Skeleton for Mars DTM atmosphere

include/tudat/astro/aerodynamics/marsDtmAtmosphereModel.h

@@ -0,0 +1,106 @@
+/*    Copyright (c) 2010-2019, Delft University of Technology
+ *    All rigths reserved
+ *
+ *    This file is part of the Tudat. Redistribution and use in source and
+ *    binary forms, with or without modification, are permitted exclusively
+ *    under the terms of the Modified BSD license. You should have received
+ *    a copy of the license with this file. If not, please or visit:
+ *    http://tudat.tudelft.nl/LICENSE.
+ *
+ */
+
+#ifndef TUDAT_MARS_DTM_ATMOSPHERE_MODEL_H
+#define TUDAT_MARS_DTM_ATMOSPHERE_MODEL_H
+
+#include "tudat/astro/aerodynamics/atmosphereModel.h"
+
+namespace tudat
+{
+
+namespace aerodynamics
+{
+
+class MarsDtmAtmosphereModel: public AtmosphereModel
+{
+public:
+
+    MarsDtmAtmosphereModel( ){ }
+
+    //! Default destructor.
+    /*!
+    * Default destructor.
+    */
+    virtual ~MarsDtmAtmosphereModel( ) { }
+
+    //! Get local density.
+    /*!
+    * Returns the local density parameter of the atmosphere in kg per meter^3.
+    * \param altitude Altitude.
+    * \param longitude Longitude.
+    * \param latitude Latitude.
+    * \param time Time.
+    * \return Atmospheric density.
+    */
+    virtual double getDensity( const double altitude, const double longitude,
+                               const double latitude, const double time )
+    {
+
+    }
+
+    //! Get local pressure.
+    /*!
+    * Returns the local pressure of the atmosphere parameter in Newton per meter^2.
+    * \param altitude Altitude.
+    * \param longitude Longitude.
+    * \param latitude Latitude.
+    * \param time Time.
+    * \return Atmospheric pressure.
+    */
+    virtual double getPressure( const double altitude, const double longitude,
+                                const double latitude, const double time )
+    {
+
+    }
+
+    //! Get local temperature.
+    /*!
+    * Returns the local temperature of the atmosphere parameter in Kelvin.
+    * \param altitude Altitude.
+    * \param longitude Longitude.
+    * \param latitude Latitude.
+    * \param time Time.
+    * \return Atmospheric temperature.
+    */
+    virtual double getTemperature( const double altitude, const double longitude,
+                                   const double latitude, const double time )
+    {
+
+    }
+
+    //! Get local speed of sound.
+    /*!
+    * Returns the local speed of sound of the atmosphere in m/s.
+    * \param altitude Altitude.
+    * \param longitude Longitude.
+    * \param latitude Latitude.
+    * \param time Time.
+    * \return Atmospheric speed of sound.
+    */
+    virtual double getSpeedOfSound( const double altitude, const double longitude,
+                                    const double latitude, const double time )
+    {
+
+    }
+
+protected:
+
+private:
+
+};
+
+
+} // namespace aerodynamics
+
+} // namespace tudat
+
+#endif // TUDAT_MARS_DTM_ATMOSPHERE_MODEL_H

src/astro/aerodynamics/CMakeLists.txt

@@ -23,7 +23,8 @@ set(aerodynamics_SOURCES
         "flightConditions.cpp"
         "trimOrientation.cpp"
         "equilibriumWallTemperature.cpp"
-        )
+        "marsDtmAtmosphereModel.cpp"
+)
 
 # Set the header files.
 set(aerodynamics_HEADERS
@@ -46,7 +47,8 @@ set(aerodynamics_HEADERS
         "aerodynamicGuidance.h"
         "equilibriumWallTemperature.h"
         "windModel.h"
-        )
+        "marsDtmAtmosphereModel.h"
+)
 
 if (TUDAT_BUILD_WITH_NRLMSISE00)
     set(aerodynamics_SOURCES

src/astro/aerodynamics/marsDtmAtmosphereModel.cpp

@@ -0,0 +1,11 @@
+
+#include "tudat/astro/aerodynamics/marsDtmAtmosphereModel.h"
+
+namespace tudat
+{
+namespace aerodynamics
+{
+
+} // namespace aerodynamics
+
+} // namespace tudat

tests/src/astro/aerodynamics/CMakeLists.txt

@@ -72,6 +72,11 @@ TUDAT_ADD_TEST_CASE(WindModel
         ${Tudat_PROPAGATION_LIBRARIES}
         )
 
+TUDAT_ADD_TEST_CASE(MarsDtmAtmosphere
+        PRIVATE_LINKS
+        ${Tudat_PROPAGATION_LIBRARIES}
+)
+
 if (TUDAT_BUILD_WITH_NRLMSISE00)
     TUDAT_ADD_TEST_CASE(NRLMSISE00Atmosphere
             PRIVATE_LINKS

tests/src/astro/aerodynamics/unitTestMarsDtmAtmosphere.cpp

@@ -0,0 +1,43 @@
+/*    Copyright (c) 2010-2019, Delft University of Technology
+ *    All rigths reserved
+ *
+ *    This file is part of the Tudat. Redistribution and use in source and
+ *    binary forms, with or without modification, are permitted exclusively
+ *    under the terms of the Modified BSD license. You should have received
+ *    a copy of the license with this file. If not, please or visit:
+ *    http://tudat.tudelft.nl/LICENSE.
+ *
+ *    References
+ *
+ */
+
+//#define BOOST_TEST_DYN_LINK
+//#define BOOST_TEST_MAIN
+
+#include <limits>
+
+#include <boost/test/unit_test.hpp>
+
+#include "tudat/astro/aerodynamics/marsDtmAtmosphereModel.h"
+
+int main( )
+{
+
+}
+//
+//namespace tudat
+//{
+//namespace unit_tests
+//{
+//
+//BOOST_AUTO_TEST_SUITE( test_mars_dtm_atmosphere )
+//
+//BOOST_AUTO_TEST_CASE( testMarsDtmAtmosphere )
+//{
+//
+//}
+//
+//BOOST_AUTO_TEST_SUITE_END( )
+//
+//} // namespace unit_tests
+//} // namespace tudat