815,
-0.009414106607437134,
-0.042421795427799225,
-0.06144995614886284,
-0.02679271437227726,
-0.010713753290474415,
0.029108751565217972,
0.01612061634659767,
0... |
722,202 | openap.kinematic | climb_const_vcas | Get speed for constant CAS climb. | def climb_const_vcas(self):
"""Get speed for constant CAS climb."""
return self._get_var("cl_v_cas_const")
| (self) | [
0.0024237337056547403,
-0.018760651350021362,
-0.012427068315446377,
0.02088012546300888,
0.052556317299604416,
0.009794285520911217,
-0.017336629331111908,
-0.07192962616682053,
0.025450238958001137,
-0.054245270788669586,
-0.012402230873703957,
0.024489853531122208,
-0.003655263688415289,
... |
722,203 | openap.kinematic | climb_cross_alt_concas | Get cross over altitude when constant CAS climb starts. | def climb_cross_alt_concas(self):
"""Get cross over altitude when constant CAS climb starts."""
return self._get_var("cl_h_cas_const")
| (self) | [
-0.031195465475320816,
0.0034016782883554697,
0.028128447011113167,
0.05117344111204147,
0.051003992557525635,
-0.01339490246027708,
0.017639586701989174,
-0.07265950739383698,
0.027857329696416855,
-0.060730334371328354,
-0.006968568544834852,
-0.008065748028457165,
-0.021943578496575356,
... |
722,204 | openap.kinematic | climb_cross_alt_conmach | Get cross over altitude from constant CAS to Mach climb. | def climb_cross_alt_conmach(self):
"""Get cross over altitude from constant CAS to Mach climb."""
return self._get_var("cl_h_mach_const")
| (self) | [
0.025992676615715027,
0.0174130629748106,
0.033624641597270966,
0.055945176631212234,
0.02413122169673443,
-0.03624759986996651,
0.01572929322719574,
-0.07425512373447418,
-0.01832686737179756,
-0.03844750300049782,
-0.019088372588157654,
0.010635675862431526,
-0.007183522917330265,
-0.012... |
722,205 | openap.kinematic | climb_range | Get climb range distance (in km). | def climb_range(self):
"""Get climb range distance (in km)."""
return self._get_var("cl_d_range")
| (self) | [
0.01858689822256565,
0.023860866203904152,
-0.01228885818272829,
-0.00459125405177474,
-0.018603965640068054,
0.0427037850022316,
0.015241597779095173,
-0.0327361524105072,
-0.014482078142464161,
-0.022222353145480156,
-0.06014713644981384,
-0.01858689822256565,
0.0023959006648510695,
0.04... |
722,206 | openap.kinematic | climb_vs_concas | Get vertical rate during constant CAS climb. | def climb_vs_concas(self):
"""Get vertical rate during constant CAS climb."""
return self._get_var("cl_vs_avg_cas_const")
| (self) | [
-0.006794804707169533,
-0.038879990577697754,
0.015294578857719898,
0.03901371359825134,
0.05833670124411583,
0.014082713983952999,
0.007062251213937998,
-0.06987031549215317,
0.029385650530457497,
0.0009240474901162088,
-0.016238998621702194,
-0.0173505712300539,
0.0025156657211482525,
-0... |
722,207 | openap.kinematic | climb_vs_conmach | Get vertical rate during constant Mach climb. | def climb_vs_conmach(self):
"""Get vertical rate during constant Mach climb."""
return self._get_var("cl_vs_avg_mach_const")
| (self) | [
0.04180153086781502,
-0.029394837096333504,
0.013894828967750072,
0.04738621413707733,
0.026468729600310326,
-0.006224248092621565,
0.00377676822245121,
-0.05624813959002495,
-0.024980595335364342,
0.035982757806777954,
-0.030699044466018677,
-0.007152242120355368,
0.024060960859060287,
-0... |
722,208 | openap.kinematic | climb_vs_pre_concas | Get vertical rate before constant CAS climb. | def climb_vs_pre_concas(self):
"""Get vertical rate before constant CAS climb."""
return self._get_var("cl_vs_avg_pre_cas")
| (self) | [
-0.02288190834224224,
-0.007150596007704735,
0.010273509658873081,
0.05016674846410751,
0.05813872441649437,
0.020396919921040535,
0.0234823077917099,
-0.07478314638137817,
0.04583052545785904,
0.0026330037508159876,
0.0006921276799403131,
-0.025350218638777733,
-0.007300696335732937,
-0.0... |
722,209 | openap.kinematic | cruise_alt | Get average cruise altitude. | def cruise_alt(self):
"""Get average cruise altitude."""
return self._get_var("cr_h_mean")
| (self) | [
-0.005807104986160994,
-0.01861664466559887,
0.06517521291971207,
0.05612121522426605,
0.04438832029700279,
-0.042760636657476425,
-0.010495176538825035,
-0.06649770587682724,
0.018955746665596962,
0.005696896929293871,
-0.011292063631117344,
-0.013377535156905651,
-0.014191376976668835,
0... |
722,210 | openap.kinematic | cruise_init_alt | Get initial crusie altitude. | def cruise_init_alt(self):
"""Get initial crusie altitude."""
return self._get_var("cr_h_init")
| (self) | [
0.005577621050179005,
-0.00864205788820982,
0.061705417931079865,
0.04034985601902008,
0.00901100505143404,
-0.04215553030371666,
0.013169262558221817,
-0.02630380168557167,
0.016459409147500992,
-0.016806652769446373,
-0.0006310091121122241,
0.023716825991868973,
-0.020348550751805305,
0.... |
722,211 | openap.kinematic | cruise_mach | Get average crusie Mach number. | def cruise_mach(self):
"""Get average crusie Mach number."""
return self._get_var("cr_v_mach_mean")
| (self) | [
0.030866719782352448,
0.03133951500058174,
0.02971850521862507,
0.07659269124269485,
0.03329823538661003,
-0.018101271241903305,
-0.031407058238983154,
-0.0394107922911644,
0.005188074428588152,
0.02164722979068756,
-0.005610212218016386,
0.02154591679573059,
0.020059991627931595,
0.003887... |
722,212 | openap.kinematic | cruise_range | Get crusie range. | def cruise_range(self):
"""Get crusie range."""
return self._get_var("cr_d_range")
| (self) | [
0.0010678424732759595,
0.025820283219218254,
-0.001244250452145934,
0.013402831740677357,
-0.03296846151351929,
0.021260816603899002,
-0.015732670202851295,
-0.03570748120546341,
0.021127205342054367,
-0.056149933487176895,
-0.011757749132812023,
0.02106039971113205,
0.0022672079503536224,
... |
722,213 | openap.kinematic | descent_const_mach | Get speed during the constant Mach descent. | def descent_const_mach(self):
"""Get speed during the constant Mach descent."""
return self._get_var("de_v_mach_const")
| (self) | [
0.07999421656131744,
0.0017544412985444069,
0.016261283308267593,
0.028884954750537872,
0.03660865128040314,
-0.014716544188559055,
-0.012349605560302734,
-0.06491225212812424,
-0.10118869692087173,
0.0025932511780411005,
0.002008783398196101,
0.02599479816854,
-0.004555318504571915,
0.006... |
722,214 | openap.kinematic | descent_const_vcas | Get speed during the constant CAS descent. | def descent_const_vcas(self):
"""Get speed during the constant CAS descent."""
return self._get_var("de_v_cas_const")
| (self) | [
0.018862029537558556,
-0.024746054783463478,
0.017204558476805687,
0.007549784611910582,
0.0597684383392334,
0.008287359960377216,
-0.015447637997567654,
-0.09189024567604065,
-0.007848129607737064,
-0.015596810728311539,
-0.010823291726410389,
0.011287383735179901,
-0.014834373258054256,
... |
722,215 | openap.kinematic | descent_cross_alt_concas | Get crossover altitude from constant Mach to CAS descent. | def descent_cross_alt_concas(self):
"""Get crossover altitude from constant Mach to CAS descent."""
return self._get_var("de_h_cas_const")
| (self) | [
-0.015142948366701603,
0.011470657773315907,
0.056504543870687485,
0.042487651109695435,
0.03583214804530144,
-0.04574817419052124,
0.007546264212578535,
-0.10373172163963318,
0.007760551292449236,
-0.03154641017317772,
-0.007315170019865036,
-0.007558869197964668,
-0.028470760211348534,
-... |
722,216 | openap.kinematic | descent_cross_alt_conmach | Get crossover altitude from constant Mach to CAS descent. | def descent_cross_alt_conmach(self):
"""Get crossover altitude from constant Mach to CAS descent."""
return self._get_var("de_h_mach_const")
| (self) | [
0.02887927182018757,
0.016980407759547234,
0.05494105443358421,
0.05370001494884491,
0.019973991438746452,
-0.05889895558357239,
0.009517413564026356,
-0.09492257982492447,
-0.04504629597067833,
-0.009072988294064999,
-0.011630531400442123,
-0.0053876107558608055,
-0.014942758716642857,
-0... |
722,217 | openap.kinematic | descent_range | Get descent range. | def descent_range(self):
"""Get descent range."""
return self._get_var("de_d_range")
| (self) | [
0.03641067445278168,
0.012353622354567051,
0.009028596803545952,
-0.005954593885689974,
-0.005514274816960096,
0.020641494542360306,
0.004399074707180262,
-0.08868928998708725,
-0.03887975215911865,
-0.04256691038608551,
-0.019258810207247734,
-0.014542871154844761,
-0.050698406994342804,
... |
722,218 | openap.kinematic | descent_vs_concas | Get vertical rate during constant CAS descent. | def descent_vs_concas(self):
"""Get vertical rate during constant CAS descent."""
return self._get_var("de_vs_avg_cas_const")
| (self) | [
0.006168300751596689,
-0.04406764358282089,
0.04667361453175545,
0.030286064371466637,
0.07296719402074814,
-0.005353934597223997,
0.005391520913690329,
-0.10036330670118332,
0.01667153462767601,
0.011117140762507915,
-0.007362704258412123,
-0.02273542992770672,
-0.02846522629261017,
-0.02... |
722,219 | openap.kinematic | descent_vs_conmach | Get vertical rate during constant Mach descent. | def descent_vs_conmach(self):
"""Get vertical rate during constant Mach descent."""
return self._get_var("de_vs_avg_mach_const")
| (self) | [
0.061912231147289276,
-0.027728384360671043,
0.045255132019519806,
0.0398700051009655,
0.03702692687511444,
-0.02324635349214077,
-0.0010786977363750339,
-0.08810200542211533,
-0.04234515503048897,
0.05244645103812218,
-0.018229154869914055,
-0.013897639699280262,
-0.007709762081503868,
-0... |
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