NAV::InsConst::WGS84 Class Reference

World Geodetic System 1984. More...

Public Member Functions
	WGS84 ()=delete
	Default Constructor.

Static Public Attributes
static constexpr double	a
	Semi-major axis = equatorial radius.
static constexpr double	b
	Semi-minor axis = polar radius.
static constexpr double	e_squared
	Square of the first eccentricity of the ellipsoid.
static constexpr double	f
	Flattening f = (a-b)/a.
static constexpr double	J2
	Dynamic form factor, derived [-].
static constexpr double	MU
	Gravitational constant (mass of Earth’s atmosphere included) [m³/s²].
static constexpr double	omega_ie
	Earth rotation rate in [rads/s].

Detailed Description

World Geodetic System 1984.

Definition at line 43 of file Constants.hpp.

Constructor & Destructor Documentation

WGS84()

NAV::InsConst::WGS84::WGS84 ( )

delete

Default Constructor.

Field Documentation

a

double NAV::InsConst::WGS84::a

staticconstexpr

Semi-major axis = equatorial radius.

Definition at line 50 of file Constants.hpp.

b

double NAV::InsConst::WGS84::b

staticconstexpr

Semi-minor axis = polar radius.

Definition at line 54 of file Constants.hpp.

e_squared

double NAV::InsConst::WGS84::e_squared

staticconstexpr

Square of the first eccentricity of the ellipsoid.

Definition at line 56 of file Constants.hpp.

f

double NAV::InsConst::WGS84::f

staticconstexpr

Flattening f = (a-b)/a.

Definition at line 52 of file Constants.hpp.

J2

double NAV::InsConst::WGS84::J2

staticconstexpr

Dynamic form factor, derived [-].

Definition at line 60 of file Constants.hpp.

MU

double NAV::InsConst::WGS84::MU

staticconstexpr

Gravitational constant (mass of Earth’s atmosphere included) [m³/s²].

Definition at line 58 of file Constants.hpp.

omega_ie

double NAV::InsConst::WGS84::omega_ie

staticconstexpr

Earth rotation rate in [rads/s].

Definition at line 62 of file Constants.hpp.

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The documentation for this class was generated from the following file:

• /home/runner/work/INSTINCT/INSTINCT/src/Navigation/Constants.hpp