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ORBEX entry to write out. More...
ORBEX entry to write out.
Data Fields | |
| SatSys | Sat = {} | 
| Satellite ID.   | |
| Vector3d | pos = Vector3d::Zero() | 
| Satellite position (m)   | |
| Vector3d | vel = Vector3d::Zero() | 
| Satellite velocity (m/s)   | |
| double | clk = NO_CLK | 
| Satellite clock (microsecond) & clock-rate (nanosecond/s)   | |
| double | clkVel = NO_CLK | 
| Vector3d | posStd = Vector3d::Ones() * NO_PV_STD | 
| Satellite position std (mm)   | |
| Vector3d | velStd = Vector3d::Ones() * NO_PV_STD | 
| Satellite velocity std (micrometer/s)   | |
| double | clkStd = NO_CLK_STD | 
| Satellite clock (picosecond)   | |
| double | clkVelStd = NO_CLK_STD | 
| Satellite clock-rate std (femtosecond/s)   | |
| Quaterniond | q = {0, 0, 0, 0} | 
| Satellite attitude in quaternions.   | |
| double OrbexEntry::clk = NO_CLK | 
Satellite clock (microsecond) & clock-rate (nanosecond/s)
| double OrbexEntry::clkStd = NO_CLK_STD | 
Satellite clock (picosecond)
| double OrbexEntry::clkVel = NO_CLK | 
| double OrbexEntry::clkVelStd = NO_CLK_STD | 
Satellite clock-rate std (femtosecond/s)
| Vector3d OrbexEntry::pos = Vector3d::Zero() | 
Satellite position (m)
| Vector3d OrbexEntry::posStd = Vector3d::Ones() * NO_PV_STD | 
Satellite position std (mm)
| Quaterniond OrbexEntry::q = {0, 0, 0, 0} | 
Satellite attitude in quaternions.
| SatSys OrbexEntry::Sat = {} | 
Satellite ID.
| Vector3d OrbexEntry::vel = Vector3d::Zero() | 
Satellite velocity (m/s)
| Vector3d OrbexEntry::velStd = Vector3d::Ones() * NO_PV_STD | 
Satellite velocity std (micrometer/s)