AeroUtils.h File Reference

#include <utils/Constants.h>
#include <Eigen/Core>
#include <cmath>

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Classes
struct	Boardcore::Aeroutils::AerodynamicCoeff

Namespaces
namespace	Boardcore
	This file includes all the types the logdecoder script will decode.
namespace	Boardcore::Aeroutils

Functions
float	Boardcore::Aeroutils::relAltitude (float pressure, float pressureRef=Constants::MSL_PRESSURE, float temperatureRef=Constants::MSL_TEMPERATURE)
	Returns the altitude given the pressure with respect to a reference pressure and temperature, using International Standard Atmosphere model.
float	Boardcore::Aeroutils::relPressure (float altitude, float pressureRef=Constants::MSL_PRESSURE, float temperatureRef=Constants::MSL_TEMPERATURE)
	Returns the pressure given the altitude with respect to a reference pressure and temperature, using International Standard Atmosphere model.
float	Boardcore::Aeroutils::relTemperature (float altitude, float temperatureRef=Constants::MSL_TEMPERATURE)
	Returns the temperature at the given altitude with respect to the reference temperature.
float	Boardcore::Aeroutils::relDensity (float pressure, float pressureRef=Constants::MSL_PRESSURE, float altitudeRef=0, float temperatureRef=Constants::MSL_TEMPERATURE)
	Returns the air density given the pressure with respect to a reference pressure, altitude and temperature, using the International Standard Atmosphere model.
float	Boardcore::Aeroutils::mslPressure (float pressureRef, float temperatureRef, float altitudeRef)
	Returns the expected pressure at mean sea level based on temperature and pressure at a reference altitude, using International Standard Atmosphere model.
float	Boardcore::Aeroutils::mslTemperature (float temperatureRef, float altitudeRef)
	Returns the expected temperature at mean sea level based on temperature at a reference altitude, using International Standard Atmosphere model.
float	Boardcore::Aeroutils::verticalSpeed (float p, float dpDt, float pRef, float tRef)
Eigen::Vector2f	Boardcore::Aeroutils::geodetic2NED (const Eigen::Vector2f &target, const Eigen::Vector2f &origin)
	Converts decimal degrees of latitude and longitude into displacement in meters between two positions the with an ellipsoidal earth model.
float	Boardcore::Aeroutils::computeRho (float d, float t0)
	Computes the rho (air density) of air at the given altitude.
float	Boardcore::Aeroutils::computeSoundSpeed (float d, float t0)
	Computes the speed of sound at the given altitude.
float	Boardcore::Aeroutils::computeMach (float d, float vtot, float t0)
	Computes the mach relative to the speed at a certain altitude.
float	Boardcore::Aeroutils::computePitotMach (float pressureTotal, float pressureStatic)
	Computes the mach from total and static pressure measures from a pitot tube.
float	Boardcore::Aeroutils::computePitotAirspeed (float pressureTotal, float pressureStatic, float d, float t0)
	Computes air speed relative to the pitot tube.
float	Boardcore::Aeroutils::computeCd (const AerodynamicCoeff &coeff, float mach)
	Computes the CD from aerodynamic coefficients and mach.