ts::SAT::satellite_position_v2_info_type Class Reference

Representation of a satellite position (version 2). More...

#include <tsSAT.h>

Inheritance diagram for ts::SAT::satellite_position_v2_info_type:

Collaboration diagram for ts::SAT::satellite_position_v2_info_type:

Classes
class	earth_orbiting_satallite_type
	Representation of an earth orbiting satellite position. More...
class	geostationary_position_type
	Representation of a geostationary satellite position. More...

Public Member Functions
	satellite_position_v2_info_type ()=default
	Default constructor.
	satellite_position_v2_info_type (PSIBuffer &buf)
	Read-in constructor.
virtual void	deserialize (PSIBuffer &buf) override
	This method deserializes (populates) the attributes of a geostationary satellite.
virtual bool	fromXML (const xml::Element *element) override
	This method populates this object from XML attributes and sub-element.
virtual void	serialize (PSIBuffer &buf) const override
	This method serializes the attributes of a geostationary satellite.
virtual void	toXML (xml::Element *root) override
	This method converts this object to XML by populating necessary attributes and sub-elements into the provided element.

Public Attributes
std::optional< earth_orbiting_satallite_type >	earthOrbiting {}
	attributes of an earth orbiting satellite
std::optional< geostationary_position_type >	geostationaryPosition {}
	attributes of a geostationary satellite.
uint8_t	position_system = 0
	1 bit.The positioning system that is used for this satellite.
uint32_t	satellite_id = 0
	24 bits, A label to identify the satellite that is detailed here.

Detailed Description

Representation of a satellite position (version 2).

See also

ETSI EN 300 648, 5.2.11.2

Constructor & Destructor Documentation

satellite_position_v2_info_type()

ts::SAT::satellite_position_v2_info_type::satellite_position_v2_info_type ( PSIBuffer &  buf )

inline

Read-in constructor.

Parameters

[in,out]

buf

Deserialization buffer. Read the descriptor payload from buf. The end of read is the end of the binary payload. If any kind of error is reported in the buffer or if the payload is not completely read, the deserialization is considered as invalid.

Member Function Documentation

fromXML()

virtual bool ts::SAT::satellite_position_v2_info_type::fromXML ( const xml::Element *  element )

overridevirtual

This method populates this object from XML attributes and sub-element.

Parameters

[in]

element

The element whose attributes and sub-elements are parsed to construct this object

Returns

true if the requisite attributes and sub-elements are available and correct

Implements ts::SAT::SAT_base.

toXML()

virtual void ts::SAT::satellite_position_v2_info_type::toXML ( xml::Element *  root )

overridevirtual

This method converts this object to XML by populating necessary attributes and sub-elements into the provided element.

Parameters

[in,out]

root

The element whose attributes and sub-elements are added to to represent values in this object

Implements ts::SAT::SAT_base.

serialize()

virtual void ts::SAT::satellite_position_v2_info_type::serialize ( PSIBuffer &  buf ) const

overridevirtual

This method serializes the attributes of a geostationary satellite.

Parameters

[in,out]

buf

A PSIBuffer with the appropriate size for the section payload.

Implements ts::SAT::SAT_base.

deserialize()

virtual void ts::SAT::satellite_position_v2_info_type::deserialize ( PSIBuffer &  buf )

overridevirtual

This method deserializes (populates) the attributes of a geostationary satellite.

Parameters

[in,out]

buf

Deserialization buffer. Read the descriptor payload from buf. The end of read is the end of the binary payload. If any kind of error is reported in the buffer or if the payload is not completely read, the deserialization is considered as invalid.

Implements ts::SAT::SAT_base.

Member Data Documentation

position_system

uint8_t ts::SAT::satellite_position_v2_info_type::position_system = 0

1 bit.The positioning system that is used for this satellite.

The value '0' can be used for a satellite in geostationary orbit and the value '1' can be used for any earth-orbiting satellite.

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

• tsSAT.h