Keep track of the current position and velocity of satellite using SGP4 model. More...

#include "satellite-sgp4-mobility-model.h"

Inheritance diagram for ns3::SatSGP4MobilityModel:

Collaboration diagram for ns3::SatSGP4MobilityModel:

Classes
struct	Matrix
	Matrix data structure to make coordinate conversion code clearer and less verbose. More...

struct	Row
	row of a Matrix More...

Public Member Functions
	SatSGP4MobilityModel ()
	Default constructor. More...

virtual	~SatSGP4MobilityModel ()
	Destructor. More...

TypeId	GetInstanceTypeId (void) const

JulianDate	GetStartTime () const
	Get the time instant considered as the simulation start. More...

void	SetStartTime (const JulianDate &t)
	Set the time instant considered as the simulation start. More...

void	SetTleInfo (const std::string &tle)
	Set satellite's TLE information required for its initialization. More...

Public Member Functions inherited from ns3::SatMobilityModel
	SatMobilityModel ()
	Default constructor. More...

virtual	~SatMobilityModel ()=0
	Destructor for SatMobilityModel. More...

GeoCoordinate	GetGeoPosition (void) const

TypeId	GetInstanceTypeId (void) const

void	NotifyGeoCourseChange (void) const

void	SetGeoPosition (const GeoCoordinate &position)

Static Public Member Functions
static TypeId	GetTypeId (void)
	Get the type ID. More...

Static Public Member Functions inherited from ns3::SatMobilityModel
static TypeId	GetTypeId (void)
	Get the type ID. More...

Static Public Attributes
static const uint32_t	TleSatInfoWidth = 69
	Satellite's information line size defined by TLE data format. More...

static const gravconsttype	WGeoSys = wgs72
	World Geodetic System (WGS) constants to be used by SGP4/SDP4 models. More...

Private Member Functions
virtual GeoCoordinate	DoGetGeoPosition () const

virtual Vector	DoGetPosition () const

virtual Vector	DoGetVelocity () const

virtual void	DoSetGeoPosition (const GeoCoordinate &position)

virtual void	DoSetPosition (const Vector &position)

JulianDate	GetTleEpoch (void) const
	Retrieve the TLE epoch time. More...

bool	IsInitialized (void) const
	Check if the satellite has already been initialized. More...

Static Private Member Functions
static Matrix	PefToItrf (const JulianDate &t)
	Retrieve the matrix for converting from PEF to ITRF at a given time. More...

static Vector3D	rTemeTorItrf (const Vector3D &rteme, const JulianDate &t)
	Retrieve the satellite's position vector in ITRF coordinates. More...

static Vector3D	rvTemeTovItrf (const Vector3D &rteme, const Vector3D &vteme, const JulianDate &t)
	Retrieve the satellite's velocity vector in ITRF coordinates. More...

static Matrix	TemeToPef (const JulianDate &t)
	Retrieve the matrix for converting from TEME to PEF at a given time. More...

Private Attributes
GeoCoordinate	m_lastPosition
	Last saved satellite position. More...

elsetrec	m_sgp4_record
	SGP4/SDP4 record. More...

JulianDate	m_start
	Simulation absolute start time. More...

std::string	m_startStr
	Simulation absolute start time in string format. More...

Time	m_timeLastUpdate
	Last position update time. More...

std::string	m_tle1

std::string	m_tle2
	satellite's TLE data. More...

bool	m_updatePositionEachRequest
	Compute position each time a packet is transmitted. More...

Time	m_updatePositionPeriod
	Period of satellite position refresh, if UpdatePositionEachRequest is false. More...

Additional Inherited Members
Public Types inherited from ns3::SatMobilityModel
typedef void(*	CourseChangeCallback) (const Ptr< const SatMobilityModel > model)
	Callback signature for `SatCourseChange` trace source. More...

Detailed Description

Keep track of the current position and velocity of satellite using SGP4 model.

Definition at line 43 of file satellite-sgp4-mobility-model.h.

Constructor & Destructor Documentation

◆ SatSGP4MobilityModel()

ns3::SatSGP4MobilityModel::SatSGP4MobilityModel ( )

Default constructor.

Definition at line 76 of file satellite-sgp4-mobility-model.cc.

References m_startStr, and SetStartTime().

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◆ ~SatSGP4MobilityModel()

ns3::SatSGP4MobilityModel::~SatSGP4MobilityModel ( )

virtual

Destructor.

Definition at line 86 of file satellite-sgp4-mobility-model.cc.

Member Function Documentation

◆ DoGetGeoPosition()

GeoCoordinate ns3::SatSGP4MobilityModel::DoGetGeoPosition ( ) const

privatevirtual

Returns: the current position.

Concrete subclasses of this base class must implement this method.

Implements ns3::SatMobilityModel.

Definition at line 145 of file satellite-sgp4-mobility-model.cc.

References elsetrec::error, GetTleEpoch(), IsInitialized(), m_lastPosition, m_sgp4_record, m_start, m_timeLastUpdate, m_updatePositionEachRequest, m_updatePositionPeriod, rTemeTorItrf(), sgp4(), and WGeoSys.

Referenced by DoGetPosition(), and SetTleInfo().

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◆ DoGetPosition()

Vector ns3::SatSGP4MobilityModel::DoGetPosition ( void ) const

privatevirtual

Returns: cartesian format position as vector

Implementation for method defined by MobilityModel

Reimplemented from ns3::SatMobilityModel.

Definition at line 129 of file satellite-sgp4-mobility-model.cc.

References DoGetGeoPosition(), and ns3::GeoCoordinate::ToVector().

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◆ DoGetVelocity()

Vector3D ns3::SatSGP4MobilityModel::DoGetVelocity ( void ) const

privatevirtual

Definition at line 107 of file satellite-sgp4-mobility-model.cc.

References elsetrec::error, GetTleEpoch(), IsInitialized(), m_sgp4_record, m_start, rvTemeTovItrf(), sgp4(), and WGeoSys.

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◆ DoSetGeoPosition()

void ns3::SatSGP4MobilityModel::DoSetGeoPosition ( const GeoCoordinate & position )

privatevirtual

Parameters

position the position to set.

Concrete subclasses of this base class must implement this method.

Implements ns3::SatMobilityModel.

Definition at line 176 of file satellite-sgp4-mobility-model.cc.

References m_lastPosition, and ns3::SatMobilityModel::NotifyGeoCourseChange().

Referenced by DoSetPosition().

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◆ DoSetPosition()

void ns3::SatSGP4MobilityModel::DoSetPosition ( const Vector & position )

privatevirtual

Parameters

position position in Cartesian format to set

Implementation for method defined by MobilityModel

Reimplemented from ns3::SatMobilityModel.

Definition at line 137 of file satellite-sgp4-mobility-model.cc.

References DoSetGeoPosition().

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◆ GetInstanceTypeId()

TypeId ns3::SatSGP4MobilityModel::GetInstanceTypeId ( void ) const

Definition at line 71 of file satellite-sgp4-mobility-model.cc.

References GetTypeId().

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◆ GetStartTime()

JulianDate ns3::SatSGP4MobilityModel::GetStartTime ( void ) const

Get the time instant considered as the simulation start.

Returns: a JulianDate object with the time considered as simulation start.

Definition at line 91 of file satellite-sgp4-mobility-model.cc.

References m_start.

◆ GetTleEpoch()

JulianDate ns3::SatSGP4MobilityModel::GetTleEpoch ( void ) const

private

Retrieve the TLE epoch time.

Returns: the TLE epoch time or 0h, 1 January 1992 if the satellite has not yet been initialized.

Definition at line 193 of file satellite-sgp4-mobility-model.cc.

References IsInitialized(), elsetrec::jdsatepoch, and m_sgp4_record.

Referenced by DoGetGeoPosition(), DoGetVelocity(), and SetTleInfo().

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◆ GetTypeId()

TypeId ns3::SatSGP4MobilityModel::GetTypeId ( void )

static

Get the type ID.

Returns: the object TypeId.

Definition at line 45 of file satellite-sgp4-mobility-model.cc.

References m_startStr, m_updatePositionEachRequest, and m_updatePositionPeriod.

Referenced by GetInstanceTypeId().

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◆ IsInitialized()

bool ns3::SatSGP4MobilityModel::IsInitialized ( void ) const

private

Check if the satellite has already been initialized.

Returns: a boolean indicating whether the satellite is initialized.

Definition at line 185 of file satellite-sgp4-mobility-model.cc.

References elsetrec::jdsatepoch, m_sgp4_record, m_tle1, and m_tle2.

Referenced by DoGetGeoPosition(), DoGetVelocity(), and GetTleEpoch().

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◆ PefToItrf()

SatSGP4MobilityModel::Matrix ns3::SatSGP4MobilityModel::PefToItrf ( const JulianDate & t )

staticprivate

Retrieve the matrix for converting from PEF to ITRF at a given time.

Parameters

t When.

Returns: the PEF-ITRF conversion matrix.

Definition at line 270 of file satellite-sgp4-mobility-model.cc.

References ns3::JulianDate::GetPolarMotion().

Referenced by rTemeTorItrf(), and rvTemeTovItrf().

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◆ rTemeTorItrf()

Vector3D ns3::SatSGP4MobilityModel::rTemeTorItrf	(	const Vector3D &	rteme,
		const JulianDate &	t
	)

staticprivate

Retrieve the satellite's position vector in ITRF coordinates.

Parameters

t When.

Returns: the satellite's position vector in ITRF coordinates (meters).

Definition at line 249 of file satellite-sgp4-mobility-model.cc.

References PefToItrf(), and TemeToPef().

Referenced by DoGetGeoPosition().

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◆ rvTemeTovItrf()

Vector3D ns3::SatSGP4MobilityModel::rvTemeTovItrf	(	const Vector3D &	rteme,
		const Vector3D &	vteme,
		const JulianDate &	t
	)

staticprivate

Retrieve the satellite's velocity vector in ITRF coordinates.

Parameters

t When.

Returns: the satellite's velocity vector in ITRF coordinates (m/s).

Definition at line 258 of file satellite-sgp4-mobility-model.cc.

References ns3::CrossProduct(), ns3::JulianDate::GetOmegaEarth(), PefToItrf(), and TemeToPef().

Referenced by DoGetVelocity().

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◆ SetStartTime()

void ns3::SatSGP4MobilityModel::SetStartTime ( const JulianDate & t )

Set the time instant considered as the simulation start.

Parameters

t	the time instant to be considered as simulation start.

Definition at line 99 of file satellite-sgp4-mobility-model.cc.

References m_start.

Referenced by SatSGP4MobilityModel().

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◆ SetTleInfo()

void ns3::SatSGP4MobilityModel::SetTleInfo ( const std::string & tle )

Set satellite's TLE information required for its initialization.

Parameters

tle	The two lines of the TLE data format.

Definition at line 204 of file satellite-sgp4-mobility-model.cc.

References DoGetGeoPosition(), elsetrec::error, GetTleEpoch(), m_sgp4_record, m_start, m_tle1, m_tle2, sgp4(), TleSatInfoWidth, twoline2rv(), and WGeoSys.

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◆ TemeToPef()

SatSGP4MobilityModel::Matrix ns3::SatSGP4MobilityModel::TemeToPef ( const JulianDate & t )

staticprivate

Retrieve the matrix for converting from TEME to PEF at a given time.

Parameters

t When.

Returns: the TEME-PEF conversion matrix.

Definition at line 300 of file satellite-sgp4-mobility-model.cc.

References ns3::JulianDate::GetGmst().

Referenced by rTemeTorItrf(), and rvTemeTovItrf().

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Member Data Documentation

◆ m_lastPosition

GeoCoordinate ns3::SatSGP4MobilityModel::m_lastPosition

mutableprivate

Last saved satellite position.

Definition at line 196 of file satellite-sgp4-mobility-model.h.

Referenced by DoGetGeoPosition(), and DoSetGeoPosition().

◆ m_sgp4_record

elsetrec ns3::SatSGP4MobilityModel::m_sgp4_record

mutableprivate

SGP4/SDP4 record.

Definition at line 141 of file satellite-sgp4-mobility-model.h.

Referenced by DoGetGeoPosition(), DoGetVelocity(), GetTleEpoch(), IsInitialized(), and SetTleInfo().

◆ m_start

JulianDate ns3::SatSGP4MobilityModel::m_start

private

Simulation absolute start time.

Definition at line 201 of file satellite-sgp4-mobility-model.h.

Referenced by DoGetGeoPosition(), DoGetVelocity(), GetStartTime(), SetStartTime(), and SetTleInfo().

◆ m_startStr

std::string ns3::SatSGP4MobilityModel::m_startStr

private

Simulation absolute start time in string format.

Definition at line 206 of file satellite-sgp4-mobility-model.h.

Referenced by SatSGP4MobilityModel(), and GetTypeId().

◆ m_timeLastUpdate

Time ns3::SatSGP4MobilityModel::m_timeLastUpdate

mutableprivate

Last position update time.

Definition at line 221 of file satellite-sgp4-mobility-model.h.

Referenced by DoGetGeoPosition().

◆ m_tle1

std::string ns3::SatSGP4MobilityModel::m_tle1

private

Definition at line 140 of file satellite-sgp4-mobility-model.h.

Referenced by IsInitialized(), and SetTleInfo().

◆ m_tle2

std::string ns3::SatSGP4MobilityModel::m_tle2

private

satellite's TLE data.

Definition at line 140 of file satellite-sgp4-mobility-model.h.

Referenced by IsInitialized(), and SetTleInfo().

◆ m_updatePositionEachRequest

bool ns3::SatSGP4MobilityModel::m_updatePositionEachRequest

private

Compute position each time a packet is transmitted.

Definition at line 211 of file satellite-sgp4-mobility-model.h.

Referenced by DoGetGeoPosition(), and GetTypeId().

◆ m_updatePositionPeriod

Time ns3::SatSGP4MobilityModel::m_updatePositionPeriod

private

Period of satellite position refresh, if UpdatePositionEachRequest is false.

Definition at line 216 of file satellite-sgp4-mobility-model.h.

Referenced by DoGetGeoPosition(), and GetTypeId().

◆ TleSatInfoWidth

const uint32_t ns3::SatSGP4MobilityModel::TleSatInfoWidth = 69

static

Satellite's information line size defined by TLE data format.

Definition at line 49 of file satellite-sgp4-mobility-model.h.

Referenced by SetTleInfo().

◆ WGeoSys

const gravconsttype ns3::SatSGP4MobilityModel::WGeoSys = wgs72

static

World Geodetic System (WGS) constants to be used by SGP4/SDP4 models.

Definition at line 47 of file satellite-sgp4-mobility-model.h.

Referenced by DoGetGeoPosition(), DoGetVelocity(), and SetTleInfo().

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

/builds/sns3/satellite/satellite/model/satellite-sgp4-mobility-model.h
/builds/sns3/satellite/satellite/model/satellite-sgp4-mobility-model.cc

Classes

Public Member Functions

Static Public Member Functions

Static Public Attributes

Private Member Functions

Static Private Member Functions

Private Attributes

Additional Inherited Members

Detailed Description

Constructor & Destructor Documentation

◆ SatSGP4MobilityModel()

◆ ~SatSGP4MobilityModel()

Member Function Documentation

◆ DoGetGeoPosition()

◆ DoGetPosition()

◆ DoGetVelocity()

◆ DoSetGeoPosition()

◆ DoSetPosition()

◆ GetInstanceTypeId()

◆ GetStartTime()

◆ GetTleEpoch()

◆ GetTypeId()

◆ IsInitialized()

◆ PefToItrf()

◆ rTemeTorItrf()

◆ rvTemeTovItrf()

◆ SetStartTime()

◆ SetTleInfo()

◆ TemeToPef()

Member Data Documentation

◆ m_lastPosition

◆ m_sgp4_record

◆ m_start

◆ m_startStr

◆ m_timeLastUpdate

◆ m_tle1

◆ m_tle2

◆ m_updatePositionEachRequest

◆ m_updatePositionPeriod

◆ TleSatInfoWidth

◆ WGeoSys