Earth Observation Mission CFI Software DataHandling Software User Manual |
Class for containing a satellite state vector for a given time. More...
Public Member Functions | |
OsvRec () | |
Default constructor. | |
OsvRec (double taiTim, double utcTim, double ut1Tim, long absOrbi, long referFrame, long timeRef, const double *posi, const double *velo, double qual) | |
Constructor with parameters. | |
Public Attributes | |
double | taiTime |
TAI time. | |
double | utcTime |
UTC time. | |
double | ut1Time |
UT1 time. | |
long | absOrbit |
Absolute orbit. | |
long | refFrame |
Reference frame. | |
long | timeRefOf |
Reference time. | |
double | position [3] |
Position vector (x, y, z components). | |
double | velocity [3] |
Velocity vector (x, y, z components). | |
double | quality |
Quality index. |
Class for containing a satellite state vector for a given time.
EECFI::OsvRec::OsvRec | ( | ) | [inline] |
Default constructor.
EECFI::OsvRec::OsvRec | ( | double | taiTim, | |
double | utcTim, | |||
double | ut1Tim, | |||
long | absOrbi, | |||
long | referFrame, | |||
long | timeRef, | |||
const double * | posi, | |||
const double * | velo, | |||
double | qual | |||
) |
Constructor with parameters.
Absolute orbit.
double EECFI::OsvRec::position[3] |
Position vector (x, y, z components).
double EECFI::OsvRec::quality |
Quality index.
Reference frame.
double EECFI::OsvRec::taiTime |
TAI time.
Reference time.
double EECFI::OsvRec::ut1Time |
UT1 time.
double EECFI::OsvRec::utcTime |
UTC time.
double EECFI::OsvRec::velocity[3] |
Velocity vector (x, y, z components).