 |
Earth Observation Mission CFI Software DataHandling Software User Manual |
 |
| |
Earth Observation Mission CFI Software DataHandling Software User Manual |
|
Class for reading/writing orbit files. More...
Public Member Functions | |
| OrbitFile () | |
| Empty constructor. | |
| OrbitFile (const string fileNam) | |
| Constructor with file name. | |
| ~OrbitFile () | |
| Destructor. | |
| void | read (const bool readFroFlag, const bool readingOsvFlag) throw (CfiError) |
| Read the whole file data block. | |
| void | read (const bool readFroFlag, const double startRange, const double stopRange, const bool readingOsvFlag) throw (CfiError) |
| 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) throw (CfiError) |
| Read the file data block between startRange and stopRange in days. | |
| void | write (const string fileNam, FixedHeader &fixedHead, vector< OsvRec > &osvData) throw (CfiError) |
| Write the file. | |
| void | decimate (double decimationDeltaTime, OrbitFile &osvOut) throw (CfiError) |
| Decimate the list of orbit state vectors according to input delta time. | |
Public Attributes | |
| vector< OsvRec > | osvRec |
| Vector of state vectors. | |
Class for reading/writing orbit files.
| EECFI::OrbitFile::OrbitFile | ( | ) |
Empty constructor.
References EECFI::EEFile::fileType.
| EECFI::OrbitFile::OrbitFile | ( | const string | fileNam | ) |
Constructor with file name.
| EECFI::OrbitFile::~OrbitFile | ( | ) |
Destructor.
References EECFI::EEFile::fixedHeader, and osvRec.
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.
| decimationDeltaTime | Number of seconds used for decimation. | |
| osvOut | Output Orbit File with the decimated list and corresponding Fixed header. |
References EECFI::CfiError::addMsg().
| void EECFI::OrbitFile::read | ( | const bool | readFroFlag, | |
| const double | startRange, | |||
| const double | stopRange, | |||
| const bool | readingOsvFlag | |||
| ) | throw (CfiError) |
Read the file data block between startRange and stopRange in orbits.
| 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. |
| void EECFI::OrbitFile::read | ( | const bool | readFroFlag, | |
| const bool | readingOsvFlag | |||
| ) | throw (CfiError) |
Read the whole file data block.
| 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). |
| void EECFI::OrbitFile::read | ( | const bool | readFroFlag, | |
| const long | timeRef, | |||
| const double | startRange, | |||
| const double | stopRange, | |||
| const bool | readingOsvFlag | |||
| ) | throw (CfiError) |
Read the file data block between startRange and stopRange in days.
| void EECFI::OrbitFile::write | ( | const string | fileNam, | |
| FixedHeader & | fixedHead, | |||
| vector< OsvRec > & | osvData | |||
| ) | throw (CfiError) |
Write the file.
| fileNam | Name of the file to write. | |
| fixedHead | FixedHeader object with fixed header data. | |
| osvData | Vector of state vectors. |
| vector<OsvRec> EECFI::OrbitFile::osvRec |
Vector of state vectors.
Referenced by ~OrbitFile().
1.7.1