minisky.quantities¶
quantities
¶
Physical quantity annotations and unit conversions used by MiniSky.
minisky uses SI units internally. To convert from imperial for example:
>>> from minisky import quantities as q
>>> q.ft_to_m(1300)
396.24
Furthermore, we recommend annotating your types with quantity kind and unit metadata, for example:
>>> from minisky import quantities as q
>>> def _(alt: q.PressureAltitudeM): ...
>>> from dataclasses import dataclass
>>> @dataclass
... class Container:
... alt: q.PressureAltitudeM
...
Use unconstrained type variables where possible. Do not unnecessarily
strictly type inputs like np.ndarray | float, they destroy type information.
For more information, see: https://github.com/open-aviation/minisky/issues/38#issuecomment-5156669559
TrueHeadingDegrees
module-attribute
¶
TrueHeadingDegrees = Annotated[_T, aerospace.HEADING_TRUE(isqx.DEG)]
MagneticHeadingDegrees
module-attribute
¶
MagneticHeadingDegrees = Annotated[_T, aerospace.HEADING_MAG(isqx.DEG)]
TurnRateDegPerS
module-attribute
¶
YawRateDegPerS
module-attribute
¶
WindDirectionDeg
module-attribute
¶
WindDirectionDeg = Annotated[_T, aerospace.HEADING_TRUE_WIND(isqx.DEG)]
VerticalDistanceM
module-attribute
¶
VerticalDistanceFt
module-attribute
¶
PressureAltitudeM
module-attribute
¶
PressureAltitudeM = Annotated[_T, aerospace.PRESSURE_ALTITUDE(isqx.M)]
PressureAltitudeFt
module-attribute
¶
PressureAltitudeFt = Annotated[_T, aerospace.PRESSURE_ALTITUDE(isqx.usc.FT)]
MslAltitudeM
module-attribute
¶
MslAltitudeM = Annotated[M" backlink-type="used-by" backlink-anchor="minisky.quantities.MslAltitudeM" optional hover>M, isqx.ALTITUDE['above_mean_sea_level'](isqx.M)]
BarometricHeightM
module-attribute
¶
AglHeightM
module-attribute
¶
AglHeightM = Annotated[_T, aerospace.HEIGHT_ABOVE_GROUND_LEVEL(isqx.M)]
CalibratedAirspeedMps
module-attribute
¶
CalibratedAirspeedMps = Annotated[_T, aerospace.CALIBRATED_AIRSPEED(isqx.M_PERS)]
CalibratedAirspeedKt
module-attribute
¶
CalibratedAirspeedKt = Annotated[_T, aerospace.CALIBRATED_AIRSPEED(isqx.usc.KNOT)]
EquivalentAirspeedMps
module-attribute
¶
EquivalentAirspeedMps = Annotated[_T, aerospace.EQUIVALENT_AIRSPEED(isqx.M_PERS)]
TrueAirspeedMps
module-attribute
¶
TrueAirspeedMps = Annotated[_T, aerospace.TRUE_AIRSPEED(isqx.M_PERS)]
TrueAirspeedKt
module-attribute
¶
TrueAirspeedKt = Annotated[_T, aerospace.TRUE_AIRSPEED(isqx.usc.KNOT)]
GroundSpeedMps
module-attribute
¶
GroundSpeedMps = Annotated[_T, aerospace.GROUND_SPEED(isqx.M_PERS)]
GroundSpeedKt
module-attribute
¶
GroundSpeedKt = Annotated[_T, aerospace.GROUND_SPEED(isqx.usc.KNOT)]
VerticalRateMps
module-attribute
¶
VerticalRateMps = Annotated[_T, aerospace.VERTICAL_RATE(isqx.M * isqx.S ** -1)]
VerticalRateFpm
module-attribute
¶
AccelerationMps2
module-attribute
¶
AccelerationMps2 = Annotated[_T, isqx.ACCELERATION(isqx.M * isqx.S ** -2)]
GravitationalAccelerationMps2
module-attribute
¶
GravitationalAccelerationMps2 = Annotated[_T, isqx.ACCELERATION_OF_FREE_FALL(isqx.M_PERS2)]
SpecificGasConstantJPerKgK
module-attribute
¶
SpecificGasConstantJPerKgK = Annotated[_T, isqx.SPECIFIC_GAS_CONSTANT(isqx.J * isqx.KG ** -1 * isqx.K ** -1)]
TemperatureGradientKPerM
module-attribute
¶
PositionDiffusionMPerSqrtS
module-attribute
¶
StaticTemperatureK
module-attribute
¶
StaticTemperatureK = Annotated[_T, aerospace.STATIC_TEMPERATURE(isqx.K)]
DensityKgPerM3
module-attribute
¶
SpeedOfSoundMps
module-attribute
¶
SpeedOfSoundMps = Annotated[_T, isqx.SPEED_OF_SOUND(isqx.M_PERS)]
MassFlowKgPerS
module-attribute
¶
MassFlowKgPerS = Annotated[_T, isqx.MASS_FLOW_RATE(isqx.KG * isqx.S ** -1)]
ZeroLiftDragCoefficient
module-attribute
¶
ZeroLiftDragCoefficient = Annotated[_T, aerospace.ZERO_LIFT_DRAG_COEFFICIENT]
LiftInducedDragCoefficient
module-attribute
¶
LiftInducedDragCoefficient = Annotated[_T, aerospace.LIFT_INDUCED_DRAG_COEFFICIENT]
InducedDragFactor
module-attribute
¶
InducedDragFactor = Annotated[_T, isqx.Dimensionless('induced_drag_factor')]
kmh_to_mps
module-attribute
¶
fpm_to_mps
module-attribute
¶
fpm_per_s_to_mps2
module-attribute
¶
fpm_per_s_to_mps2 = isqx.convert(isqx.usc.FT * isqx.MIN ** -1 * isqx.S ** -1, isqx.M * isqx.S ** -2)