Class for reading/writing orbit files. More...

Inheritance diagram for EECFI::OrbitFile:

Public Member Functions
	OrbitFile ()
	Default constructor.
	OrbitFile (const std::string &fileNam)
	Constructor with file name.
	OrbitFile (const OrbitFile &other)
	~OrbitFile () NOEXCEPT
	Destructor.
OrbitFile &	operator= (const OrbitFile &other)
void	read (const bool readFroFlag, const bool readingOsvFlag)
	Read the whole file data block.
void	read (const bool readFroFlag, const double startRange, const double stopRange, const bool readingOsvFlag)
	Read the file data block between startRange and stopRange in orbits.
void	read (const bool readFroFlag, const long timeRef, const double startRange, const double stopRange, const bool readingOsvFlag)
	Read the file data block between startRange and stopRange in days.
void	write (const std::string &fileNam, const FixedHeader &fixedHead, const std::vector< OsvRec > &osvData)
	Write the file.
void	decimate (double decimationDeltaTime, OrbitFile &osvOut)
	Decimate the list of orbit state vectors according to input delta time.
long	xsltAdd ()
	Add xslt reference with default stylesheet.
Public Attributes
std::vector< OsvRec >	osvRec
	Vector of state vectors.

Detailed Description

Class for reading/writing orbit files.

Constructor & Destructor Documentation

EECFI::OrbitFile::OrbitFile ( )

Default constructor.

EECFI::OrbitFile::OrbitFile ( const std::string & fileNam ) [explicit]

Constructor with file name.

EECFI::OrbitFile::OrbitFile ( const OrbitFile & other )

Copy constructor.

Parameters:

other

The OrbitFile to copy from

EECFI::OrbitFile::~OrbitFile ( )

Destructor.

Member Function Documentation

void EECFI::OrbitFile::decimate	(	double	decimationDeltaTime,
		OrbitFile &	osvOut
	)

Decimate the list of orbit state vectors according to input delta time.

Being t0 the time of the 1st state vector of input list (calling object) and D the decimationDeltaTime, the state vectors from the input list that will be included in the output list will be those closer to every time t=t0+k*D (k=1,2...n). Important: the fixed header of calling object must have been read.

Parameters:

	decimationDeltaTime	Number of seconds used for decimation.
	osvOut	Output Orbit File with the decimated list and corresponding Fixed header.

References EECFI::CfiError::addMsg(), EECFI::EEFile::fixedHeader, osvRec, EECFI::CfiClass::throwWarn, EECFI::FixedHeader::valStartDate, EECFI::FixedHeader::valStopDate, and EECFI::FixedHeader::version.

OrbitFile & EECFI::OrbitFile::operator= ( const OrbitFile & other )

Copy assigment operator.

Parameters:

other

The OrbitFile to copy/assign from

References osvRec.

void EECFI::OrbitFile::read	(	const bool	readFroFlag,
		const bool	readingOsvFlag
	)

Read the whole file data block.

Parameters:

	readFroFlag	Type of input file: "true" for ROF and DORIS files "false" for POF files.
	readingOsvFlag	Select if state vectors are read (true) or only times and orbit numbers (false).

References EECFI::EEFile::fileName, EECFI::EEFile::fileType, osvRec, and EECFI::CfiClass::throwWarn.

void EECFI::OrbitFile::read	(	const bool	readFroFlag,
		const long	timeRef,
		const double	startRange,
		const double	stopRange,
		const bool	readingOsvFlag
	)

Read the file data block between startRange and stopRange in days.

Parameters:

	readFroFlag	Type of input file: "true" for ROF and DORIS files "false" for POF files.
	readingOsvFlag	Select of state vectors are read (true) or only times and orbit numbers (false).
	startRange	Start day.
	stopRange	Stop day.
	timeRef	Time reference.

References EECFI::EEFile::fileName, EECFI::EEFile::fileType, osvRec, and EECFI::CfiClass::throwWarn.

void EECFI::OrbitFile::read	(	const bool	readFroFlag,
		const double	startRange,
		const double	stopRange,
		const bool	readingOsvFlag
	)

Read the file data block between startRange and stopRange in orbits.

Parameters:

	readFroFlag	Type of input file: "true" for ROF and DORIS files "false" for POF files.
	readingOsvFlag	Select of state vectors are read (true) or only times and orbit numbers (false).
	startRange	Start orbit.
	stopRange	Stop orbit.