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[T, a, P, rho]
= atmoslapse(height, g, heatRatio, characteristicGasConstant, lapseRate, heightTroposphere, heightTropopause, density0, pressure0, temperature0)
[T, a, P, rho] = atmoslapse(height, g, heatRatio, characteristicGasConstant, lapseRate, heightTroposphere, heightTropopause, density0, pressure0, temperature0) implements the mathematical representation of the lapse rate atmospheric equations for ambient temperature, pressure, density, and speed of sound for the input geopotential altitude. To customize this atmospheric model, specify the atmospheric properties in the function input.
The function holds temperature and pressure values below the geopotential altitude of 0 km and above the geopotential altitude of the tropopause.
Calculate the atmosphere at 1000 m with the International Standard Atmosphere input values:
[T, a, P, rho] = atmoslapse(1000, 9.80665, 1.4, 287.0531, 0.0065, ...
11000, 20000, 1.225, 101325, 288.15 )
T =
281.6500
a =
336.4341
P =
8.9875e+004
rho =
1.1116U.S. Standard Atmosphere, 1976, U.S. Government Printing Office, Washington, D.C.
atmoscira | atmoscoesa | atmosisa | atmosnonstd | atmospalt

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