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// This file is part of INSTINCT, the INS Toolkit for Integrated |
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// Navigation Concepts and Training by the Institute of Navigation of |
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// the University of Stuttgart, Germany. |
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// |
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// This Source Code Form is subject to the terms of the Mozilla Public |
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// License, v. 2.0. If a copy of the MPL was not distributed with this |
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// file, You can obtain one at https://mozilla.org/MPL/2.0/. |
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/// @file StandardAtmosphere.hpp |
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/// @brief Standard Atmosphere pressure model |
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/// @author T. Topp (topp@ins.uni-stuttgart.de) |
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/// @date 2023-01-31 |
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#pragma once |
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#include <gcem.hpp> |
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namespace NAV |
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{ |
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/// @brief Calculates the standard atmosphere total pressure |
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/// @param[in] altitudeMSL Geodetic height above MSL (mean sea level) [m] |
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/// @return The total pressure in [hPa] = [mbar] |
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/// @note See \cite RTKLIB RTKLIB ch. E.5, eq. E.5.1, p. 149 |
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[[nodiscard]] constexpr double calcTotalPressureStAtm(double altitudeMSL) |
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{ |
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return 1013.25 * gcem::pow(1 - 2.2557e-5 * altitudeMSL, 5.2568); |
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} |
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} // namespace NAV |
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