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SUPPORT SITE |
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Path: AerospaceUtils/AtmosphericCalculations
% Computes the atmospheric temperature using a simplified model.
Type AtmTemp for demo.
Since version 1.
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Form:
tOut = AtmTemp( h )
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Inputs
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h (1,:) Altitude (km)
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Outputs
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tOut (1,:) Atmospheric Temperature (�K)
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References: Wertz, J.R., Spacecraft Attitude Determination and Control,
Kluwer, 1976, p. 820.
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Common: Graphics/Plot2D
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