1i \SrSSKrSSKJrJrJrJrJrJr \\\S\\\4Sjr \\4Sjr Sr g) z(Various elevation-related calculations N)standard_pressurestandard_temperatureearth_temperature_lapse_rateair_gas_constant earth_gravityearth_atmosphere_molar_massgcjUS:a[R"S5 XX#X- --- Xg-XS-- --$)aUThis function returns an estimate of the pressure in pascals as a function of elevation above sea level. NOTES: * This equation is only accurate up to 11,000 meters * results might be odd for elevations below 0 (sea level), like Dead Sea. h=elevation relative to sea level (m) Ps= static pressure (pascals) Ts= temperature (kelvin) Tl= temperature lapse rate (kelvin/meter) Hb= height at the bottom of the layer R= universal gas constant for air g= gravitational acceleration M= Molar mass of atmosphere P = Ps * (Ts / ((Ts + Tl) * (h - Hb))) ^ ((g * M)/(R * Tl)) returns pressure in pascals g|@zUElevation used exceeds the recommended maximum elevation for this function (11,000m) )warningswarn)hPsTsTlHbRgMs T/var/www/html/motor_solar_iot/venv/lib/python3.13/site-packages/pysolar/elevation.pyget_pressure_with_elevationrsD  7{ d Bqv&'ae-? @@AcXU--$)a4This function returns an estimate of temperature as a function above sea level. NOTES: * This equation is only accurate up to 11,000 meters * results might be odd for elevations below 0 (sea level), like Dead Sea. Ts= temperature (kelvin) Tl= temperature lapse rate (kelvin/meter) returns temp in kelvin )r rrs rget_temperature_with_elevationr8s U rc[S5 Sn[S5H.n[U5n[U5n[SXU4-5 US- nM0 g)Nz(Elevation(m) Pressure(Pa) Temperature(K)r z%i %i %ii)printrangerr)r _PTs relevation_testr"DsL 45 A 2Y ' * *1 - jA!9$% T  r) __doc__r constantsrrrrrr rrr"rrrr%sT$  '8B^ r