ns3::LeoOrbitalShell Class Reference

Orbit definition. More...

#include "leo-orbital-shell.h"

Collaboration diagram for ns3::LeoOrbitalShell:

Public Member Functions
	LeoOrbitalShell ()=default
	constructor
	LeoOrbitalShell (double a, double i, std::size_t p, std::size_t s, double f=0, double r=360.0)
	Constructor.

Public Attributes
double	alt
	Altitude of orbit (km, from earth surface).
double	inc
	Inclination of orbit (degrees).
double	phasing {0}
	Walker Delta phasing factor F (0 means no inter-plane stagger).
std::size_t	planes
	Number of planes with that altitude and inclination.
double	raanSpanDeg {360.0}
	RAAN span in degrees (360 for Walker Delta, 180 for Walker Star).
std::size_t	sats
	Number of satellites in those planes.

Detailed Description

Orbit definition.

Definition at line 75 of file leo-orbital-shell.h.

Constructor & Destructor Documentation

LeoOrbitalShell() [1/2]

ns3::LeoOrbitalShell::LeoOrbitalShell ( )

default

constructor

LeoOrbitalShell() [2/2]

ns3::LeoOrbitalShell::LeoOrbitalShell ( double a, double i, std::size_t p, std::size_t s, double f = 0, double r = 360.0 )

inline

Constructor.

Parameters

a	altitude (km, from earth surface)
i	inclination (degrees)
p	number of planes
s	number of satellites per plane
f	Walker Delta phasing factor (default 0)
r	RAAN span in degrees (360 for Walker Delta, 180 for Walker Star)

Definition at line 90 of file leo-orbital-shell.h.

References alt, inc, phasing, planes, r, raanSpanDeg, and sats.

Member Data Documentation

alt

double ns3::LeoOrbitalShell::alt

Altitude of orbit (km, from earth surface).

Definition at line 106 of file leo-orbital-shell.h.

Referenced by LeoOrbitalShell(), ns3::LeoOrbitNodeHelper::CreateNodesAndInstallMobility(), LeoOrbitConstructorTestCase::DoRun(), LeoOrbitSerializationTestCase::DoRun(), ns3::LeoOrbitNodeHelper::Install(), ns3::operator<<(), and ns3::operator>>().

inc

double ns3::LeoOrbitalShell::inc

Inclination of orbit (degrees).

Definition at line 108 of file leo-orbital-shell.h.

Referenced by LeoOrbitalShell(), ns3::LeoOrbitNodeHelper::CreateNodesAndInstallMobility(), LeoOrbitConstructorTestCase::DoRun(), LeoOrbitSerializationTestCase::DoRun(), ns3::LeoOrbitNodeHelper::Install(), ns3::operator<<(), and ns3::operator>>().

phasing

double ns3::LeoOrbitalShell::phasing {0}

Walker Delta phasing factor F (0 means no inter-plane stagger).

Definition at line 114 of file leo-orbital-shell.h.

Referenced by LeoOrbitalShell(), ns3::LeoOrbitNodeHelper::CreateNodesAndInstallMobility(), LeoOrbitConstructorTestCase::DoRun(), LeoOrbitSerializationTestCase::DoRun(), ns3::LeoOrbitNodeHelper::Install(), ns3::operator<<(), and ns3::operator>>().

planes

std::size_t ns3::LeoOrbitalShell::planes

Number of planes with that altitude and inclination.

Definition at line 110 of file leo-orbital-shell.h.

Referenced by LeoOrbitalShell(), ns3::LeoOrbitNodeHelper::CalculateNumberOfOrbitSatellites(), ns3::LeoOrbitNodeHelper::CreateNodesAndInstallMobility(), LeoOrbitConstructorTestCase::DoRun(), LeoOrbitSerializationTestCase::DoRun(), ns3::LeoOrbitNodeHelper::Install(), ns3::operator<<(), and ns3::operator>>().

raanSpanDeg

double ns3::LeoOrbitalShell::raanSpanDeg {360.0}

RAAN span in degrees (360 for Walker Delta, 180 for Walker Star).

Definition at line 116 of file leo-orbital-shell.h.

Referenced by LeoOrbitalShell(), ns3::LeoOrbitNodeHelper::CreateNodesAndInstallMobility(), LeoOrbitConstructorTestCase::DoRun(), LeoOrbitSerializationTestCase::DoRun(), ns3::LeoOrbitNodeHelper::Install(), ns3::operator<<(), and ns3::operator>>().

sats

std::size_t ns3::LeoOrbitalShell::sats

Number of satellites in those planes.

Definition at line 112 of file leo-orbital-shell.h.

Referenced by LeoOrbitalShell(), ns3::LeoOrbitNodeHelper::CalculateNumberOfOrbitSatellites(), ns3::LeoOrbitNodeHelper::CreateNodesAndInstallMobility(), LeoOrbitConstructorTestCase::DoRun(), LeoOrbitSerializationTestCase::DoRun(), ns3::LeoOrbitNodeHelper::Install(), ns3::operator<<(), and ns3::operator>>().

---

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

• src/mobility/model/leo-orbital-shell.h