ts::SAT::satellite_position_v2_info_type::earth_orbiting_satallite_type Class Reference

Representation of an earth orbiting satellite position. More...

#include <tsSAT.h>

Inheritance diagram for ts::SAT::satellite_position_v2_info_type::earth_orbiting_satallite_type:

Collaboration diagram for ts::SAT::satellite_position_v2_info_type::earth_orbiting_satallite_type:

Public Member Functions
	earth_orbiting_satallite_type ()=default
	Default constructor.
	earth_orbiting_satallite_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
ieee_float32_t	argument_of_perigree = 0
	Argument of perigee in degrees.
ieee_float32_t	day_fraction = 0
	Epoch day fraction.
uint16_t	day_of_the_year = 0
	16 bits. Epoch day of the year.
ieee_float32_t	drag_term = 0
	Drag term (or radiation pressure coefficient or BSTAR) in 1/EarthRadii.
ieee_float32_t	eccentricity = 0
	Shape of the orbit(0 = circular, Less than 1 = elliptical).
uint8_t	epoch_year = 0
	8 bits. lLast 2 digits of the epoch year.
ieee_float32_t	inclination = 0
	Angle between the equator and the orbit plane in degrees.
ieee_float32_t	mean_anomaly = 0
	Mean anomaly in degrees.
ieee_float32_t	mean_motion = 0
	Mean number of orbits per day the object completes in revolutions/day.
ieee_float32_t	mean_motion_first_derivative = 0
	Mean motion derivative divided by 2 in revolutions per day-squared.
ieee_float32_t	mean_motion_second_derivative = 0
	The mean motion second derivative divided by 6 in revolutions per day-cubed.
ieee_float32_t	right_ascension_of_the_ascending_node = 0
	Right ascension of the ascension node in degrees.

Detailed Description

Representation of an earth orbiting satellite position.

See also

ETSI EN 300 648, 5.2.11.2

Constructor & Destructor Documentation

earth_orbiting_satallite_type()

ts::SAT::satellite_position_v2_info_type::earth_orbiting_satallite_type::earth_orbiting_satallite_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::earth_orbiting_satallite_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::earth_orbiting_satallite_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::earth_orbiting_satallite_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::earth_orbiting_satallite_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

eccentricity

ieee_float32_t ts::SAT::satellite_position_v2_info_type::earth_orbiting_satallite_type::eccentricity = 0

Shape of the orbit(0 = circular, Less than 1 = elliptical).

The value provided is the mean eccentricity.

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

• tsSAT.h